GB2065836A - Engine control systems - Google Patents

Abstract

An automotive hydrostatic transmission (2, 4) is controlled by a system providing conjoint control of transmission ratio and engine fuel supply according to pre-established algebraic expressions to optimise engine fuel consumption. The system shown includes an accelerator potentiometer (Ap) which provides direct control of the motor swashplate and indirect control of system pressure via the engine throttle, the pump swashplate being controlled as a function of system pressure. The system may also include an accumulator providing for regenerative braking, and a mechanical bypass of the hydrostatic transmission which becomes effective above a preselected vehicle speed. <IMAGE>

Description

SPECIFICATION Engine control systems This invention relates to engine control systems.

In engines such as those used in, for example, cars, trucks, earth moving machinery or in stationary engines it is a continual problem to optimize the engine speed in relation to various parameters. Particularly with the gasoline/spark ignition version of the receiprocating engine, considerable effort has previously been expended with a view to optimizing the engine.

According to the present invention there is provided a system for optimizing the operation of an engine for maximum output including a first device and a second device, each interconnected to control the engine speed in accordance with a function of at least one algebraic expression.

The first and second devices may conveniently be swash plates respectively in a pump and motor.

Embodiments of the present invention will now be described, by way of example, with reference to the accompanying drawings in which: Fig. 1 is a flow and control diagram of an embodiment of the invention.

Fig. 1 A is a modification of the embodiment shown in Fig. 1, particularly for use with a diesel engine, Fig. 2 represents a portion of Fig. 1, particularly showing the hydraulics system, Fig. 3 is a diagrammatic representation of part of the system as used for an automobile and showing the clutches, Fig. 4 is a representation of a control curve plotting certain equations as a function of the accelerator potentiometer output, Fig. 5 is a diagrammatic representation of some of the electronic control logic, Fig. 6 is a graphical performance map for a Toyota 2TC engine, Fig. 7 ;s a diagrammatical representation of a mathematicai flow chart, and Fig. 8 is a representation of a brake control curve.

It will be understood that a gasoline engine in an automobile which has a conventional transmission system very rarely works at its optimum specific fuel consumption. Attempts have been made to optimize the fuel consumption of a car under highway conditions by providing three-speed gear boxes and other conventional systems. It is well known that if an infinite number of gears was available then an extremely talented driver could reduce fuel consumption to about half the normal value.

Using a hydrostatic system in the transmission it is possible to provide a continuously variable speed ratio between the engine and the road wheels. The described embodiment of the present invention provides a hydraulic system whose efficiency can be optimized whereby the operating efficiency of the engine is optimized in accordance with road conditions as they change so that an improved specific fuel consumption for any given road load is obtained. This is one advantageous result which may be achieved by using the described embodiment of the invention.

A second advantageous result which may be achieved by using the described embodiment of the invention is that un-used kinetic energy can be stored hydrostatically in an accumulator by compressing a gas such as nitrogen. As is well known, when, for example, a car is driven towards traffic lights which suddenly change to red whereby the car has to stop, then kinetic energy is wasted. However, by using the described embodiment of the invention, this kinetic energy of the car can be stored by causing it to drive liquid into a cylinder. When the car gets a green light, then the kinetic energy is released and re used to drive the car up to speed again.

Figure 1 is a flow and control diagram of an embodiment of the invention. It will be seen that two hydraulic units, a pump 2 and a motor 4 are provided, whereby the pump drives the motor. Both these units are variable displacement units using swash plates together with an electronic system to control the angle of the swash plates in such a way as to optimize hydraulic pressure and flow having regard to efficiency and engine torque as well as speed. This is basically effected by using three equations, as described below.

For convenience, we set forth below a list of the symbols which will be used in the following description: LIST OF SYMBOLS a Acceleration BHPh Brake horsepower hour BMEP Brake mean effective pressure BSFC Brake specific fuel consumption D Diameter of accumulator D, Rolling drag = k1 = 45 Ib Da Aerodynamic drag Dt Total drag = Dr + Da d1 Pump displacement d2 Motor displacement AE Energy stored per unit mass of gas F Braking force F' Thrust force g Acceleration of gravity = 32.2 [ft/s2] h Conversion factor = 33000 [ft Ib/min HP] k1 Rolling drag = Dr k2 Drag coefficient m Mass=w/g N1 Engine power output N2 Motor power output n1 Rotational speed of engine and pump shaft n2 Rotational speed of motor shaft n2c Motor speed command function f(Ap) n1c Engine speed command function f(Ap) n3 Rotational speed of axle n1 Engine speed control function f[APc - P3)] P Pressure P1 Accumulator pressure AP2 System pressure P3 Motor outlet pressure AP3 Accumulator pressure diff. P4 - P3 P4 V 30.1 inlet pressure tP4 = APcAPcP2P4 APc Pressure command function f(Ap) P5 Reservoir pressure P11 Initial value of P1 P12 Maximum value of P1 = maximum acceptable system pressure r Roadwheel effective radius (0.875 ft) r2 Motor to road wheel ratio 2.7/1 r1 Mechanical bypass ratio 1.3/1 Rig constant (equivalent road wheel radius) = r/r2 s Distance covered T1 Engine torque T2 Motor torque T Absolute temperature (Appendix I and Reference 1) V Volume of gas in accumulator V Rate of flow of liquid v Velocity over road vimin Minimum initial velocity W Work or kinetic energy w Weight of car w9 Weight of gas in accumulator Displacement of pump expressed as fraction of maximum Displacement of motor expressed as function of maximum 1/In2 Mechanical efficiency of pump and motor 711X72 Leakgage factor of pump and motor p Density of nitrogen gas a Acceptable stress Referring particularly to Figures 1 , 2 and 3, an accelerator potentiometer Ap is controlled by the driver of an automobile in the same manner as he would control the present throttle control or accelerator in a car, but in this embodiment he commands a road wheel speed as the result of a selected voltage or some other parameter.This voltage we will call Ap (accelerator potentiometer). This command from the accelerator potentiometer controls or commands the road wheel speed, i.e. the car velocity. Thus, the road wheel speed n2C is a function (which is equation 12 below) of the potentiometer position or output in Figure 1 and the description below. This means that when the driver makes this command by opening his throttle the electronic control circuits will send the rear swash plate in motor 4 to maximum because, in fact, the road wheel speed cannot immediately be obtained due to car inertia and it takes time for the car to obtain that speed. In this way the system is prepared for receiving maximum acceleration if demanded.

The accelerator potentiometer also commands a system hydraulic pressure as a function of the same potentiometer (equation 1 3 below). Equation 13 therefore controls the system pressure via the throttle or, in other words, equation 13 is responsible for opening the throttle, which is a butterfly valve 6, to a position that can produce a given pressure in the system. This pressure is identified as AP2 and is the pressure that, in fact, creates the acceleration via the hydraulic motor. It is now necessary to control the swash plate of the pump 2 and in this way optimize the engine torque for best fuel consumption.

This is done not directly as a function of Ap, the accelerator potentiometer position, but as a subfunction of a system pressure. When the system pressure command is effected it commands, via equation 14 below, an equivalent engine speed in r.p.m. by adjusting at. This is the displacement of the swash plate in the pump 2.

Therefore, the engine's operating parameters have been optimized to match road conditions at the best fuel consumption.

The reason for controlling engine speed as a function of pressure is so that the engine does not attempt to supply the energy that may be available from the accumulator.

The above description is concerned with the n, command cycle and this will be considered again later. For the moment, the regeneration cycle will be considered.

A car may be travelling at, for example 30 m.p.h. and may suddenly need to be stopped. This may be, for example when traffic lights are red and the driver stops the car as a result of the system permitting the angle of the swash plate of the motor 4 to be increased. This pumps liquid from the reservoir to the accumulator against the head of gas in the accumulator, thereby storing the kinetic energy of the car from that speed down to zero. When the driver subsequently wants to move off and he opens his accelerator there may still be energy stored in the accumulator. Obviously the accelerator potentiometer should not command engine energy whilst accumulator energy is available because the accumulator must be emptied ready for a regeneration cycle when the car is next stopped.This is why n2C has been used as a function of pressure to control the engine speed via X" i.e., through the forward swash plate. What happens, in effect is, that APc minus AP3 makes the command for engine speed.

IfAP3 equais APc the engine will not operate but the car will move off under the accumulator energy.

åP3 is the pressure in the accumulator, and APc is the pressure commanded by the driver via the accelerator potentiometer. Should the driver increase his throttle command to a point where he commands a pressure greater than the accumulator pressure then APc minus AP3 is a positive number and the engine will now assist the accumulator by causing a pressure differential across check valve CV1, (Fig. 1) thus closing the check valve and putting the pressure which would be created by the engine into series with the pressure from the accumulator and thus driving the car with the sum of the two.

It will be appreciated that at all times, when the throttle is open the accelerator switch AS causes all solenoid valves to open simultaneously, i.e. SV1, 2 and 3.

To recap, - when the drive commands a pressure by virtue of opening his throttle, if that pressure is less than the pressure in the accumulator there will be a negative command to the engine side of the electronic control circuits and this causes nothing to happen as far as the engine is concerned, but the accelerator switch will open the control valves allowing pressure from the accumulator to pass through CV1, i.e. check valve 1, and along the pressure line so as to drive the hydraulic motor before returning to the reservoir. Recapping again, should the driver now change his mind and command a pressure higher than the pressure in the accumulator, then the difference will be positive. This difference will cause a command for engine power via the equations previously referred to.The operation of the swash plate at the pump and the engine throttle, i.e. butterfly valve 6, will cause the pressure to rise across CV1 thus closing that valve. This now causes the engine effort to be added to the effort from the accumulator.

The system so far is capable of providing optimum control over engine fuel consumption and hydraulic system efficiency under steady state road conditions and this is achieved by the design parameters of the embodiment described. However, this is a variable because no account has been taken in these equations for change of grade because it is not known how steep the hill is going to be that that the driver is going to climb. Also, no account has been taken for the change of wind, - this would mean that the system would be incapable of following the curves and something would have to change. The thing that would change would be engine power which would increase and most probabaly go beyond the optimum.It must be remembered that in the steady state condition the n2 command has been realized and the swash plate of the motor has found its optimum position for that steady state conditions.

If a car encountered a hill or a head wind the car would tend to slow down, and the motor swash plate would then remodulate. This would cause the system flow to increase for the same car speed and this would tend to increase the engine torque. This would be a change which would take place in the swash plate of the pump 2.

To avoid exceeding permissible torque or optimum torque another feedback signal has been introduced and is derived from the actual angle of the swash plate at the motor - A at S2 in Fig. 1. This signal is fed to A at the left side of Figure 1 whereby the engine speed command N,, is modified by that function which is na2 /O/x, x being a parameter dependent on car design.

It is necessary to provide for reversing of the car and still keep the system flow in the same direction so that all components work in the normal way even in reverse. To do this a switch is introduced which reverses n2C and n2C inputs and causes the swash plate to move to the other side of center. This reverses the wheels whilst keeping the system operating in the same direction. A drive-park control is also required to allow the driver to start and rev. his engine without moving the vehicle and this is done by a drive-park switch which interrupts the signal from the basic AP command. Under these conditions there will be no positive swash plate angle at S, and no pressure command. The engine may therefor be started and the speed controlled by a hand operated accelerator AH.

It should be said, of course, that anything that can be done with electronics can be done mechanically. In fact, controls can be produced by hydraulics, - and hydraulic amplifiers are a possibility even with sound which can be simplified and produced hydraulically as well as electronically.

Controlls to perform the same function could also be built using pneumatic principles, but the thing to be concerned with is the intelligence of these controls and what they do, - whether they are electronic controls or other means.

The reservoir and charge pump perform another, second, function. They serve to pressurize the low pressure side of the system which at all times must be at a specific pressure whether the car is in regeneration mode or drive mode. A system of two check valves is therefore used. When the car is regenerating it supplies pressure to what was previously the high pressure side and vice versa, when the car goes into the other mode.

Although a hydrostatic system like this, improves the gas mileage of an automobile on the road, for example, or any other similar such energy system, it is mainly because of the fact that engines require tailoring to their load conditions. The hydraulic system in itself loses more energy than a conventional transmission as such. Therefore while this system provides better road gas mileage throughout the control parameters, it could be done better if at certain points a straight-through mechanical system could be incorporated. In any drive system there is probably a range where a straight-through non-variable mechanical system would be optimum. This is the case in the described system in which at 55 feet a second and upwards, a straight-through mechanical drive for a properly chosen ratio does optimize the system without the hydraulic arrangement.Therefor, it is arranged so that above 55 feet per second when n2C equals n2, a mechanical drive is clutched into service and the hydraulics are clutched out. The control for this comes from the n2 command system at C which closes and opens the clutches as required and shown on the diagram. This in the present case improves the gas mileage during that part of the range by approximately an additional 25to.

The following description is both theoretical and practical since it is based on the constructed embodiment of this invention, it being appreciated that some of the material above may be repeated.

However, for completeness sake it is included in the present description.

In the present embodiment, continuously variable units are used for both hydraulic pump and motor (Figures 1 and 2). A hydro-pneumatic accumulator is so incorporated that automatic combined and independent operation with the engine is provided. The pressurized reservoir feeds the accumulator while maintaining system boost pressure and a clutch operated mechanical bypass is used to eliminate hydraulic system losses in the steady state cruise range.

The advantages of this arrangement are for the most part self-evident, but the importance of the second swash plate at m2 should be emphasized viz: a) It provides modulated deceleration control, b) modulated accumulator output with minimum energy loss, and c) compietes the control loop permitting system pressure as well as engine torque to be optimized Electronic control of the engine throttle and both swash plates is based on three read only memories which receive coordinates resulting from three equations (Figs. 4 and 5). A flow system capable of satisfying this philosophy is shown in Fig. 2 where two continuously variable units are shown at m, and m2 in a hydrostatic loop, with an accumulator at nil suction.The reservoir supplies boost to both sides of the loop via CV3 and CV4 GS well as providing accumulator flow and makeup is provided by the makeup pump. The throttle potentiometer Ap provides the primary driver-input (Figs. 4 and 5) and the brake potentiometer provides regenerative control and mechanical brakes. The mode control DPS confirms , and 2 = zero, C, and ClA disengaged (Fig. 3) and SV1,2,3, closed when in the park P position.

A hand control is provided for engine starting etc. and an override control (for simplicity not shown) is provided, permitting the driver to lock the system into hydraulic mode when driving conditions are such that excessively frequent shifts would occur As reverse is accomplished by running the motor swash plate in the reverse quadrant, hydraulic flow and characteristics are identical to forward operation.

Basic Theoretical Considerations as applied to the embodiment Figure 6 which is a performance map of the Toyota 2TC engine, derived from a rig calibration in actual experiments, demonstrates the efficiency versus n, and torque, in terms of BSFC. It is evident from this map that engine efficiency can be optimized for any load demand providing the appropriate engine speed is maintained. Viz: efficiency cc Torque.

Also T, cc S,\P2 which suggests controlling S, by AP2 via n,. It will be evident after some thought that control initiation would not take place as AP2 could not be raised, s, 1 being initially zero.

Consequently n, is controlled by a function of APc minus AP3 via S, which has the facility to optimize engine torque also when the accumulator is charge, at which time AP2 + AP at the pump. The volumetric efficiency of a hydrostatic system being approximately proportional to pressure, suggests the optimization of the pressure power relationship. The latter may be accomplished by controlling system pressure by Ap via the throttle valve and when the accumulator is charged the engine contribution is proportional to APc minus AP3.

A fixed enginejroad wheel ratio is superior to hydraulic drive for a considerable portion of the steady state range due to its better efficiency (Table 2A and Fig. 3). It is arranged so that no motoring losses result from the hydraulic components, nor does leakage occur other than that produced by the low boost pressure.

The regeneration of braking energy, which is considerable in urban driving, is treated in Appendix I (Fig. 8).

Hydraulic Operation Assuming some charge in the accumulator, the engine running and the drive/park control (DPC) in the drive position: (Fig. 2). When the accelerator is depressed: a) Ap commands a pressure APc via the butterfly valve b) APc commands n2 resulting in S2 > minimum c) SV, 2 3 open with n2 command > zero d) Vehicle accelerates under accumulator influence when APc < AP3.

Flow is via C B F and E In the event that the pressure commanded is greater than AP3: e) APc - AP3 increases the butterfly setting matching AP2 to APC f) n2 modulates S2 determining n2 g) n Ic modulates SX determining n, h) AP4 > zero closes CV, putting accumulator pressure and pump pressure into a summation mode.

When the accelerator is closed: i) SV12,3 close with n2 command being zero j) nXc = zero returns S, to zero k) S2 returns to a blocked minimum of 10% applying light breaking.

When the brake is applied: Increasing S2 via the brake potentiometer causes flow to increase from the reservoir to the accumulator via H, F and D.

As will be clear, Figures 1 and 1 a, show a hydrostatic system comprising a carburetted engine driving a variable displacement motor/pump, capable of swash plate operation both sides of centre. An accumulator (ACC) is connected to both sides of the main loop and a reservoir (RES) to the low pressure side. The motor swash plate goes to reverse side of centre for both braking and reverse operation. Check valve (CV1) permits free-wheeling and facilitates accumulator direct operation. When higher pressures are demanded, CV1 being closed by engine generated pressure difference, accumulator flow becomes serial with the pump flow.

Electronic Control: The same potentiometer wiper is operated by both brake and accelerator pedals. The output (Ap) generates two basic commands, engine speed by modulating the throttle valve (6) and system pressure (AP2) by adjusting the motor/swash plate setting (52)77" becomes a function of AP2c -AP3 to compensate tor energy available from HP.The final degree of freedom is under the influence of P1C(X1) by manipulation of the pump swash plate (S). Control techniques using various combinations of parameters applied to this anci other hydraulic arrangements were investigated but the system illustrated, where manifold pressure and engine speed are used to optimize engine operation, was adopted although some of the variations following the same basic logic are acceptable alternatives.

Mode by Mode Operation Park: In this mode the drive/park control of the car (not shown) sends Sr to zero, S2 to maximum, confirms that SV1 (Figures 1 and 2) is closed and opens ignition and control-power supply circuits.

Start: This mode differs from "park" in that power circuits are energized and throttle control under the influence of S3 becomes proportional to Ap. Throttle feed back is omitted in Figure 1 for better readability.

Drive: In this mode all controls are in automatic. Assuming the accumulator empty and the engine running; when the accelerator is depressed, AS closes SV2 and opens SV1. A speed command increases throttle angle. The resulting increase in engine RPM (n,) provides a manifold pressure command that is satisfied by the modulation of S, consequently pump displacement The engine speed/torque relationship is thus determined. Concurrent with the speed command a pressure command is issued LAP2C(Ap) that modulates the motor swash plate (S2), AP2 therefore follows a predetermined curve. Flow of hydraulic fluid is via the main loop only.Should AP2c < AP3 (accumulator charged) then S2 control is provided proportional to Ap, a zero n, command is sent and flow takes place via SV1 and CV1 driving the motor and returning to the Reservoir (RES). When the same conditions prevail except that AP2c > AP3 normal drive conditions prevail except that a pump generated differential pressure accross CV1 closes that valve and flow from the Accumulator (ACC) passes to the inlet of the pump.

Brake: In this mode, when the brake pedal is depressed, a zero n, command is issued and S2 control is switched to direct Ap proportional control. System pressure closes CV1 and flow to ACC is from RES via the motor/pump unit and CV2. Should ACC fully charge during the cycle, constant pressure fluid friction braking continues via RV1. In the event of emergency braking being required, additional pressure on the pedal after the potentiometer has reached its "stop" causes the output of a load cell LC to apply mechanical brakes.

Reverse: This mode operates identically to forward mode except that the drive park control reverses the direction of S2 control and sends the swash plate to the other side of centre.

Mechanical Bypass It is an advantage to bypass the hydraulic system with a direct mechanical drive, during some portion of the vehicle's cruise range. In the subject case this is above about 50 ft/sec. with a 1.3 1 engine to road wheel ratio. This is straightforward design work but two points are made below: 1) An n2 speed command generator (not shown in figure 1) provides n2c(Ap).

The mechanical bypass is activated in steady state only when velocity exceeds 55 ft/sec and n2C = n2. The system reverts to hydraulic mode when n2C > n2 by 10%.

2) The pump and motor are declutched, therefore stationary during operation of the bypass.

The system runs in hydraulic mode until D > 40 ft/sec beyond which the bypass is available. Above 40 ft/sec when n2C = n2 SV2 closes, CIA disengages after 100 ms, C, engages after 100 ms, C2 disengages and throttle goes to direct control [T(Ap)] simultaneously. The system is then running in mechanical bypass mode.

Acceleration is commanded when n2C + 10% > n2 under which circumstances SV2 opens and throttle control reverts to control by APc(Ap) simultaneously; after 100 ms CIA engages and C, disengages simultaneously and C2 engages after 100 ms. The system is thus returned to hydraulic mode until n2 = n2c When the brake potentiometer is operated the system is confirmed in hydraulic mode (Fig. 8) and deceleration is controlled by S2.

Parameters of the Chosen Automobile For the purpose of this study the car is assumed to have an area of A = 1 7 ft2, a drag factor of K = 0.35 and the equivalent dynamic mass is set at m = 77.6 = 2500 Ibw. In the interest of simplification and to remain on the conservative side the latter is also used for rolling resistance computation.

Motor size d2 is based on acceleration requirements at maximum system pressure AP2 = 5000 psi.

It was elected to design for a velocity of 73.33 ft/s to be reached in less than 1 2 sec. So we have to add the inertia force to the drag at this velocity to obtain the total thrust force F' = T2/re + (73.33/12) w/g = 605.9 Ib and for S2 = 1 and q2 = 0.9 we have d2 = 24Fl6/AP22 = 3.29 in 3/rev rhe nearest size available is 3.15 in 3/rev.

The exact treatment of the acceleration process in the appendix shows that the velocity 73.33 ftjs (50 mph) is really attained in 10.9 sec. (see Table 2).

The hydraulic pump should ideally be operating at optimum during normal cruise (say 80 ft/sec.l at which time S, should approximate 90%, n2 at this speed is 2357 rpm and n, to give optimum torqe is about 1380 rpm; hence d, = n2d2S2/n,S, = 3.12 in 3/rev So we choose d, = d2 = 3.15 in 3/rev.

Derivation of Design Parameters The system is required to satisfy three energy equations that may be written: 27cnT,/60 = N for m, and m2 and

= N for the hydraulic loop (AP2 in psi).

As in a mechanical system the hydraulic system must satisfy continuity conditions viz: n,dn'st = d282n2/n'=# and may be treated with the following three equations: 27rT1 = AP2d"S,/77 27rT2 = rAP2d282 T,= K,re + K2(r37r2/302)n22 It is evident that while the torque-speed relationship of m2 is predetermined, this is not for so for m, where n, and T, are variable at any given load providing their product is not changed. In the case of the loop this holds for R7 and AP2. This permits optimization of both engine torque and system pressure as n, and AP2 may be regulated without changing road wheel thrust (Figs. 2, 6 and 7).

The limiting parameter governing optimization is n, for on the one hand m, may not exceed 4000 RPM plus a short duration overrun of some 100 RPM and, in steady plate, engine operation at less than about 450 RPM is impracticable. It was chosen to optimize over an arbitrary steady state range between 10 and 120 ft/sec with 1 3" wheels having an effective radius of 10.5" or r = 0.875 ft.

It is convenient now to list those parameters which are available direct functions of velocity, namely Dt, N2 and T2 (Table 2). Equation 5 may now be derived after N, viz. N, = Nl112X7'2 where efficiencies are estimated. Points along the target curve may now be found by applying values of N, (Fig.

6 and 7) and projecting for n,. A relevant curve may now be defined viz. n,(v). A maximum system AP2 has been chosen (Appendix I) and with reference to efficiency maps of hydraulic pumps and motors, a steady state ranee # 100 to 3000 PSI is established. A linear equation is now provided for AP2(n,) and AP2 (v) Eq. 6 by substitution. The latter is now modified to converge at Ap = 140 and APc =5000, (Fig. 4). This being system maximum pressure difference.

Pump and Motor Size Motor size (D2 = in3/rev) is based on acceleration (lapsed time) requirements at maximum system AP = 5000 PSI, the road wheel radius (r = 0.875 ft) and the overall ratio (r, = 2.7), the latter being chosen to suit n2 limits. A design was chosen for a velocity of 73.3 ft/sec to be reached in 12 seconds.

For average drag (Da) col. 2 of Table 2A is consulted.

The motor size is therefore:

The pump must accommodate the optimum cruise range where 8, is greatest. Parameters are selected therefore at v = 60 ft/sec, where T2 = 26.5, n2 = 1768, #P2 and n, = 855. Then if 77 =0.9

It is evident in this case that pump and motor should be sized similarly and the nearest size conveniently available was 3.1 5 in3/rev viz. m, and m2.

Completion of Table No. 2 and 2A Table 2 is now completed in accordance with the flow diagram (Fig. 7) using estimated efficiencies, subsequent efficiency values from the appropriate efficiency maps and iteration until desired accuracy is obtained. The constants in the equations are then adjusted for final adjustments of the obtained curve, concentrating on the bottom end as the mechanical bypass is incorporated.

Table 2A is now compiled using ratio r, = 1.3/1.

Control Curves An accelerator potentiometer (Ap) contains 140 arbitrary units, 100 of which represent steadystate conditions. System pressure (åP2) is commanded by a function of Ap eq. (13) .-. pressure command APc = (Ap). As the latter is accomplished by modulating the throttle no engine power is commanded when åP3 2 P2 as the throttle will close in order to satisfy AP2 = APc.

Car speed is the result of n2C (ape) eq. (12) which modulates the motor m2 swash plate angle (62).

This results in @2 = 100% when n2 < n2c so that maximum torque is available on demand for acceleration.

In order to maintain optimum fuel efficiency engine speed n1 must be governed by m1 pressure difference AP4 and to that end there is provided n, [(APc - AP3)] eq. (14) (Figs. 2, 4, and 5) and Tables 1 and 2.

It would appear that 100% 82 during acceleration would make control difficult. This however is overcome by exaggerating mechanical throttle travel at the beginning. If v =10 ft/sec is demanded for example, 82 will obviously rapidly demodulate at this velocity is quickly satisfied.

If desired, the incorporation of an accelerometer sensitive to horizontal and vertical forces in a system capable of responding to the sum of acceleration and velocity components, so that a given accelerator demand is satisfied by speed and/or acceleration, is feasible.

Some Words on theAttachedAppendices 1) Appendix I deals to some considerable depth with the accumulator with the main object of justifying our particular approach. For example, cne can contend that the frequency of deceleration from more than about 44 ft/sec to zero is small and therefore negligible in terms of energy saved. It is desired additionally to explain our attitude to the polytropic exponent.

2) Appendix II deals with available modes of acceleration.

3) Appendix Ill describes the hydraulic pump/motor units.

Conclusions The advantages of this concept, as disclosed in the described embodiment, are manifest in the fact that drive input is at S2, both pressure and torque may be optimized and regenerated energy may be independent or in series with the prime mover output.

1) Any throttling approach to control acceleration during the re-use of regenerated energy, results in very high losses due to non-productive pressure drop over the throttling device, whereas, with S2 control, the main pressure drop is the working pressure.

2) It must be emphasized that optimum system pressure is not necessarily proportional to optimum engine torque for all steady-state conditions.

3! The series and/or independent, engine/accumulator arrangement permits torque summing, also the vehicle may be driven without running the engine.

It is estimated at this point that, based on a mixed urban-suburban-highway driving environment, mileage will exceed 70 MPG, which value also represents the highway cruise mileage expected. An interesting speculation is that urban driving mileage may, in tact, exceed highway mileage.

The foregoing estimate includes an adequate contingency to allow for car auxiliary power consumption and the simplified tretment of drag etc. in this study.

By reason of the control techniques developed, it is expected that one will achieve excellent drivability and flexibility.

APPENDIX I - Braking and Acceleration THE PNEUMATIC ACCUMULATOR 1. General The function of the pneumatic accumulator is to store energy during braking and to spend it subsequently for accelerating the car. This involves a considerable saving of energy and hence of fuel, especially in urban driving.

Here the question arises whether or not the compression of the accumulator gas can be regarded as an adiabatic process. Clearly, the adiabatic process is a limiting case (with no heat exchange at all).

The other limit is found by assuming that heat losses from the accumulator vessel to the environment are negligible (this can be ensure, if necessary, by thermal insulation) but that the vessel itself is always at the same temperature as the gas. Then the energy stored per pound of gas will be greater than that stored by adiabatic compression, due to the fact that - according to assumption -- the shell acts as a heat sink and stored additional energy which is recovered during expansion of the gas.

The real process is probably much closer to the adiabatic than to the other limit. For convenience, therefore regard the process as adiabatic. This will involve only a minor error and that on the safe side.

In the working pressure range, the accumulator gas (nitrogen) does not follow the ideal gas closely.

Exact results can be obtained by using a recently developed empirical equation of state. Formulae have been set up for pressure, internal energy, enthalpy and entropy as functions of density and temperature.

By means of these formulae, the energy stored per unit mass of gas is found as the difference of the internal energies at the beginning and the end of the process while the entropy remains constant.

Assuming an initial temperature T, = 700F = 294.44 K, an initial pressure P" = 3000 psia = 206.9 bar and final pressure P42 = 5000 psia = 344.83 bar, one finds the initial density p, = 14.01 [Ib/ft3] = 0.2245 [kg/lit] the final density P2 = 17.79 [Ib/ft3] = 0.285 [kg/lit] the final temperature r2 = 1 53.80F (341 K) the stored energy hE = 8518.4 [ft Ib/lb] = 25.47 (kJ/kg) 2. Accumulator Size The accumulator is assumed to be a spherical vessel of inside diameter D, provided with a bellows and fitted with compressed nitrogen gas. Its size is to be such that it can store the kinetic energy W of the car at a velocity of 44 [ft/s] = 30 mph (disregarding losses).This is often the speed limit in urban driving. On the open road, one seldom slows down from full speed to zero, so that the capacity of the accumulator will seldom be exceeded.

Then for a car weight of 2500 Ib one has W = 751 55.5 [ft/lb] = 101.94 kJ and the weight of the gas needed for storage will be wg = W/AE = 8.8227 Ib = 4 kg and its volume at pressure P" will be V, = 0.6292 ft3 = D37r/6. The thickness of the shell has to be ds = DP12/A@ where a is the acceptable stress of the material.If Ys is the specific weight of the shell material (Steel), the weight of the shell will be w = ysD27rds = 1.5V1ys P12/v = (1.5P 5P 12V/C#EP1W (15)l The weight of the hydraulic liquid that enters into the accumulator will be WL = (VLW/AE)(1/PI - 1/P2) (16) where the specific weight of the liquid is y, = 53 [1b/ft3] = 0.85 [kg/lit] = 0.85[g/cm3] Further y9 = 0.28[lb/in3] = 483.84 [Ib/ft3] = 7.75 [g/cm3] a = 50000 psi = 3448.3 bar So one finds the total weight of the accumulator W1 = W0 + Wl + WB = 8.82 + 7.08 + 45.7 = 61.6lb = 27.94 kg The volume of the hydraulic liquid in the accumulator is V,=0.13356 [ft3] =3.782 lit The total volume of the sphere is V, = 0.63 ft3 corresponding to an inside diameter D = 12.76 in = 32.41 cm If the sphere is replaced by two spheres having the same total volume and weight, their diameters will be 10.13 in = 25.72.

3. Regenerative and Friction Braking Normally, in the first part of the braking process the braking is purely regenerative. The hydraulic motor (driven by the road wheels) acts as a pump and presses liquid into the accumulator while liquid is sucked from the low-pressure container. So the accumulator pressure increases from an initial value P11 up to P, while the volume of the gas decreases from V, to V. Since there is a constant gear ratio between the hydraulic motor shaft and road wheels, we have V = V1 - Bs (17) where s is the distance traveled by the car during regenerative braking and the constant B has the dimension of an area. Evidently B = The motor swash plate is set at maximum displacement so that 82 = 1.

The energy differential that is stored in the accumulator will be -(P1-P5)dV=B(P1 -P5)ds=Fds where P5 is the low pressure level, F is the braking force and ij is the mechanical efficiency.of the hydraulic motor.

The dynamic equation for the vehicle is

where k, is the road resistance (including gear friction) and k2 is the drag factor.

Introducing the kinetic energy W = (w/2g)v2 and the constants k3 = 2k2gAv k4 = k1BP5/Z we can write eq. (18) in the form

This is a linear differential equation for W which can be solved by quadratures if P, is expressed as a function of s. This down by means of eq. (17) and a formulae P and S.

So the solution of eq. (18a) is

where W, is the initial kinetic energy.

The accumulator will be fully charged when the liquid volume V, has been pumped into it. The corresponding distance is = V#B = 152.23 ft = 46.4[m] The corresponding energy W2 is found from eq. (1 9). At this point, the pressure has reached its maximum acceptable value P1 From then on, the accumulator is inactive while the pressure is kept constant by liquid friction in RV2.

Using the conditions: for s = s2, W = W2, v - v2, t = t2, one finds for the liquid friction braking period closed formulae for W, v and t (time elapsed from the beginning of braking). Letting W =0 allows the total braking distance s3 to be calculated. The results are shown in Table 3.

The numerical data used were as follows: d2=3.15 [in3] r3=0.324074ft k, =45 lb k2 = 73.913 x 10 [lbs2/ft2] 71 = 0.9388 TI'=0.98 It will be noted that s2 (distance covered during regenerative braking) is independent of the initial velocity V1. Energy W2 and velocity v2 at this point, however, are dependent of vr and so are s3 and t3.

It has been assumed here that the initial velocity of the car has been large enough for the accumulator to be fruity charged by regenerative braking. The minimum initial velocity required for this is found by letting s = s2 and W = O in eq. (19). One finds limit = 46.5[ft/s] = 31.7 mph = 51 [km/h] If the initial velocity is less than vimin, the car will come to a standstill before the accumulator is fully charged. Under these circumstances, the braking is purely regenerative and the braking distance is, of course, dependent on v,. One finds it by trial and error from eq. (19). The braking time is found by numerical integration.

For emergency cases, dry friction brakes are available on all four wheels.

Table 3 is a brief summary of braking distances in the normal (regenerative plus liquid friction of purely regenerative) and emergency modes of braking. The road friction coefficient has been assumed to be 0.64.

Table 3 Braking Distances Mode Initial Velocity Braking Distance Normal 60 mph (96.54 km/h) 463.49ft(141.27 m) " 31.7 mph (51 km/h) 152.23 ft (46.4 m) Emergency 60 mph (96.54 km/h) 179.62 ft (54.75 m) 31.7mph (51 km/h) 50.78 ft (15.48m) APPENDIX II MODES OF MAXIMUM ACCELERATION 1. Acceleratlon by Engine Actlon The first mode of acceleration is by engine action alone. It is assumed that the accumulator is in the discharged condition. Acceleration of the vehicle from zero to cruising velocity is achieved in two stages. At first, the torque is limited by the maximum pressure acceptable in the hydraulic system.

Hence, the thrust force F' is constant and the engine power output increases with velocity, starting from zero. When the power output is equal to the full rated power of the engine, it remains constant while the thrust force decreases. This is the second stage of the acceleration process.

From the dynamic equation it follows dt = (w/g)dv/(F' - k1 - k2v2) (20) First stage: P2 = const = P,2 82 = 1 Then F' = const =T2/re = 11(P - P6@d2/s#r@ and from eq. (20) we find t = [w/2gy(F' - k1)]1 n[(1 + yv)/(1 - yv)] (21)

where

The power output of the engine is N, = 74 HP = 40700 [ft Ib/s] = n2d2s2#P2/So(##') (24) Then, since AP2 = P12 - P is known, n2 can be calculated for this transition point from eq. (24).

One finds n2 = 1537.66 rpm. The corresponding velocity is then v2 = 52.18 [ft/s] = 35.58 mph = 57.24 [km/h]. The corresponding time and distance are found from eqs (23) and (24); t2 =7.825 sec size 205.5 ft = 62.64[m] Beyond this point, the power output remains constant and therefore, according to eq. (24), the system pressure P2 must decrease with increasing n2. This is the second stage of the acceleration process. We have therefore, N2 = (1111')2N1 = 32560 [ft Ib/s] F' = N2/v Substituting this in (20) and satisfying the conditions: forv=v2 t=t2, S=s2 one finds for the second stage closed formulae for t and s as functions of v.

It will be noted that the denominator in (2) becomes zero for v = v00 = 1 51.57 [ft/s] = 103.34 mph = 166.28[km/h] This is the end velocity the vehicle considered here can attain if there is no speed limit, i.e. on a race track.

2. Acceleration by Simultaneous Accumulator and Engine Action If the accumulator is in the charged condition owing to previous regenerative braking, acceleration is accomplished by connecting the accumulator in series with the pump (cf. Fig. 2). This will ensure that the system pressure is always at its maximum acceptable value P12 = 5000 psia so that the maximum possible acceleration will be obtained. This is the second mode of acceleration.

This goes on until the accumulator is completely discharged. The distance covered up to that point is '2' = V1(2#en'/d2) = 146.2 ft = 44.56 [m]. From here on, acceleration is accomplished by engine action alone (Mode 1). Since s"2 < s'2" the engine power is sufficient to maintain maximum pressure and the pressure will decrease only beyond the transition point, i.e. for s < s'2.

So there is no difference in the acceleration behaviour of the car in Modes 1 and 2. Table 4 applies to both modes equally. However, as long as the accumulator is active (Mode 2), the engine has only to contribute the difference between accumulator pressure and maximum pressure and consequently very little energy and very little fuel are consumed until the accumulator is discharged.

Table 4 shows the length of time required for attaining velocities of 30, 50 and 60 mph both in Modes 1 and 2. The specification is easily met.

TABLE 1 Form of Equations Used for Table 2 and the Control Curves Dt = 45 + 0.005739P2 1 N2 = 0.00182PDt 2 T2=0.37 Dt 3 N1 = N1/#1#2#'1#'2 4 n1 = 480 - 2.75v + 0,15v 5 #P2 = 1062 - 3v + 0.165v 6 T1 = N1h/2#n1 7 #1 =T124##1/P2d1 8 # = n1d1#1#'1 9 n2 = 29.466P 10 #2 = ##'2/n2d2 11 n2c = 35.36A[ for 0 # Ap # 100 12 #Pc =1062- 3.6Ap + 0.2376Ap2 for 1 Ap 1 140 13 n1c = 0.8891(#P - #Pa - 500) or 1051 > (AP - #P3) # 5000 14 SEETABLE 2B FOR S1 UNTS EOUATION 1 2 3 4 5 6 7 8 9 10 11 v Dt N2 T2 N1 n1 #P2 T1 S1 # n2 @2 SFC MILEAGE 120 151.42 33.07 56.024 42.836 2310.0 3078.0 97.393 9.712 4988.7 3534.9 0.430 0.415 35.4 110 134.42 26.91 49.735 34.194 1992.5 2728.0 90.133 0.748 4525.7 3241.3 0.430 0.41 41.2 100 118.90 21.64 43.993 26.882 1705.0 2412.0 82.807 0.784 4067.2 2946.6 0.428 0.4 48.8 90 104.86 17.176 38.798 21.179 1447.5 2128.5 76.845 0.827 3650.1 2651.9 0.425 0.4 55.8 80 92.296 13.438 34.150 16.448 1220.0 1878.0 70.810 0.865 3219.7 2357.3 0.421 0.4 63.8 70 81.211 10.346 30.048 12.602 1022.5 1660.5 64.731 0.896 3801.5 2062.6 0.418 0.41 71.1 60 71.604 7.819 26.493 9.571 855.0 1476.0 58.790 0.916 3403.4 1768.0 0.418 0.415 79.3 50 63.475 5.776 23.486 7.247 717.5 1324.5 53.051 0.922 2028.2 1473.3 0.423 0.42 86.2 40 56.829 4.137 21.025 5.310 610.0 1206.0 45.722 0.867 1615.3 1178.6 0.420 0.45 94.1 30 51.651 2.820 18.11 3.810 532.5 1120.5 37.487 0.749 1205.7 884.0 0.416 0.48 90.0 20 47.956 1.746 17.744 2.605 485.0 1068.0 28.215 0.563 821.1 589.3 0.422 0.5 80.6 10 45.739 .832 16.718 1.387 467.0 1051.1 15.587 0.296 395.8 294.7 0.397 0.9 42.0 Fvs lb HP lb.ft HP RPM PSI lb.ft in /min RPM lb/8HPh mi/G TALE2-CAR OPRIMIZATION AND PERFORMANCE PARAMETERS SEETABLE 2C FOR SIUNITS v D1 N2 T2A T1A N1 n2A n1A SFC MILEAGE 120.951 151.416 33.069 66.244 82.824 33.743 1309.6 2095.3 0.4 46.68 110 134.419 26.911 58.808 73.527 27.460 1200.9 1920.7 0.4 58.58 100 118.900 21.640 52.019 65.038 22.081 1091.3 1746.1 0.4 59.44 90 104.858 17.176 45.876 57.358 17.526 982.2 1571.5 0.4 67.40 80 92.296 13.438 40.380 50.486 13.712 873.0 1396.9 0.4 76.57 70 82.211 10.346 35.530 44.422 10.557 763.9 1222.3 0.43 80.95 60 71.604 7.819 31.327 39.167 7.979 654.8 1047.6 0.51 77.41 50 63.47 5.776 27.770 34.720 5.894 545.7 873.0 0.58 76.79 40 56.824 4.137 24.860 31.083 4.221 436.5 688.4 0.64 77.73 fvs lb HP lb.ft lb.ft HP RPM RPM lb/BHPH mi/Ga TABLE 2A - CAR OPTIMIZATION AND PERFORMANCE PARAMETERS Equation 1 2 3 4 5 6 7 8 9 10 11 v v Dt N2 T2 N1 n1 #P2 T1 #1 # N2 #2 SFC MILEAGE 120 36.578 673.82 24.670 75.989 31.956 2310.1 212.28 132.100 0.712 81.750 3535.9 0.430 0.252 12.55 110 33.528 498.17 20.075 67.459 25.509 1992.5 188.14 122.253 0.748 74.163 3241.3 0.430 0.249 14.61 100 30.480 529.11 16.143 59.670 20.054 1705.0 166.34 112.316 0.784 66.649 2846.6 0.428 0.243 17.31 90 27.432 466.63 12.813 52.624 15.800 1447.5 146.79 104.229 0.827 59.814 2651.9 0.426 0.243 19.79 80 24.384 410.72 10.025 46.320 12.270 1220.0 129.52 96.044 0.865 52.761 2357.3 0.421 0.243 22.63 70 21.336 361.39 7.71B 40.756 9.401 1022,5 114.52 87.799 0.898 62.295 2062.6 0.418 0.249 25.22 60 18.288 318.64 5.833 35.934 7.140 855.0 101.79 79.740 0.916 55.772 1768.0 0.418 0.252 28.13 50 15.240 232.46 4.309 31.855 5.406 717.5 91.34 71.956 0.922 33.236 1473.3 0.423 0.255 30.58 40 12.192 252.89 3.086 28.517 3.961 610.0 83.17 62.015 0.867 26.470 1178.6 0.420 0.274 33.38 30 9.144 229.85 2.104 25.921 2.842 532.5 77.28 50.846 0.749 19.758 884.0 0.416 0.280 31.92 20 6.096 213.40 1.303 24.067 1.943 485.0 73.66 38.268 0.563 13.455 589.3 0.422 0.304 28.59 10 3.048 203.54 0.621 22.676 1.035 467.0 72.49 21.142 0.295 6.486 294.7 0.397 0.547 14.90 fvs m/s N kW Nm kW pm ber Nm lit/min cpm kg/kWli km/lit TABLE 2B - CAR OPTIMIZATION AND PERFORMANCE PARAMETERS (SI UNITS) Note: 1 bar = 10@ Pa # 1 at Fuel denslty 0.775 kg/lit v v Dt N2 T2A T1A N1 n2A n1A SFC MILEAGE 120.951 36.866 673.80 24.669 89.851 112.339 25.172 1309.6 2095.3 0.243 16.56 110 33.528 598.16 20.076 79.765 99.729 20.485 1200.9 1820.7 0.243 18.65 100 30.480 529.11 16.143 70.556 88.215 16.472 1091.3 1746.1 0.243 21.08 90 27.432 466.62 12.813 62.224 77.798 13.074 982.2 1571.5 0.243 23.91 80 24.384 410.72 10.025 54.770 68.477 10.229 873.9 1396.9 0.243 27.16 70 21.336 361.39 7.718 48.191 60.252 7.876 763.9 1222.3 0.261 28.71 60 18.288 318.64 5.833 42.491 53.125 5.952 654.8 1047.6 0.310 27.46 50 15.240 282.46 4.309 37.666 47.093 4.397 454.7 873.0 0.353 27.24 40 12.192 252.87 3.086 33.719 42.160 3.149 436.5 698.4 0.389 27.57 fv5 m/s N kW Nm Nm kW rpm rpm kg/kWh km/lit TABLE 2C - CAR OPTIMIZATION AND PERFORMANCE PARAMETERS (SIUNITS) TABLE 4 LENGTH OF TIME REQUIRED FOR ACCELERATION Acceleration to 30 mph 50 mph 60 mph 48.27 km/h 80.45 km/h 96.54km/h Mode 1 or 2 6.574 10.288 13.969 sec Specified 8 25 sec The described embodiment can be looked at from another angle since, as in the automobile, any device driven by an engine (particularly a spark ignition engine) that requires to be accelerated by power input and decelerated by braking, has three major areas on energy wastage. In order of magnitude they are: 1. Mis-matching of engine speed for any given steady state condition. i.e.: there is an optimum engine speed for any power output. Miles per gallon on the road or its equivalent may be reduced to 30% of the optimum by gross mis-matching of engine speed.

2. Particularly where rapid acceleration followed by rapid deceleration occurs frequently, as results in city driving of e.g. an automobile, a large proportion of the energy consumed by the vehicle is in the form of kinetic energy which is lost to the environment by applying friction brakes.

3. Losses are introduced also by the system which transmits power from engine to the ultimate driven device. (Transmission).

To improve energy utilization, a continuously variable speed ratio between engine and load is necessary together with a method of storing and re-using energy. The proper and efficient operation of this requires an appropriate control technique.

The system in the described embodiment will use hydraulic, pneumatic and electronic methods to demonstrate a unique flow and control system that satisfies efficiency aims and provides driver controlability.

The first area of loss mentioned is treated by introducing into a hydrostatic loop Fig. 3 a variable displacement pump and motor. Relative speed of input and output may be continuously varied by changing the displacement of either or both pump and motor. It should be emphasized now that increasing one unit and decreasing the other by the same amount will maintain the same input to output torque ratio but will increase or decrease system hydraulic pressure depending upon whether it is the pump or the motor that is increased. This arrangement therefore permits optimization of engine torque as well as, independently system pressure. This system uses the pump swash plate to determine engine speed n, and the motor swash plate to determine road velocity or the speed of the motor. Engine throttle controls system pressure.

The second area of loss is treated by introducing a vessel pressurized with gas (the accumulator) ACC and a second pressure vessel called the reservoir RES. Oil is driven from the reservoir to the accumulator by the motor when deceleration takes place. The accumulator is placed such that flow may pass, during re-use of energy via SV1 and CV1 to drive the motor and return oil to the reservoir via SV3; CV5 preventing communication of the high pressure with the low.During regeneration the motor swash plate regulates the flow of oil from the Reservoir viaR::V4, CV5 and CV2, SV1,2 and 3 being closed as a result of a closed accelerator operating the accelerator switch TS, also the brake switch BS ensures that the pump swash plate is at zero when the brake pedal operates the accelerator potentiometer AP, and SV1 prevents oil intended for the accumulator from passing through the bypass line at CV1. This is considered a unique arrangement that accomplishes the objectives while at the same time permitting re-use of regenerated energy most efficiently yet under driver control as no throttling valve is necessary in the oil path, acceleration rate being controlled by the swash plate angle only. It facilitates also the use of engine power simultaneously with accumulated energy.Note that it is important to use regenerated energy during acceleration in order to provide space for regeneration during the following deceleration cycle.

The third area of loss of energy, the transmission system itself. The losses in a hydraulic or similar electrical or pneumatic system are often greater than a simple mechanical system. Their advantage is that they can facilitate efficiencies at the engine that outweigh losses in the transmission; nevertheless the transmission should be optimized and this concept also affords a very convenient method of so doing. This is inherent in the fact mentioned above, that by adjusting both swash plates simultaneously engine and road wheel torque can be maintained while changing system pressure and flow. Thus hydraulic efficiency may be regulated without imparing engine or road wheel conditions.

This unique flow technique facilitates a unique control technique which in combination provides a unique overall system. Having decided to control: a) System pressure as a function of AP via the engine fuel input (throttle, etc.) b) Engine speed as a function of system pressure command minus accumulator pressure (APc - AP3) Fig. 3. The reason for subtracting åP3 is to facilitate combined engine and accumulator use when the engine would otherwise move off its optimum torque curve.

c) Motor or road wheel speed as a function of AP via the motor swash plate angle. This has the tendency to send S2 to maximum when the command speed is greater than actual speed making maximum road wheel torque available to the driver and returning it to optimum when n2C = n2.

An additional feed back intelligence is necessary to adjust for steady state operation with conditions other than level road, no wind and design car weight, this is accomplished by multiplying n1c (engine speed command) by a function of S2. This results in the torque or the engine following the optimum curve even under changing environment.

This system may be with or without a mechanical bypass. This is a direct mechanical drive which is automatically engaged and the hydraulic system switched out by three clutches. There is a steady state range where for a given set of vehicle parameters such a device iaof considerable fuel saving advantage. When this is included in the system a signal "B" from the n2 intelligence drives the direct throttle control conditioner BC1 putting direct throttle control at the operators disposal via C and sending other controls to zero. "B" is also taken to BC, the mechanical bypass signal conditioner that appropriatelv operates C, ClA and C2. Figure 3.

A reverse control RS causes the motor swash plate to move past centre reversing direction of the road wheels while permitting the engine and transmission to operate in the normal direction. A drive park control DPC is incorporated. This de-activates engine and pump control via AP allowing the driver by the hand throttle Th to start and control engine speed without powering the road wheels. An alternative claimed for this is to cause DPC to switch APc to "E" thence to a conditioner (similar to BC1) to control the throttle as a direct function of APc at C.

The emergency valve EV1 is to prevent violent discharge of stored energy should a system burst occur. It is operated by two flow meters (not shown) one at EV1 and one at the reservoir inlet. Should flow at the first position exceed that of the second by a predetermined amount EV1 cioses and must be manually re-opened.

Devices etc., named or suggested as alternatives etc., that are not described in detail are current state-of-the-art technology or can easily be devised by an expert.

Just as the invention of a single device will seek protection of tha idea of the relative arrangement of materials which produce a result or some aspect of uniqueness, this invention claims a unique arrangement of components electrical, electronic, hydraulic and mechanical etc.

The control logic may be expressed by three polynomials which may vary in degree etc. quite widely depending on chosen system characteristics, plus an additional feed back function from S2 viz:

1) n2 (Ap) 2) #P2 (Ap) # Figures 4 and 7 illustrete this 3) n10 (#P - #P2) 4) n1#2 % /x Also, satisfying continuity, three equations govern the power path viz:: 1) At the pump, energy = [(n1T1)] - 2) In the hydraulic circuit energy [(V0AP2)] 3) At the motor engine energy = [(n2T2)j In the described embodiment an example of our control system is given in which it so happens that we use the throttle to control the system pressure and we use the swash plate of the pump to control the engine speed. However, this procedure could be reversed -- in other words, the swash plate could be made to control the pressure and the engine throttle valve used to control the speed. This would work although it would make certain differences to the performance and it could be used as an alternative.The same argument could be applied to the whole system since we are dealing with aC equation and, as is well known, one can juggle parameters from one side of an equation to the other providing you obey the rules. Such rearrangement is, of course, envisaged as representing further embodiments of this invention.

Mathematical manipulation could still be carried out and different cars could result in certain modifications. However, the described embodiment describes a system which is actually controlling, in one case OR1 and, in the other case of 82; n2 of the road wheel speed is commanded and acuomplished by adjusting the rear swash plate. Of course, these parameters can be traded one to the other It will furthermore be appreciated that units such as the accumulator might be re-arranged but in the location shown in Figure 2 it seems to make the whole described system controllable and it allows one to go via the engine, summing engine torque and accumulator pressure, or by-passing through a bypass line which is one operation that indicates the position of the accumulator. The back wheels are driven directly. At the same time one obtains complete control in both modes, because of the rear swash plate control.

Variations of the described embodiments will readily occur to an expert skilled in the art, especially for gasoline engines or diesel engines. As will be clear above, instead of commanding road speed one can command the pressure (AP2c) by modulating the rear swash plate S2. It will be understood that the present invention is not restricted to the embodiments disclosed but the scope therefore is determined by the appended claims.

Claims (8)

1. A system for optimizing the operation of an engine for maximum output including.

a first device and a second device, each interconnected to control the engine speed in accordance with a function of at least one algebraic expression.

2. A system for optimizing the operation of an engine for maximum output according to claim 1 wherein said first device is a first swash plate device, and said second device is a second swash plate device, wherein each swash plate is connected in a hydraulic system to control the engine speed and at least one swash plate device is operable in accordance with a function of at least one algebraic expression.

3. A system according to claim 2 wherein the first swash plate is operable as a function of a first algebraic expression and the second swash plate is operable as a function of second algebraic expression.

4. A system according to claim 3 wherein the first algebraic expression is APc - APc and the second algebraic expression is Ap where AP = Pressure command function, AP3 = Accumulator pressure difference (P4P3), Ap = Throttle potentiometer setting, P3= Motor outlet pressure P4 Inlet pressure.

5. A system according to claim 4 wherein the first swash plate device is a pump and the second swash plate device is a motor.

6. A system according to claim 5 wherein the operation of the engine is controlled as a function of three equations which can be derived from a graphical representation of (a) n2C against Ap, (b) åPe against Ap, and (c) n1C against (APc - AP3) where n2C = Motor speed command function nrC Engine speed command function.

7. A system according to claim 6 wherein (a) the pump and motor are interconnected in said hydraulic system by a first and a second hydraulic line, (b) a first solenoid valve and a first check valve are provided in said second hydraulic line, (c) a second check valve is provided in a by-pass hydraulic line for said pump from said first hydraulic line to said second hydraulic line, (d) an accumulator unit is connected through a second solenoid valve to the junction of said first solenoid valve and said first check valve, and (e) a reservoir unit is connected through a third solenoid valve to the junction of said first check valve and said motor.

8. A system according to claim 1 wherein the operation of the engine is controlled as a function of three equations which can be derived from a graphical representation of (a) n2C against Ap, (b) APc against Ap, and (c) n1c against (APc 05a åP3) where AP = Pressure command function, AP3= Accumulator pressure difference (P4 P3), P3 = Motor outlet pressure P4= Inlet pressure n2C = Motor speed command function f(Ap) nrC = Engine speed command function f(Ap).