CA1115012A - Apparatus for cleaning jet engine nozzles - Google Patents
Apparatus for cleaning jet engine nozzlesInfo
- Publication number
- CA1115012A CA1115012A CA370,569A CA370569A CA1115012A CA 1115012 A CA1115012 A CA 1115012A CA 370569 A CA370569 A CA 370569A CA 1115012 A CA1115012 A CA 1115012A
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- CA
- Canada
- Prior art keywords
- outlet
- jet engine
- valve
- fuel
- nozzles
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
APPARATUS FOR CLEANING JET ENGINE NOZZLES
ABSTRACT OF THE DISCLOSURE
An apparatus and process is provided for cleaning residue fuel varnish and carbon from the fuel nozzles and guide vanes of a jet engine. The apparatus is constructed to dispense a detergent and water solution under sufficient pressure through the nozzles themselves to scrub residue fuel varnish and carbon from the fuel nozzles and from the guide vanes of a jet engine of an aircraft without the need for removing the same from the engine. In its operation, the apparatus serves to wet down the surfaces of the nozzles and guide vanes with a detergent solution for a period of, time (i.e. about twenty minutes), then to scour the surfaces with a pulsating detergent spray, and finally to purge the surfaces with a pressurized air stream. The apparatus is conveniently mounted on a vehicle, so that it can be moved to the work site.
ABSTRACT OF THE DISCLOSURE
An apparatus and process is provided for cleaning residue fuel varnish and carbon from the fuel nozzles and guide vanes of a jet engine. The apparatus is constructed to dispense a detergent and water solution under sufficient pressure through the nozzles themselves to scrub residue fuel varnish and carbon from the fuel nozzles and from the guide vanes of a jet engine of an aircraft without the need for removing the same from the engine. In its operation, the apparatus serves to wet down the surfaces of the nozzles and guide vanes with a detergent solution for a period of, time (i.e. about twenty minutes), then to scour the surfaces with a pulsating detergent spray, and finally to purge the surfaces with a pressurized air stream. The apparatus is conveniently mounted on a vehicle, so that it can be moved to the work site.
Description
APPARATUS FOR Cl,EANING JET ENGIME NOZZLES
BACKGROUND OF THE INVENTION
This application is a division of Canadian Serial No. 309,224, filed August 14, 197~.
It has been the usual practice during overhaul to xemove the fuel nozzles and guide vanes from the jet engines of an aircraft, and to soak the parts in an appropriate solution so as to remove the residue fuel varnish and carbon Erom the surfaces thereof. However, such a procedure is time consuming and costly.
The apparatus and process of the present invention serves to cause a high pressure spray of water and detergent solution to be emitted from the fuel nozzles of the jet - engine with the nozzles and guide vanes in place in the engine, in order to clean the nozzles and guide vanes thoroughly with-out the need to dismantle the same from the engine.
As mentioned above, the apparatus to be described may conveniencly be mounted in a vehicle to be transported to the work site. A feature of the apparatus in the embodiment to be 20 described is that it incorporates pneumatic logic modules which ~ -operate compIetely without electricity so as to be operable ~`
in any atmosphere without any danger of explosion and thereby to be safe for hangar use.
"` .' Thus, the invention can be defined as an apparatus for cleaning residue fuel varnish and carbon from the fuel nozzles ` and guide vanes of a jet engine which includes an inlet for - receiving compressed air, an outlet configured to be coupled . ::
,' ~ ~'' --1-- . ..
. - ~
into the fuel system of a jet engine so that the fluid emitted by the outlet may be discharged through the fuel nozzles of the jet engine to perform a cleaning function, and pneumatically operated control means for causing a pressurized stream of a cleaning solution to be emitted through the outlet.
In a further embodiment the aforesaid pneumatically controlled control means includes automatic sequencing timer means for causing a first stream of cleaning solution to be emitted through the outlet at relatively low pressure and for a predetermined time interval for wetting purposes, and for subsequently causing a second stream of cleaning solution to be emitted through the outlet at relatively high pressure and as intermittent bursts.
In a Eurther embodiment, the invention contemplates an apparatu~ for cleaning residue fuel varnish and carbon from the fuel nozzles and guide vanes of a jet engine, which includes an inlet for receiving compressed air, an outlet configured to be coupled into the fuel system of a jet engine so that fluid emitted by the outlet may be discharged through the fuel nozzles of the jet engine to perform a cleaning function, and air reseiver means. A first compressed air operated pump means is coupled to the inlet for introducing compressed air into the air receiver means so as to achieve a predetermined air pressure in the air receiver means, and a first liquid accumulator means is coupled to the air receiver means. A reser-voir is provided for a cleaning solution, and a second compressed air operated pump means is coupled to the inlet and to the .:
reservoir and to the first liquid accumulator means for intro-ducing cleaning solution from the reservoir into the first liquid accumulator means against the pressure of compressed air from the air receiver means. A first conduit means couples the first liquid accumulator to the outlet, and a first valve
BACKGROUND OF THE INVENTION
This application is a division of Canadian Serial No. 309,224, filed August 14, 197~.
It has been the usual practice during overhaul to xemove the fuel nozzles and guide vanes from the jet engines of an aircraft, and to soak the parts in an appropriate solution so as to remove the residue fuel varnish and carbon Erom the surfaces thereof. However, such a procedure is time consuming and costly.
The apparatus and process of the present invention serves to cause a high pressure spray of water and detergent solution to be emitted from the fuel nozzles of the jet - engine with the nozzles and guide vanes in place in the engine, in order to clean the nozzles and guide vanes thoroughly with-out the need to dismantle the same from the engine.
As mentioned above, the apparatus to be described may conveniencly be mounted in a vehicle to be transported to the work site. A feature of the apparatus in the embodiment to be 20 described is that it incorporates pneumatic logic modules which ~ -operate compIetely without electricity so as to be operable ~`
in any atmosphere without any danger of explosion and thereby to be safe for hangar use.
"` .' Thus, the invention can be defined as an apparatus for cleaning residue fuel varnish and carbon from the fuel nozzles ` and guide vanes of a jet engine which includes an inlet for - receiving compressed air, an outlet configured to be coupled . ::
,' ~ ~'' --1-- . ..
. - ~
into the fuel system of a jet engine so that the fluid emitted by the outlet may be discharged through the fuel nozzles of the jet engine to perform a cleaning function, and pneumatically operated control means for causing a pressurized stream of a cleaning solution to be emitted through the outlet.
In a further embodiment the aforesaid pneumatically controlled control means includes automatic sequencing timer means for causing a first stream of cleaning solution to be emitted through the outlet at relatively low pressure and for a predetermined time interval for wetting purposes, and for subsequently causing a second stream of cleaning solution to be emitted through the outlet at relatively high pressure and as intermittent bursts.
In a Eurther embodiment, the invention contemplates an apparatu~ for cleaning residue fuel varnish and carbon from the fuel nozzles and guide vanes of a jet engine, which includes an inlet for receiving compressed air, an outlet configured to be coupled into the fuel system of a jet engine so that fluid emitted by the outlet may be discharged through the fuel nozzles of the jet engine to perform a cleaning function, and air reseiver means. A first compressed air operated pump means is coupled to the inlet for introducing compressed air into the air receiver means so as to achieve a predetermined air pressure in the air receiver means, and a first liquid accumulator means is coupled to the air receiver means. A reser-voir is provided for a cleaning solution, and a second compressed air operated pump means is coupled to the inlet and to the .:
reservoir and to the first liquid accumulator means for intro-ducing cleaning solution from the reservoir into the first liquid accumulator means against the pressure of compressed air from the air receiver means. A first conduit means couples the first liquid accumulator to the outlet, and a first valve
-2-is included in the first conduit means. A control means coupled to the first valve controls the flow of the cleaning solution through the fixst conduit means from the first liquid accumu-lator means to the outlet.
The invention also contemplates a process for cleaning - the fuel nozzles and guide vanes of jet engines which comprises disconnecting the fuel system of the engine from the fuel nozzles. A first step initially introduces a pressurized stream of cleaning solution at relatively low pressure into the fuel nozzles for wetting purposes, and a second step after a pre-determined time interval subsequently introduces the stream of cleaning solution at relatively high pressure into the fuel no~zles to be emitted through the fuel nozzles.
BRIEF DESCRIPTION OF THE DRAWINGS
FIGURES lA and lB are pictorial representations of apparatus constructed in accordance with the invention; and FIGURE 2 is a schematic functional diagram o the apparatus.
DETAILED DESCRIPTION OF THE ILLUSTRATED EMBODIMENT
As shown in FIGURES lA and lB, the apparatus of the . ~
invention may be mounted on a three-wheeled cart 10 which may be towed to the work site by a handle 12.
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~ -3-In the schematic diagram of FIGU~E 2 f compressed air of a pressure, for example, of 100 psi is in~roduced through an inlet "I", and through a 3-way air supply valve 23 and 10 micron air fil~ ~`
ter 24, and through a pressure regulator 27A and lubricator 28A to an air operated pneumatic booster pump 20, the pump being equipped ; with an appropriate air muffler 20A. Valve 23 has an "on" position in which compressed air is supplied to the booster pump 20; a "mix" position illustrated in FIGURE 2; and an-"off" position.
sooster pump 20 is coupled through a check vaIve 15B to an air receiver 30, and is coupled back ~hrough a check valve 15A to the inlet of regulator 27A. The outlet of filter 24 is.also coupled through a pressure regulator 25, and through a three-way valve 29 and air filter 26 to a series of pneumatic sequencing timers 34, 35 and 36, the timer 34 being normally open, and the timers 35 and 36 being normally closed.
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Timer 34 may be set to close within a time range, for example, of 1.5-15 seconds; the timer 35 may be set to open within a time range of 3-30 minutes, for example; and the timer 36 may be set to open within a time range of 5-50 seconds, for example.
The output of timer 34 is coupled to a pneumatic control valve 38D, and the output of timer 36 is coupled to pneumatic contro valves 38E and 38F. The output of timer 35 is coupled through a normally open portion of control valve 38E to a pneumatic control valve 38B and to a further pneumatic control valve 40. The output o air filter 26 is also passed through a normally ciosed portion of pneum~tic control valve 38D to a pneumatic control valve 38A.
~4~
The output of booster pump 20 is introduced through check valve 15B to the air receiver 30, whose internal pressure is desig-nated by a gage 46. Air receiver 30 is coupled through a pressure regulator 45 to a relatively small piston-type accumulator 32 whose capacit~, for example, may be one gallon; and directly to a rela-tively large piston-type accumulator 41 whose capacity for example, may be five gallons. A relief valve 17 is provided in the line between the air receiver 30 and piston accumulator 32.
:
The pressure regulator 45 reduces the pressure intxo-]0 duced to accumulator 32 from the air receiver 30 to a relatively lo~
value, so that a detergent solution is emitted from the accumula-tor 32 at relatively low pressure; whereas the air receiver is directly coupled to the accumulator 41 so that a solution dis-charged from the accumulator 41 is at relatively high pressure.
.~
The output of air filter 24 is also passed through a check valve 51A and a pressure regulator 27B and through a lubricator 28B
to an air-operated liquid pump 14, and through a check valve 51B
and receiver 54 to the normally closed pneumatic control valve 38C.
Pump 14 is equipped with a muffler 14A. Receiver 54 is included to insure adequate pressure to operate actuator 50A when the apparatus ` is operated on marginal air supply systems. When valve 38C is opened, the air pressure fxom recei~er 54 passes ~o the actuator 50A which controls a spring-loaded normally closed valve l9C. When valve l9C is opened, pressurized air from accumulator 41 and air 25 receiver 30 is discharged to an outlet O through check valve 15E.
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:
A reservoir 2 for a water and de~ergent solution is pro-vided in the apparatus, and is coupled through a 25 micron filter -~
31 and through a check valve 15C to pump 14. Pump 14 pumps the detergent through a check valve 15D into accumulator 32, and through an additional check valve 15F into accumula~or 41. Accumulator 32 ; discharges its contents through a spring-loaded normally closed ball valve l9A to outlet O; and accumulator 41 discharges its contents through a spring-loaded normally closed ball valve l9B and through a motor-operated ball valve l9D to outlet O. Outlet O is coupled to an appropriate hose 47 which is equipped with a fitting 16 and two short hoses 52 and 53.
In the operation of the apparatus, the fuel system is interrupted and the hoses 52 and 53 are attached to tne fuel system, ~ ;
so that the detergent solution may be discharged through the 15 nozzles to perform the desired cleaning function. The jet engine usually includes primary and secondary fuel injection systems.
, Hoses 52 and 53 provide connections to both systems. The hoses provide flexibility for connection to the rigid fuel lines of`the ` engine.
A by-pass circuit for pump 14 through a shut-off valve 50 is provided, as well as an independent driving air supply for the ~ pump through valve 23 in its "mix" position (illustrated in FIGURE
; 2). This provides a mixing circuit for the detergent in reservoir 2 which has a tendency to separate out of solution if left standing ,~ .
25 for any length of time. To initiate a "mix" cyole/ it is merely ; necessary to turn valve 23 to its illustrated "mix" position and .
~6--- open valve 50. Driving air is now supplied to the l~quid pump 14 only, and the solution is circulated through reservoir 2. ~.
The output of air filter 24 is also introduced ~hrough a check valve 51A, through a lubricator 28C, and through the normally closed control valve 38A to an actuator 50C which operates ~alve ~: l9A. When valve 38A is opened, the actuator 50C is caused to open the valve l9A and discharge the contents of accumulator 32 through outlet O. The output from the air filter 24 is also introduced through the normally closed control valve 38B to an actuator 50B
which operates the spring-loaded valve l9B. When the control valve 38B is opened, the valve l9B is opened. The pressurized air from the air filter 24 is also applied to the normally closed control valve 40, and when the valve 40 is operated, an air motor 18 is actuated which causes the valve l9D to rotate, intermittently to open and close. When valve 19B is opened, and when motor 18 is activated, intermittent bursts of t~he contents of accumulator 41 ar introduced to outlet O.
To operate the system of FIGURE 2, the air supply valve 23 is opened, causing the booster pump 20 to operate and pump air into the air receiver 30, until an air pressure in the air receive of, for example, 500 psi is indicated by gage 46. At the same tim~
; ! the pump 14 pumps the detergent solution from reservoir 2 into the accumulators 32 and 41, until both accumulators are filled with the detergent solution.
:
. , .
When the gage 46 indicates an air pressure of 500 psi in the air receiver 30, for example, the valve 29 is opened to start the sequence of operations in the system. When the valve 29 is opene the pressurized air from air filter 26 passes through the timer 34 to the control valve 28D ~o operate the control valve 38D. This causes the pressurized air to flow through the control valve 38D to operate the control valve 38A. When control valve 38A is operated, it causes actuator 50C to open valve l9A. The air pressure from receiver 30 now forces the piston in accumulator 32 downwardly to ` 10 cause the detergent solution within the accumulator 32 to be dis-charged through valve l9A, and through the outlet O of the system to the fuel nozzle of the jet engine. This initial discharge of about one gallon of the detergent solution is under low pressure, and it serves to wet the surfaces of the nozzle and guide vanes of :~ iJ~ the jet engine.
After a selected time interval established by the setting of timer 34, (e.gO 1.5-15 seconds~ the timer 34 closes, and the control valve 38D returns to its normally closed position, causing control valve 38A to turn of~ valve l9A to terminate the discharge of low pressure detergent from accumulator 32. After a preset time interval ~e.g. 3-30 minutes) during which p~Tlp 14 and booster 20 recharge, timer 35 opens. The pressurized air from timer 35 flows th~ough valve 38E to operate valves 38E and 40, so that the latter : ~
,~
: -5~2 control valves are opened. The opening of valve 38B causesactuator 50B to open valve 19B, and the opening of valve 40 causes air motor 18 to open and close valve l9D. The contents of the accumulator 41 are then forced through valves l9B and l9D to be emitted as pulsations of detergent solution under high pressure from the outlet O, and subsequently through the nozzles of the jet engine being cleaned. The flow rate in a constructed e~bodiment, for example, is 25 gallons per minute.
The timer 36 times out ater a preset time, in the range for example, of 5-50 seconds. When that occurs, the timer 36 causes the control valve 38E to close, and causes control valve 38F to : open~ When control valve 38E closes, both valves 38B and 40 close to terminate the intermittent flow of detergent to outlet O. When control valve 38F opens, valve 38C is opened to cause actuator 50A
to open valve l9C~ The opening of valve l9C by actuator 50A
causes pressurized air to flow from accumulator 41 and air receiver ~ 30 through check valve 15E, and through outlet O to the nozzle of ;; the jet engine to air dry the surfaces of the jet engine wetted by the detergent emission from the apparatus~ Valve 29 must be actuated to terrninate venting of air receiver 30 and accumulator 41 when pressure indicated on gage 46 is approximately lOQ psi~
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: . .
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Valve 29 is a three-way val~e, and it is now turned to its second position to interrupt the introduction of pressurized air to the control system, and to vent and reset the timers 34, 35 and 36.
The air receiver 30 now re-charges, and the cycle may be repeated S after the predetermined pressure is indicated by gage 46, by again turning valve 29. ~;
The operation of the apparatus, as described in ~IGURE 2 therefore, first causes a small amount of detergent solution to be emitted by the nozzle of ~he jet engine for cleaning purposes.
Then, under the automatic control of the system of FIGURE ~, pul-; sating jets of the detergent solution are emitted at high pressure through the fuel nozzle of the jet engine thoroughly to clean the nozzle and the guide vanes of residue fuel varnish and carbon de-posits~ After a predetermined time, the pulsating jets of the detergent solution are terminated, and a stream of pressurized air is emitted through the nozzle to dry the wetted surfaces of the nozzle and of the guide vanes of the engine.
The invention provides, therefore, a relatively simple apparatus and process which automatically enables the nozzles and :~:
I guide vanes of jet engines to be thoroughly cleaned, without any ~:~
need for dismantling the same, and in a simple and expeditious manner. As mentioned ahove, the apparatus of the invention, in -10- , ';~ : ' the embodiment described above, is advantageous in that it is com-pletely pneumatic in its operation, so as to be capable of use in aircraft hangars without any danger of creating fires or explosions It will be appreciated that while a particular embodiment of the invention has been shown and described, modifications may ;~ be made. It is intended in the accompanying claims to cover all the modifications which come within the spirit and scope of the invention.
. , ~ .
'~
~, : ' .
' i .
The invention also contemplates a process for cleaning - the fuel nozzles and guide vanes of jet engines which comprises disconnecting the fuel system of the engine from the fuel nozzles. A first step initially introduces a pressurized stream of cleaning solution at relatively low pressure into the fuel nozzles for wetting purposes, and a second step after a pre-determined time interval subsequently introduces the stream of cleaning solution at relatively high pressure into the fuel no~zles to be emitted through the fuel nozzles.
BRIEF DESCRIPTION OF THE DRAWINGS
FIGURES lA and lB are pictorial representations of apparatus constructed in accordance with the invention; and FIGURE 2 is a schematic functional diagram o the apparatus.
DETAILED DESCRIPTION OF THE ILLUSTRATED EMBODIMENT
As shown in FIGURES lA and lB, the apparatus of the . ~
invention may be mounted on a three-wheeled cart 10 which may be towed to the work site by a handle 12.
.'~
.'~
~ -3-In the schematic diagram of FIGU~E 2 f compressed air of a pressure, for example, of 100 psi is in~roduced through an inlet "I", and through a 3-way air supply valve 23 and 10 micron air fil~ ~`
ter 24, and through a pressure regulator 27A and lubricator 28A to an air operated pneumatic booster pump 20, the pump being equipped ; with an appropriate air muffler 20A. Valve 23 has an "on" position in which compressed air is supplied to the booster pump 20; a "mix" position illustrated in FIGURE 2; and an-"off" position.
sooster pump 20 is coupled through a check vaIve 15B to an air receiver 30, and is coupled back ~hrough a check valve 15A to the inlet of regulator 27A. The outlet of filter 24 is.also coupled through a pressure regulator 25, and through a three-way valve 29 and air filter 26 to a series of pneumatic sequencing timers 34, 35 and 36, the timer 34 being normally open, and the timers 35 and 36 being normally closed.
. : ' :
Timer 34 may be set to close within a time range, for example, of 1.5-15 seconds; the timer 35 may be set to open within a time range of 3-30 minutes, for example; and the timer 36 may be set to open within a time range of 5-50 seconds, for example.
The output of timer 34 is coupled to a pneumatic control valve 38D, and the output of timer 36 is coupled to pneumatic contro valves 38E and 38F. The output of timer 35 is coupled through a normally open portion of control valve 38E to a pneumatic control valve 38B and to a further pneumatic control valve 40. The output o air filter 26 is also passed through a normally ciosed portion of pneum~tic control valve 38D to a pneumatic control valve 38A.
~4~
The output of booster pump 20 is introduced through check valve 15B to the air receiver 30, whose internal pressure is desig-nated by a gage 46. Air receiver 30 is coupled through a pressure regulator 45 to a relatively small piston-type accumulator 32 whose capacit~, for example, may be one gallon; and directly to a rela-tively large piston-type accumulator 41 whose capacity for example, may be five gallons. A relief valve 17 is provided in the line between the air receiver 30 and piston accumulator 32.
:
The pressure regulator 45 reduces the pressure intxo-]0 duced to accumulator 32 from the air receiver 30 to a relatively lo~
value, so that a detergent solution is emitted from the accumula-tor 32 at relatively low pressure; whereas the air receiver is directly coupled to the accumulator 41 so that a solution dis-charged from the accumulator 41 is at relatively high pressure.
.~
The output of air filter 24 is also passed through a check valve 51A and a pressure regulator 27B and through a lubricator 28B
to an air-operated liquid pump 14, and through a check valve 51B
and receiver 54 to the normally closed pneumatic control valve 38C.
Pump 14 is equipped with a muffler 14A. Receiver 54 is included to insure adequate pressure to operate actuator 50A when the apparatus ` is operated on marginal air supply systems. When valve 38C is opened, the air pressure fxom recei~er 54 passes ~o the actuator 50A which controls a spring-loaded normally closed valve l9C. When valve l9C is opened, pressurized air from accumulator 41 and air 25 receiver 30 is discharged to an outlet O through check valve 15E.
. . .
:
A reservoir 2 for a water and de~ergent solution is pro-vided in the apparatus, and is coupled through a 25 micron filter -~
31 and through a check valve 15C to pump 14. Pump 14 pumps the detergent through a check valve 15D into accumulator 32, and through an additional check valve 15F into accumula~or 41. Accumulator 32 ; discharges its contents through a spring-loaded normally closed ball valve l9A to outlet O; and accumulator 41 discharges its contents through a spring-loaded normally closed ball valve l9B and through a motor-operated ball valve l9D to outlet O. Outlet O is coupled to an appropriate hose 47 which is equipped with a fitting 16 and two short hoses 52 and 53.
In the operation of the apparatus, the fuel system is interrupted and the hoses 52 and 53 are attached to tne fuel system, ~ ;
so that the detergent solution may be discharged through the 15 nozzles to perform the desired cleaning function. The jet engine usually includes primary and secondary fuel injection systems.
, Hoses 52 and 53 provide connections to both systems. The hoses provide flexibility for connection to the rigid fuel lines of`the ` engine.
A by-pass circuit for pump 14 through a shut-off valve 50 is provided, as well as an independent driving air supply for the ~ pump through valve 23 in its "mix" position (illustrated in FIGURE
; 2). This provides a mixing circuit for the detergent in reservoir 2 which has a tendency to separate out of solution if left standing ,~ .
25 for any length of time. To initiate a "mix" cyole/ it is merely ; necessary to turn valve 23 to its illustrated "mix" position and .
~6--- open valve 50. Driving air is now supplied to the l~quid pump 14 only, and the solution is circulated through reservoir 2. ~.
The output of air filter 24 is also introduced ~hrough a check valve 51A, through a lubricator 28C, and through the normally closed control valve 38A to an actuator 50C which operates ~alve ~: l9A. When valve 38A is opened, the actuator 50C is caused to open the valve l9A and discharge the contents of accumulator 32 through outlet O. The output from the air filter 24 is also introduced through the normally closed control valve 38B to an actuator 50B
which operates the spring-loaded valve l9B. When the control valve 38B is opened, the valve l9B is opened. The pressurized air from the air filter 24 is also applied to the normally closed control valve 40, and when the valve 40 is operated, an air motor 18 is actuated which causes the valve l9D to rotate, intermittently to open and close. When valve 19B is opened, and when motor 18 is activated, intermittent bursts of t~he contents of accumulator 41 ar introduced to outlet O.
To operate the system of FIGURE 2, the air supply valve 23 is opened, causing the booster pump 20 to operate and pump air into the air receiver 30, until an air pressure in the air receive of, for example, 500 psi is indicated by gage 46. At the same tim~
; ! the pump 14 pumps the detergent solution from reservoir 2 into the accumulators 32 and 41, until both accumulators are filled with the detergent solution.
:
. , .
When the gage 46 indicates an air pressure of 500 psi in the air receiver 30, for example, the valve 29 is opened to start the sequence of operations in the system. When the valve 29 is opene the pressurized air from air filter 26 passes through the timer 34 to the control valve 28D ~o operate the control valve 38D. This causes the pressurized air to flow through the control valve 38D to operate the control valve 38A. When control valve 38A is operated, it causes actuator 50C to open valve l9A. The air pressure from receiver 30 now forces the piston in accumulator 32 downwardly to ` 10 cause the detergent solution within the accumulator 32 to be dis-charged through valve l9A, and through the outlet O of the system to the fuel nozzle of the jet engine. This initial discharge of about one gallon of the detergent solution is under low pressure, and it serves to wet the surfaces of the nozzle and guide vanes of :~ iJ~ the jet engine.
After a selected time interval established by the setting of timer 34, (e.gO 1.5-15 seconds~ the timer 34 closes, and the control valve 38D returns to its normally closed position, causing control valve 38A to turn of~ valve l9A to terminate the discharge of low pressure detergent from accumulator 32. After a preset time interval ~e.g. 3-30 minutes) during which p~Tlp 14 and booster 20 recharge, timer 35 opens. The pressurized air from timer 35 flows th~ough valve 38E to operate valves 38E and 40, so that the latter : ~
,~
: -5~2 control valves are opened. The opening of valve 38B causesactuator 50B to open valve 19B, and the opening of valve 40 causes air motor 18 to open and close valve l9D. The contents of the accumulator 41 are then forced through valves l9B and l9D to be emitted as pulsations of detergent solution under high pressure from the outlet O, and subsequently through the nozzles of the jet engine being cleaned. The flow rate in a constructed e~bodiment, for example, is 25 gallons per minute.
The timer 36 times out ater a preset time, in the range for example, of 5-50 seconds. When that occurs, the timer 36 causes the control valve 38E to close, and causes control valve 38F to : open~ When control valve 38E closes, both valves 38B and 40 close to terminate the intermittent flow of detergent to outlet O. When control valve 38F opens, valve 38C is opened to cause actuator 50A
to open valve l9C~ The opening of valve l9C by actuator 50A
causes pressurized air to flow from accumulator 41 and air receiver ~ 30 through check valve 15E, and through outlet O to the nozzle of ;; the jet engine to air dry the surfaces of the jet engine wetted by the detergent emission from the apparatus~ Valve 29 must be actuated to terrninate venting of air receiver 30 and accumulator 41 when pressure indicated on gage 46 is approximately lOQ psi~
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Valve 29 is a three-way val~e, and it is now turned to its second position to interrupt the introduction of pressurized air to the control system, and to vent and reset the timers 34, 35 and 36.
The air receiver 30 now re-charges, and the cycle may be repeated S after the predetermined pressure is indicated by gage 46, by again turning valve 29. ~;
The operation of the apparatus, as described in ~IGURE 2 therefore, first causes a small amount of detergent solution to be emitted by the nozzle of ~he jet engine for cleaning purposes.
Then, under the automatic control of the system of FIGURE ~, pul-; sating jets of the detergent solution are emitted at high pressure through the fuel nozzle of the jet engine thoroughly to clean the nozzle and the guide vanes of residue fuel varnish and carbon de-posits~ After a predetermined time, the pulsating jets of the detergent solution are terminated, and a stream of pressurized air is emitted through the nozzle to dry the wetted surfaces of the nozzle and of the guide vanes of the engine.
The invention provides, therefore, a relatively simple apparatus and process which automatically enables the nozzles and :~:
I guide vanes of jet engines to be thoroughly cleaned, without any ~:~
need for dismantling the same, and in a simple and expeditious manner. As mentioned ahove, the apparatus of the invention, in -10- , ';~ : ' the embodiment described above, is advantageous in that it is com-pletely pneumatic in its operation, so as to be capable of use in aircraft hangars without any danger of creating fires or explosions It will be appreciated that while a particular embodiment of the invention has been shown and described, modifications may ;~ be made. It is intended in the accompanying claims to cover all the modifications which come within the spirit and scope of the invention.
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Claims (4)
1. Apparatus for cleaning residue fuel varnish and carbon from the fuel nozzles and guide vanes of a jet engine including an inlet for receiving compressed air; an outlet configured to be coupled into the fuel system of a jet engine so that the fluid emitted by the outlet may be discharged through the fuel nozzles of the jet engine to perform a cleaning function; and pneumatically operated control means for causing a pressurized stream of a cleaning solution to be emitted through the outlet, and in which said pneumatically controlled control means includes automatic sequencing timer means for causing a first stream of cleaning solution to be emitted through the outlet at a relatively low pressure and for a predetermined time interval for wetting purposes, and for subsequently causing a second stream of cleaning solution to be emitted through the outlet at relatively high pressure and as intermittent bursts.
2. The apparatus defined in claim 1, in which said pneumatically controlled control means includes means for subsequently causing a drying air stream to be emitted from the outlet.
3. The apparatus defined in claim 1, in which said pneumatically controlled control means comprises a plurality of pneumatically operated control valves.
4. The apparatus defined in claim 1, in which said bursts of cleaning solution have a pressure of the order of 500 p.s.i.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA370,569A CA1115012A (en) | 1977-10-11 | 1981-02-10 | Apparatus for cleaning jet engine nozzles |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US05/841,008 US4167193A (en) | 1977-10-11 | 1977-10-11 | Apparatus for cleaning jet engine nozzles |
| US841,008 | 1977-10-11 | ||
| CA309,224A CA1115011A (en) | 1977-10-11 | 1978-08-14 | Apparatus and process for cleaning jet engine nozzles |
| CA370,569A CA1115012A (en) | 1977-10-11 | 1981-02-10 | Apparatus for cleaning jet engine nozzles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1115012A true CA1115012A (en) | 1981-12-29 |
Family
ID=27165799
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA370,569A Expired CA1115012A (en) | 1977-10-11 | 1981-02-10 | Apparatus for cleaning jet engine nozzles |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1115012A (en) |
-
1981
- 1981-02-10 CA CA370,569A patent/CA1115012A/en not_active Expired
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| Date | Code | Title | Description |
|---|---|---|---|
| MKEX | Expiry |