CN109094792A

CN109094792A - The application method of aircraft residual neat recovering system

Info

Publication number: CN109094792A
Application number: CN201810982494.6A
Authority: CN
Inventors: 叶丛杰
Original assignee: Individual
Current assignee: Individual
Priority date: 2018-08-27
Filing date: 2018-08-27
Publication date: 2018-12-28

Abstract

The invention discloses a kind of application methods of aircraft residual neat recovering system, the aircraft residual neat recovering system includes aircraft, the left and right ends of the aircraft are respectively provided with wing, launch device is equipped in the aircraft, the launch device front end is equipped with driving space, the launch device front end is connected by power dynamic bar, the power rail extends forward into the driving space, the configuration of the present invention is simple, manufacturing cost and maintenance cost are low, it can be realized the recycling of the waste heat to the tail gas of engine, improve the power of the model of an airplane, reduce the waste of fuel, meet the policy of energy-saving and emission-reduction, whole device operational safety is stablized, it is easy to operate, the service life of device is higher, low manufacture cost, and it is easy to operate.

Description

The application method of aircraft residual neat recovering system

Technical field

The present invention relates to model of an airplane fields, the specifically application method of aircraft residual neat recovering system.

Background technique

Currently, with the development of science and technology society development, people are also increasing to spiritual demand, like play model fly The people of machine is also more and more, and aircraft engine can generate the tail gas that high temperature is spent up to 700 more on startup, but so more Heat fails to be utilized carefully, is wasted in vain, so being badly in need of design, a to can use high-temperature tail gas secondary to carry out The model aircraft started.

Summary of the invention

Technical problem to be solved by the invention is to provide the application methods of aircraft residual neat recovering system, are able to solve State the problems of the prior art.

The present invention is achieved through the following technical solutions:

The present invention is a kind of application method of aircraft residual neat recovering system, which includes aircraft, described to fly The left and right ends of machine are respectively provided with wing, and launch device is equipped in the aircraft, and the launch device front end is equipped with driving space, institute It states launch device front end and is connected by power dynamic bar, the power rail extends forward into the driving space, the power The front end of bar, which is rotatably assorted, is connected with rocking bar, and the front end of the rocking bar, which is rotatably assorted, is connected with the first crankshaft, first crankshaft Left end be equipped with the tenth bevel gear, the right end of first crankshaft is equipped with the 5th bevel gear, and described first crankshaft or so extends point Not Guan Chuan the left and right ends wall in the driving space communicate with the outside world, first crankshaft is rotated by bearing and the aircraft matches Connection is closed, the left and right both ends of first crankshaft, which are respectively rotatably assorted, is connected with equirotal wheel, the left side in the driving space Upper end wall, which is equipped with, runs through slot, and described upwardly extend through slot is communicated with belt wheel space, and the right end wall through slot is equipped with liquid bar Space is pressed, liquid bar pressure space upper end is equipped with hydraulic cylinder, and the hydraulic cylinder lower end has been connected by power hydraulic stem, the hydraulic stem It extends down into liquid bar pressure space, the lower end in liquid bar pressure space extends into described in slot, institute to the left The left end for stating liquid bar pressure space is equipped with the second T connector, and described that telescopic shaft is equipped in slot, the lower end of the telescopic shaft, which is equipped with, to be used With the 9th bevel gear engaged with the tenth bevel gear, the outer ring of the telescopic shaft is equipped with to be cooperated with second T connector Second annular T slot, second T connector are inserted into the second annular T slot, second T connector and the second annular T slot Sliding connection, the upper end of the telescopic shaft are equipped with the inner cavity of opening upwards, and the left end wall of the inner cavity is equipped with keyway, institute It states and is equipped with the first Pulley shaft in the inner cavity of telescopic shaft, the lower-left end face of first Pulley shaft is equipped with sliding with the keyway The dynamic long key being cooperatively connected, first Pulley shaft and the telescopic shaft are slidably matched company by the long key and the keyway Connect, first Pulley shaft is rotatably assorted with the end wall through slot by bearing and is connect, first Pulley shaft to On extend into be rotatably assorted in the belt wheel space with the upper end wall in the belt wheel space and connect, first Pulley shaft exists Part in the belt wheel space is equipped with the first belt pulley, and the right side of first Pulley shaft is equipped with king bolt paddle shaft, described King bolt paddle shaft is rotatably assorted with two end walls up and down in the belt wheel space and connect, and the king bolt paddle shaft is equipped with and described the Opposite second belt pulley of one belt pulley, first belt pulley is connect with second belt pulley by belt, described The upper end wall that the belt wheel space is extended through in big propeller axial direction communicates with the outside world, and the top of the king bolt paddle shaft is equipped with Big propeller, the driving space have lower end wall to grab to be connected with long axis, and the upper end of the long axis is equipped with described the 6th bevel gear of five bevel gears engagement, the lower end wall that the long axis extends downwardly through the driving space enter the tail portion In space, the lower end of the long axis is equipped with third hand tap gear, and left hand end wall, which is rotatably assorted, in the trailing space is connected with wheel shaft, The right end of the wheel shaft is equipped with the 4th bevel gear engaged with the third hand tap gear, and described wheel shaft or so extends left and right respectively and passes through The left hand end wall for wearing the trailing space communicates with the outside world, and the left and right both ends of the wheel shaft are respectively equipped with identical with above-mentioned diameter Wheel, the aircraft are not additionally provided with hot-air engine device；

The application method are as follows: first start the launch device, thus in east after driving the power rail left front, thus described in driving Rocking bar back-and-forth motion is swung up and down, to drive first crank rotation, is linked on first crankshaft to drive Wheel rotation, first crank rotation drive the length to engage by the 5th bevel gear with the 6th bevel gear Axis rotation, to drive the third hand tap gear to rotate, to engage by the third hand tap gear with the 4th bevel gear The wheel shaft is driven to rotate, so that the wheel connected on the wheel shaft be driven to rotate, the rotation of first crankshaft is to pass through Tenth bevel gear drives the telescopic shaft to rotate with described engage, and the telescopic shaft rotation is to drive first belt Wheel shaft rotation, the first Pulley shaft rotation drives first pulley rotation, to drive described second by belt Pulley rotation, so that the king bolt paddle shaft is driven to rotate, so that the big propeller is driven to rotate, the launch device The first air cavity of tail gas heating, then indirect switchs the motor, so that intermittent drive the fan by the motor shaft Rotation, so that intermittent cool down to second air cavity, to drive described first by expanding with heat and contract with cold for the inert gas Sliding block and second sliding block move up and down, so that drive first bull stick moves up and down swing, to drive institute The second crank rotation is stated, to drive four second bevel gears rotations, to pass through the second bevel gear and described the The engagement of one bevel gear drives four first bevel gear axis rotations, to pass through the 7th bevel gear and the 8th cone tooth Wheel engagement drives the minor spiral paddle shaft rotation, to drive the small propeller to rotate, when the aircraft reaches certain speed It is that can take off, when needing to land, drives the hydraulic cylinder, the hydraulic stem is ramped up, to drives the telescopic shaft It ramps up, so that the 9th bevel gear is disengaged from the tenth bevel gear, then the aircraft just slowly declines.

The hot-air engine device includes first hot-gas system as a preferred technical solution, the launch device Left end is equipped with exhaust pipe, and the exhaust pipe is extended downwardly to be communicated with the heating pipe, and the heating pipe is to give institute State the heating of the first hot-gas system, the lower end of the heating pipe is mutually connected with outlet pipe, the outlet pipe extend downwardly again to Left extension communicates with the outside world, and the right end of first hot-gas system is equipped with the second hot-gas system, first hot-gas system Lower end sets power space, and the first air cavity is equipped in first hot-gas system, and first air cavity lower end is equipped with first communicated Sliding slot, the lower end of the first sliding groove are equipped with the first small chamber communicated, and the first small chamber extends downwardly and the power space It communicates, the first sliding block is slidably connected in the first sliding groove, the lower end surface of first sliding block is equipped with the first concave block, institute It states the first concave block and is inserted into described first small intracavitary, first concave block lower end surface is equipped with the inner cavity that Open Side Down, described The inner cavity of first concave block, which is rotatably assorted, is connected with the first short axle, and the inner cavity of first concave block is additionally provided with the first bull stick, and described One bull stick upper end is rotatably assorted with first short axle and connect, and the lower end of first bull stick extends in the power space, The second air cavity is equipped in second hot-gas system, the lower end of second air cavity is communicated equipped with second sliding slot, and described second is sliding The lower end of slot is communicated equipped with the second small chamber, and the second small chamber is extended downwardly to be communicated with the power space, second air cavity It is communicated with first air cavity by the tracheae, is slidably connected with the second sliding block in the second sliding slot, described second Sliding block lower end surface is equipped with the second concave block, and second concave block can find the described second small intracavitary, second concave block lower end surface Equipped with the inner cavity that Open Side Down, the inner cavity of second concave block, which is rotatably assorted, is connected with the second short axle, second concave block it is interior Chamber is additionally provided with the second bull stick, and second short axle is rotatably assorted with the upper end of second bull stick and connect, second bull stick to Under extend into the power space, the left side of second hot-gas system is equipped with cooling space, the cooling space position In the tracheae lower end and power space upper end, the left side of the cooling space is equipped with motor, and the motor right end is dynamic Power is connected with motor shaft, and the motor shaft is equipped with fan, the second crankshaft is equipped in the power space, and second crankshaft is left Right both ends are rotatably assorted with the left hand end wall in the power space and connect, and set that there are two angles as 107 on second crankshaft Ten degree of pars convoluta, the lower end of first bull stick and the pars convoluta of left end are rotatably assorted connection, the lower end of second bull stick and right The pars convoluta at end is rotatably assorted connection, and described second crankshaft or so extends the end wall of left and right two point for extending through the power space It Jin Ru not control in two wings, be set on each wing there are two the same wing space, second crankshaft passes through respectively It wears two wing spaces close to the wing to enter in the wing space far from the wing, second crankshaft Second bevel gear is equipped in each wing space, wing space lower end wall, which is rotatably assorted, is connected with first bevel gear Axis, first bevel gear axis upper end are equipped with the first bevel gear engaged with the second bevel gear, each wing space lower end Equipped with turbine mechanism, the turbine mechanism includes turbine space, and it is empty that the first bevel gear axis extends downwardly through the wing Between lower end wall enter the turbine space in, first bevel gear axis lower end be equipped with the 7th bevel gear, the turbine space Interior front and back end is equipped with the through slot that communicates with the outside world, is equipped with minor spiral paddle shaft in the turbine space, above and below the minor spiral paddle shaft Front and back is respectively symmetrically equipped with the identical l-shaped rod of size, and the front/rear end of the turbine space, which is respectively equipped with, to be open to described The first annular T slot of turbine space, the front end of four l-shaped rods are each extended over into the first annular T slot, Ge Gesuo The front end for stating l-shaped rod is respectively equipped with the first annular T head being slidably matched with the first annular T slot, in the minor spiral paddle shaft Between be equipped with the 8th bevel gear that engage with the 7th bevel gear, the front end of each minor spiral paddle shaft is equipped with small propeller.

5th bevel gear, the 6th bevel gear, the third hand tap gear and described as a preferred technical solution, The diameter of 4th bevel gear is identical, and the 9th bevel gear is identical as the tenth bevel gear diameter.

The first bevel gear, the second bevel gear, the 7th bevel gear and described as a preferred technical solution, 8th bevel gear diameter is identical, and the gas in first air cavity and second air cavity is inert gas.

The beneficial effects of the present invention are:

1. first starting the launch device, thus in east after driving power rail left front, so that rocking bar be driven to be moved forward and backward the upper bottom Dynamic, to drive the first crank rotation, to drive the wheel rotation being linked on the first crankshaft, the first crank rotation is to logical It crosses the 5th bevel gear and engages drive long axis rotation with the 6th bevel gear, to drive third hand tap gear to rotate, to pass through third Bevel gear engages with the 4th bevel gear drives wheel shaft rotation, so that the wheel connected on wheel shaft be driven to rotate, the first crankshaft turns It is dynamic to be rotated to pass through the tenth bevel gear with drive telescopic shaft rotation, telescopic shaft rotation is engaged to the first Pulley shaft of drive, The rotation of first Pulley shaft drives the first pulley rotation, so that the second pulley rotation is driven by belt, to drive big Propeller shaft rotation, so that big propeller be driven to rotate, the first air cavity of tail gas heating of launch device, then indirect switch is electric Machine, so that intermittent drive fan rotation by motor shaft, so that intermittent cool down to the second air cavity, to pass through inert gas Expand with heat and contract with cold the first sliding block of driving and the second sliding block moves up and down, so that first bull stick be driven to move up and down swing, To drive the second crank rotation, so that four second bevel gear rotations are driven, to pass through second bevel gear and the first cone tooth Wheel engagement drives four first bevel gear axis rotations, drives small propeller to engage by the 7th bevel gear with the 8th bevel gear Axis rotation is that can take off when aircraft reaches certain speed, to complete work of taking off so that small propeller be driven to rotate.

2. when needing to land, driving hydraulic cylinder ramps up hydraulic stem, so that telescopic shaft is driven to ramp up, so that the Nine bevel gears are disengaged from the tenth bevel gear, and then aircraft just slowly declines, to complete landing work.

3. the configuration of the present invention is simple, manufacturing cost and maintenance cost are low, can be realized to the waste heat of the tail gas of engine It recycles, improves the power of the model of an airplane, reduce the waste of fuel, meet the policy of energy-saving and emission-reduction, whole device operation Safety and stability, easy to operate, the service life of device is higher, low manufacture cost, and is easy to operate.

Detailed description of the invention

In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with It obtains other drawings based on these drawings.

Fig. 1 is the overall structure diagram of the application method of aircraft residual neat recovering system of the invention.

Fig. 2 is the structure left view of turbine apparatus in Fig. 1.

Fig. 3 is the structural schematic diagram in Fig. 1 at A.

Fig. 4 is the structural schematic diagram in Fig. 1 at B.

Specific embodiment

The preferred embodiment of the present invention is described in detail with reference to the accompanying drawing, so that advantages and features of the invention energy It is easier to be readily appreciated by one skilled in the art, so as to make a clearer definition of the protection scope of the present invention.

As shown in Figs 1-4, the present invention is a kind of application method of aircraft residual neat recovering system, the aircraft residual neat recovering system Including aircraft 100, the left and right ends of the aircraft 100 are respectively provided with wing 30, are equipped with launch device 23, institute in the aircraft 100 It states 23 front end of launch device and is equipped with driving space 62,23 front end of launch device is connected by power dynamic bar 93, the power Bar 93 extends forward into the driving space 62, and the front end of the power rail 93, which is rotatably assorted, is connected with rocking bar 61, described The front end of rocking bar 61, which is rotatably assorted, is connected with the first crankshaft 60, and the left end of first crankshaft 60 is equipped with the tenth bevel gear 59, institute The right end for stating the first crankshaft 60 is equipped with the 5th bevel gear 26, and the extension of the first crankshaft 60 or so extends through the driving space 62 left and right ends wall communicates with the outside world, and first crankshaft 60 is rotatably assorted with the aircraft 100 by bearing and is connect, described The left and right both ends of first crankshaft 60, which are respectively rotatably assorted, is connected with equirotal wheel, and the upper left end wall in the driving space 62 is set Have through slot 22, described upwardly extend through slot 22 is communicated with belt wheel space 50, and the right end wall through slot 22 is equipped with liquid bar Space 63 is pressed, the liquid bar pressure 63 upper end of space is equipped with hydraulic cylinder 66, and 66 lower end of hydraulic cylinder has been connected by power hydraulic stem 65, The hydraulic stem 65 extends down into liquid bar pressure space 63, and the lower end in liquid bar pressure space 63 extends into the left Described to run through in slot 22, the left end in liquid bar pressure space 63 is equipped with the second T connector 64, described interior equipped with telescopic shaft through slot 22 57, the lower end of the telescopic shaft 57 is equipped with the 9th bevel gear 58 to engage with the tenth bevel gear 59, the telescopic shaft 57 outer ring is equipped with the second annular T slot 56 cooperated with second T connector 64, and second T connector 64 is inserted into described second In annular T slot 56, second T connector 64 is slidably connected with the second annular T slot 56, the upper end of the telescopic shaft 57 Inner cavity equipped with opening upwards, the left end wall of the inner cavity are equipped with keyway 55, are equipped with first in the inner cavity of the telescopic shaft 57 Pulley shaft 52, the lower-left end face of first Pulley shaft 52 are equipped with the long key being slidably connected with the keyway 55 54, first Pulley shaft 52 is slidably connected by the long key 54 with the keyway 55 with the telescopic shaft 57, institute State the first Pulley shaft 52 and be rotatably assorted by bearing with the end wall through slot 22 and is connect, first Pulley shaft 52 to On extend into the belt wheel space 50 to be rotatably assorted with the upper end wall in the belt wheel space 50 and connect, first belt pulley Part of the axis 52 in the belt wheel space 50 is equipped with the first belt pulley 53, and the right side of first Pulley shaft 52 is equipped with big spiral shell Paddle shaft 20 is revolved, the king bolt paddle shaft 20 is rotatably assorted with two end walls up and down in the belt wheel space 50 and connect, the king bolt Paddle shaft 20 is equipped with second belt pulley 51 opposite with first belt pulley 53, first belt pulley 53 and described the Two belt pulleys 51 are connected by belt, and the king bolt paddle shaft 20 is upwardly extended through the upper end wall in the belt wheel space 50 and outer Boundary communicates, and the top of the king bolt paddle shaft 20 is equipped with big propeller 21, and the driving space 62 has lower end wall to grab cooperation It is connected with long axis 29, the upper end of the long axis 29 is equipped with the 6th bevel gear 27 engaged with the 5th bevel gear 26, the length The lower end wall that axis 29 extends downwardly through the driving space 62 enters in the trailing space 31, and the lower end of the long axis 29 is set There is third hand tap gear 32, left hand end wall, which is rotatably assorted, in the trailing space 31 is connected with wheel shaft 34, the right end of the wheel shaft 34 Equipped with the 4th bevel gear 33 engaged with the third hand tap gear 32, the wheel shaft 34 or so extends left and right respectively and runs through the tail The left hand end wall in portion space 31 communicates with the outside world, and the left and right both ends of the wheel shaft 34 are respectively equipped with wheel identical with above-mentioned diameter Son, the aircraft 100 are not additionally provided with hot-air engine device；

The application method are as follows: first start the launch device 23, thus in east after driving the power rail 93 left front, to drive The back-and-forth motion of rocking bar 61 is swung up and down, so that first crankshaft 60 be driven to rotate, is linked at described first to drive Wheel rotation on crankshaft 60, the rotation of the first crankshaft 60 is to pass through the 5th bevel gear 26 and the 6th bevel gear 27 engagements drive the long axis 29 to rotate, to drive the third hand tap gear 32 to rotate, to pass through the third hand tap gear 32, which engage the drive wheel shaft 34 with the 4th bevel gear 33, rotates, so that the wheel connected on the wheel shaft 34 be driven to turn Dynamic, the rotation of first crankshaft 60 drives described 57 turns of telescopic shaft to engage by the tenth bevel gear 59 with described 68 Dynamic, to drive first Pulley shaft 52 to rotate, the rotation of the first Pulley shaft 52 is driven for the rotation of telescopic shaft 57 First belt pulley 53 rotates, to drive second belt pulley 51 to rotate by belt, to drive the king bolt Paddle shaft 20 rotates, so that the big propeller 21 is driven to rotate, the first air cavity of tail gas heating 94 of the launch device 23, and then Indirect switchs the motor 92, so that intermittent drive the fan 90 to rotate by the motor shaft 91, thus intermittent Second air cavity 81 cooling is given, to drive first sliding block 77 and described the by expanding with heat and contract with cold for the inert gas Two sliding blocks 83 move up and down, so that drive first bull stick 72 moves up and down swing, to drive described second bent Axis 71 rotates, to drive four second bevel gears 37 to rotate, to pass through the second bevel gear 37 and described first The engagement of bevel gear 36 drives four first bevel gear axis 38 to rotate, to pass through the 7th bevel gear 47 and the described 8th The engagement of bevel gear 46 drives the minor spiral paddle shaft 45 to rotate, to drive the small propeller 44 to rotate, when the aircraft 100 Reaching certain speed is that can take off, and when needing to land, drives the hydraulic cylinder 66, the hydraulic stem 65 is ramped up, from And the telescopic shaft 57 is driven to ramp up, so that the 9th bevel gear 58 is disengaged from the tenth bevel gear 59, then The aircraft 100 just slowly declines.

Wherein, the hot-air engine device includes first hot-gas system 79, and the left end of the launch device 23 is equipped with row Feed channel 24, the exhaust pipe 24 is extended downwardly to be communicated with the heating pipe 78, and the heating pipe 78 is to described The heating of first hot-gas system 79, the lower end of the heating pipe 78 are mutually connected with outlet pipe 25, and the outlet pipe 25 is to downward It stretches to extend to the left again and communicate with the outside world, the right end of first hot-gas system 79 is equipped with the second hot-gas system 82, and described first The lower end of hot-gas system 79 sets power space 70, is equipped with the first air cavity 94, first air cavity in first hot-gas system 79 94 lower ends are equipped with the first sliding groove 76 that communicates, and the lower end of the first sliding groove 76 is equipped with the first small chamber 75 communicated, and described first Small chamber 75 is extended downwardly to be communicated with the power space 70, and the first sliding block 77 is slidably connected in the first sliding groove 76, The lower end surface of first sliding block 77 is equipped with the first concave block 73, and first concave block 73 is inserted into the described first small chamber 75 Interior, 73 lower end surface of the first concave block is equipped with the inner cavity that Open Side Down, and the inner cavity of first concave block 73, which is rotatably assorted, to be connected with First short axle 74, the inner cavity of first concave block 73 are additionally provided with the first bull stick 72,72 upper end of the first bull stick and described first Short axle 74 is rotatably assorted connection, and the lower end of first bull stick 72 extends in the power space 70, the second hot gas dress It sets and is equipped with the second air cavity 81 in 82, the lower end of second air cavity 81 is communicated equipped with second sliding slot 87, the second sliding slot 87 Lower end is communicated equipped with the second small chamber 88, and the second small chamber 88 is extended downwardly to be communicated with the power space 70, second gas Chamber 81 is communicated with first air cavity 94 by the tracheae 80, is slidably connected with the second sliding block in the second sliding slot 87 83,83 lower end surface of the second sliding block is equipped with the second concave block 84, and second concave block 84 can be found in the described second small chamber 88, Second concave block, 84 lower end surface is equipped with the inner cavity that Open Side Down, and the inner cavity of second concave block 84, which is rotatably assorted, is connected with second Short axle 85, the inner cavity of second concave block 84 are additionally provided with the second bull stick 86, second short axle 85 and second bull stick 86 Upper end is rotatably assorted connection, and second bull stick 86 extends down into the power space 70, second hot-gas system 82 left side is equipped with cooling space 89, and the cooling space 89 is located on 80 lower end of tracheae and the power space 70 The left side at end, the cooling space 89 is equipped with motor 92, and 92 right end of motor has been connected by power motor shaft 91, the motor Axis 91 is equipped with fan 90, is equipped with the second crankshaft 71 in the power space 70,71 left and right ends of the second crankshaft with it is described The left hand end wall in power space 70 is rotatably assorted connection, sets that there are two angles as 170 degree of song on second crankshaft 71 Portion, the lower end of first bull stick 72 and the pars convoluta of left end are rotatably assorted connection, the lower end of second bull stick 86 and right end Pars convoluta is rotatably assorted connection, and second crankshaft 71 or so extends the end wall of left and right two point for extending through the power space 70 It Jin Ru not be set on each wing 30 there are two the same wing space 35, second crankshaft in two wings 30 in left and right 71, which extend through two wing spaces 35 close to the wing 30, enters the wing space far from the wing 30 In 35, second crankshaft 71 is equipped with second bevel gear 37,35 lower end of wing space in each wing space 35 Wall, which is rotatably assorted, is connected with first bevel gear axis 38, and 38 upper end of first bevel gear axis is equipped with and nibbles with the second bevel gear 37 The first bevel gear 36 of conjunction, each 35 lower end of wing space are equipped with turbine mechanism, and the turbine mechanism includes turbine space 39, institute It states first bevel gear axis 38 and extends downwardly through the lower end wall in the wing space 35 and enter in the turbine space 39, described the One bevel gear shaft, 38 lower end is equipped with the 7th bevel gear 47, and front and back end is equipped with the through slot communicated with the outside world in the turbine space 39 43, the turbine space 39 is interior to be equipped with minor spiral paddle shaft 45, and about 45 front and back of minor spiral paddle shaft is respectively symmetrically equipped with size The identical l-shaped rod 40 of size, the front/rear end of the turbine space 39 are respectively equipped with opening to the first of the turbine space 39 Annular T slot 41, the front end of four l-shaped rods 40 are each extended over into the first annular T slot 41, each l-shaped rod 40 front end is respectively equipped with the first annular T head 42 being slidably matched with the first annular T slot 41, in the minor spiral paddle shaft 45 Between be equipped with the 8th bevel gear 46 that engage with the 7th bevel gear 47, the front end of each minor spiral paddle shaft 45 is equipped with small spiral shell Revolve paddle 44.

Wherein, the 5th bevel gear 26, the 6th bevel gear 27, the third hand tap gear 32 and the 4th cone tooth The diameter of wheel 33 is identical, and the 9th bevel gear 58 is identical as 59 diameter of the tenth bevel gear.

Wherein, the first bevel gear 36, the second bevel gear 37, the 7th bevel gear 47 and the 8th cone tooth Take turns that 46 diameters are identical, first air cavity 94 is inert gas with the gas in second air cavity 81.

The beneficial effects of the present invention are:

The basic principles, main features and advantages of the present invention have been shown and described above.The technology of the industry Personnel are it should be appreciated that the present invention is not limited to the above embodiments, and the above embodiments and description only describe this The principle of invention, various changes and improvements may be made to the invention without departing from the spirit and scope of the present invention, these changes Change and improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention by appended claims and its Equivalent defines.

Claims

1. a kind of application method of aircraft residual neat recovering system, which includes aircraft, a left side for the aircraft Right both ends are respectively provided with wing, launch device are equipped in the aircraft, the launch device front end is equipped with driving space, described to start Device front end is connected by power dynamic bar, and the power rail extends forward into the driving space, before the power rail End, which is rotatably assorted, is connected with rocking bar, and the front end of the rocking bar, which is rotatably assorted, is connected with the first crankshaft, the left end of first crankshaft Equipped with the tenth bevel gear, the right end of first crankshaft is equipped with the 5th bevel gear, and described first crankshaft or so extension extends through The left and right ends wall in the driving space communicates with the outside world, and first crankshaft is rotatably assorted company by bearing and the aircraft It connects, the left and right both ends of first crankshaft, which are respectively rotatably assorted, is connected with equirotal wheel, the left upper end in the driving space Wall, which is equipped with, runs through slot, and described upwardly extend through slot is communicated with belt wheel space, and it is empty that the right end wall through slot is equipped with liquid bar pressure Between, liquid bar pressure space upper end is equipped with hydraulic cylinder, and the hydraulic cylinder lower end has been connected by power hydraulic stem, and the hydraulic stem is downward It extends into liquid bar pressure space, the lower end in liquid bar pressure space extends into described in slot, the liquid to the left Bar presses the left end in space to be equipped with the second T connector, described to be equipped with telescopic shaft in the slot, the lower end of the telescopic shaft be equipped with to 9th bevel gear of the tenth bevel gear engagement, the outer ring of the telescopic shaft are equipped with cooperate with second T connector second Annular T slot, second T connector are inserted into the second annular T slot, and second T connector and the second annular T slot slide It is cooperatively connected, the upper end of the telescopic shaft is equipped with the inner cavity of opening upwards, and the left end wall of the inner cavity is equipped with keyway, described to stretch The first Pulley shaft is equipped in the inner cavity of contracting axis, the lower-left end face of first Pulley shaft is equipped with matches with keyway sliding The long key of connection, first Pulley shaft and the telescopic shaft is closed to be slidably connected by the long key and the keyway, First Pulley shaft is rotatably assorted with the end wall through slot by bearing and is connect, and first Pulley shaft prolongs upwards It extends into be rotatably assorted in the belt wheel space with the upper end wall in the belt wheel space and connect, first Pulley shaft is described Part in belt wheel space is equipped with the first belt pulley, and the right side of first Pulley shaft is equipped with king bolt paddle shaft, the big spiral shell Rotation paddle shaft is rotatably assorted with two end walls up and down in the belt wheel space to be connect, and the king bolt paddle shaft is equipped with and first skin Opposite second belt pulley of belt wheel, first belt pulley are connect with second belt pulley by belt, the big spiral shell The upper end wall that rotation paddle shaft is upwardly extended through the belt wheel space communicates with the outside world, and the top of the king bolt paddle shaft is equipped with big spiral shell Paddle is revolved, the driving space has lower end wall to grab to be connected with long axis, and the upper end of the long axis is equipped with and the described 5th bores 6th bevel gear of gear engagement, the lower end wall that the long axis extends downwardly through the driving space enter the trailing space Interior, the lower end of the long axis is equipped with third hand tap gear, and left hand end wall, which is rotatably assorted, in the trailing space is connected with wheel shaft, described The right end of wheel shaft is equipped with the 4th bevel gear engaged with the third hand tap gear, and described wheel shaft or so extends left and right respectively and runs through institute The left hand end wall for stating trailing space communicates with the outside world, and the left and right both ends of the wheel shaft are respectively equipped with wheel identical with above-mentioned diameter Son, the aircraft are not additionally provided with hot-air engine device；

2. the application method of aircraft residual neat recovering system according to claim 1, it is characterised in that: the hot-air engine device Including first hot-gas system, the left end of the launch device is equipped with exhaust pipe, and the exhaust pipe extends downwardly and institute It states heating pipe to communicate, to heat to first hot-gas system, the lower end of the heating pipe communicates the heating pipe There is outlet pipe, the outlet pipe is extended downwardly to extend to the left again and be communicated with the outside world, the right end of first hot-gas system Equipped with the second hot-gas system, the lower end of first hot-gas system sets power space, is equipped with first in first hot-gas system Air cavity, first air cavity lower end are equipped with the first sliding groove communicated, and the lower end of the first sliding groove is equipped with the first small chamber communicated, The first small chamber is extended downwardly to be communicated with the power space, and the first sliding block is slidably connected in the first sliding groove, The lower end surface of first sliding block is equipped with the first concave block, first concave block be inserted into it is described first small intracavitary, described the One concave block lower end surface is equipped with the inner cavity that Open Side Down, and the inner cavity of first concave block, which is rotatably assorted, is connected with the first short axle, described The inner cavity of first concave block is additionally provided with the first bull stick, and first bull stick upper end is rotatably assorted with first short axle and connect, described The lower end of first bull stick extends in the power space, and the second air cavity, second gas are equipped in second hot-gas system The lower end of chamber is communicated equipped with second sliding slot, and the lower end of the second sliding slot is communicated equipped with the second small chamber, and the second small chamber is downward Extension is communicated with the power space, and second air cavity is communicated with first air cavity by the tracheae, and described second is sliding The second sliding block is slidably connected in slot, second sliding block lower end surface is equipped with the second concave block, and second concave block can be looked into Small intracavitary to described second, second concave block lower end surface is equipped with the inner cavity that Open Side Down, the inner cavity rotation of second concave block Be connected with the second short axle, the inner cavity of second concave block is additionally provided with the second bull stick, second short axle with described second turn The upper end of bar is rotatably assorted connection, and second bull stick extends down into the power space, second hot-gas system Left side be equipped with cooling space, the cooling space is located at the tracheae lower end and power space upper end, the cooling The left side in space is equipped with motor, and the motor right end has been connected by power motor shaft, and the motor shaft is equipped with fan, described dynamic It is equipped with the second crankshaft in power space, the left hand end wall in second crankshaft left and right ends and the power space is rotatably assorted company It connects, sets that there are two angles on second crankshaft as 170 degree of pars convoluta, the lower end of first bull stick and the song of left end Portion is rotatably assorted connection, and the lower end of second bull stick and the pars convoluta of right end are rotatably assorted connection, and described second crankshaft or so prolongs Stretch extend through the power space the end wall of left and right two respectively enter left and right two wings in, each wing is equipped with Wing space as two, the wing space that second crankshaft extends through two close wings enter separate In the wing space of the wing, second crankshaft is equipped with second bevel gear in each wing space, described Wing space lower end wall, which is rotatably assorted, is connected with first bevel gear axis, and first bevel gear axis upper end is equipped with and second cone The first bevel gear of gear engagement, each wing space lower end are equipped with turbine mechanism, and the turbine mechanism includes turbine space, institute State first bevel gear axis extend downwardly through the wing space lower end wall enter the turbine space in, it is described first cone tooth Wheel shaft lower end is equipped with the 7th bevel gear, and front and back end is equipped with the through slot communicated with the outside world, the turbine space in the turbine space Interior to be equipped with minor spiral paddle shaft, front and back is respectively symmetrically equipped with the identical l-shaped rod of size, the whirlpool to the minor spiral paddle shaft up and down The front/rear end in wheel space is respectively equipped with first annular T slot of the opening to the turbine space, the front end point of four l-shaped rods It does not extend into the first annular T slot, the front end of each l-shaped rod is respectively equipped with to be slided with the first annular T slot The first annular T head of cooperation, the minor spiral paddle shaft centre is equipped with the 8th bevel gear engaged with the 7th bevel gear, each The front end of the minor spiral paddle shaft is equipped with small propeller.

3. the application method of aircraft residual neat recovering system according to claim 1, it is characterised in that: the 5th cone tooth Wheel, the 6th bevel gear, the third hand tap gear are identical with the diameter of the 4th bevel gear, the 9th bevel gear and institute It is identical to state the tenth bevel gear diameter.

4. the application method of aircraft residual neat recovering system according to claim 1, it is characterised in that: the first cone tooth Wheel, the second bevel gear, the 7th bevel gear are identical with the 8th bevel gear diameter, first air cavity and described the Gas in two air cavitys is inert gas.