High power clutch with cleaning features

Abstract

A method of cleaning a clutch included in a drive train is disclosed in this paper. The method includes dispensing a cleaning agent, preferably a foamed cleaning agent, into the clutch. The clutch optionally includes clutch plates with evacuation channels formed in the clutch plates designed to carry cleaning agent and/or debris away from engagement surfaces of the clutch plates.

Claims

1. An aircraft comprising an airframe, a gas turbine engine configured to provide thrust for propelling the airframe, a high power accessory system configured to be driven by the gas turbine engine, and a high power clutch configured to selectively transmit rotation from the gas turbine engine to the high power accessory system, the high power clutch including a case, an input shaft, an output shaft, and clutch plates housed in the case and mounted for rotation about an axis, wherein the case of the high power clutch is opened to air surrounding the high power clutch, and wherein the clutch plates include perforations formed through the clutch plates that are sized to carry a foamed cleaning agent through associated clutch plates and evacuation channels formed in surfaces of associated clutch plates that face along the axis that are sized to carry the foamed cleaning solution radially outward away from the axis upon rotation of the clutch plates.

2. The aircraft of claim 1, wherein the clutch plates are each formed to include a central aperture such that each clutch plate has an inner diameter and an outer diameter, and wherein the evacuation channels extend from the inner diameter to the outer diameter.

3. The aircraft of claim 1, wherein the case of the high power clutch is formed to include a clutch input and a clutch output open to air around the case and sized to conduct the foamed cleaning agent into and out of the case.

4. The aircraft of claim 3, wherein the clutch output is arranged to face downwardly when the aircraft is in a generally flat or landed configuration.

5. The aircraft of claim 4, wherein the clutch input is arranged to open facing upwardly when the aircraft is in a generally flat or landed configuration.

6. The aircraft of claim 1, wherein the case of the high power clutch is formed to include a clutch opening that is open to air around the case and is sized to conduct the foamed cleaning agent.

7. The aircraft of claim 6, wherein the clutch output is arranged to face downwardly when the aircraft is in a generally flat or landed configuration.

8. The aircraft of claim 1, wherein the clutch plates comprise primarily carbon materials.

9. The aircraft of claim 1, wherein the high power accessory system is configured to provide thrust for propelling the airframe upon receipt of rotation from the gas turbine engine through the high power clutch.

10. The aircraft of claim 9, wherein the high power accessory system is a lift fan configured to produce thrust directed to provide lift for takeoff and landing of the aircraft.

11. A gas turbine engine system with a high power clutch, the system comprising a high power accessory system configured to be driven by the gas turbine engine, and a high power clutch configured to selectively transmit rotation from the gas turbine engine to the high power accessory system, the high power clutch including a case, an input shaft configured to be coupled to the gas turbine engine, an output shaft coupled to the high power accessory system, and clutch plates housed in the case and mounted for rotation about an axis, wherein the case of the high power clutch is opened to air surrounding the high power clutch, and wherein the clutch plates include perforations formed through the clutch plates that are sized to carry a foamed cleaning agent through associated clutch plates and evacuation channels formed in surfaces of associated clutch plates that face along the axis that are sized to carry the foamed cleaning solution radially outward away from the axis upon rotation of the clutch plates.

12. The system of claim 11, wherein the clutch plates are each formed to include a central aperture such that each clutch plate has an inner diameter and an outer diameter, and wherein the evacuation channels extend from the inner diameter to the outer diameter.

13. The system of claim 11, wherein the case of the high power clutch is formed to include a clutch input and a clutch output open to air around the case and sized to conduct the foamed cleaning agent into and out of the case.

14. The system of claim 13, wherein the clutch output is arranged to face downwardly relative to ground supporting the system.

15. The system of claim 14, wherein the clutch input is arranged to open facing upwardly when the relative to ground supporting the system.

16. The system of claim 11, wherein the case of the high power clutch is formed to include a clutch opening that is open to air around the case and is sized to conduct the foamed cleaning agent.

17. The system of claim 16, wherein the clutch output is arranged to face downwardly relative to ground supporting the system.

18. The system of claim 11, wherein the clutch plates comprise primarily carbon materials.

19. An air-cooled, dry high power clutch configured to selectively transmit rotation from a rotational input to a high power accessory system, the clutch comprising a case, an input shaft that extends into the, an output shaft that extends into the, and clutch plates housed in the case and mounted for rotation about an axis, the clutch plates including perforations formed through the clutch plates that are sized to carry a foamed cleaning agent through associated clutch plates and evacuation channels formed in surfaces of associated clutch plates that face along the axis sized to carry the foamed cleaning solution radially outward away from the axis upon rotation of the clutch plates.

20. The clutch of claim 11, wherein the case is formed to include a clutch input and a clutch output open to air around the case and sized to conduct the foamed cleaning agent into and out of the case.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a perspective view of an aircraft including propulsion system having (i) a gas turbine engine that produces thrust and power to drive other systems, (ii) a lift fan that produces lift for take-off and landing, and (iii) a high power clutch configured to selectively transmit rotation from the gas turbine engine to the lift fan;

(2) FIG. 2 is a perspective view of the propulsion system of FIG. 1 showing that the clutch is coupled between a driving shaft that extends from the gas turbine engine and a driven shaft that extends into the lift fan;

(3) FIG. 3 is a partially diagrammatic view of the propulsion system of FIGS. 1 and 2 with a simplified cross sectional view of the clutch showing that a cleaning agent source may be coupled to the clutch to dispense a foamed cleaning solution into the clutch to clean friction plates in the clutch;

(4) FIG. 4 is a diagram showing steps that may be included in a method of cleaning the clutch shown in FIGS. 1-3; and

(5) FIG. 5 is a perspective view of one of the friction plates included in the clutch of FIGS. 1-3 showing that each friction plate is formed to include excavation channels shaped to carry cleaning solution and/or debris away from a primary surface of the friction plate.

DETAILED DESCRIPTION

(6) For the purposes of promoting an understanding of the principles of the disclosure, reference will now be made to a number of illustrative embodiments illustrated in the drawings and specific language will be used to describe the same.

(7) An aircraft 10 according to the present disclosure includes an airframe 12 and a propulsion system 14 as shown in FIGS. 1 and 2. The propulsion system 14 provides thrust to move the airframe 12 during takeoff, flight, and landing. Maintenance of propulsion system 14 can increase the life and duty cycle of the propulsion system 14 so that the aircraft 10 has increased readiness for flight missions. In a specific example, a method 100 of cleaning internal components of a high power clutch 20 of the propulsion system 14 as described in this disclosure can lead to increased readiness.

(8) The exemplary propulsion system 14 includes a gas turbine engine 16, a lift fan 18, and the high power clutch 20 as shown in FIGS. 1 and 2. The gas turbine engine 16 produces thrust for propelling the airframe 12 forward and power to drive other systems, such as the lift fan 18. The lift fan 18 produces thrust directed to provide lift for take-off and landing. The high power clutch 20 is selectively transmits rotation from the gas turbine engine 16 to the lift fan 18.

(9) The clutch 20 is illustratively configured to facilitate a disclosed method of cleaning 100 in order to increase life and duty cycle of the clutch 20 and thereby increase readiness of the aircraft 10. The clutch 20 illustratively includes a case 22, an input shaft 24, an output shaft 26, and clutch plates 28 as shown in a simplified form in FIG. 3. The case 22 houses the shafts 24, 26 and the clutch plates 28. Hydraulic actuators (not shown) drive clutch plates 28 into engagement so as to couple output shaft 26 to input shaft 24 for rotation therewith during operation of the accessory lift fan 18.

(10) The case 22 is illustratively shaped to define a clutch input 32 and a clutch output 34 that are open to air during operation of the propulsion system 14. The clutch input 32 of the exemplary embodiment opens facing upwardly when the aircraft 10 is in a generally flat flight or landed configuration as suggested in FIG. 3. The clutch output 34 of the exemplary embodiment opens facing downwardly when the aircraft 10 is in a generally flat flight or landed configuration as suggested in FIG. 3.

(11) The input shaft 24 extends from the engine 16 into the case 22 as shown in FIG. 3. The input shaft 24 is shaped to house clutch plates 28 arranged in the case 22. The input shaft 24 is illustratively formed to include perforations 25 sized to carry a foamed cleaning agent radially through the input shaft 24 and into contact with clutch plates 28.

(12) The output shaft 26 extends from inside the case 22 to the lift fan 18 as shown in FIG. 3. The output shaft 26 also illustratively extends through the clutch plates 28.

(13) The clutch or friction plates 28 of the exemplary embodiment comprise primarily carbon materials designed to handle high temperatures during operation. Each clutch plate 28 is formed to include a central aperture 40 and has an inner diameter 41 and an outer diameter 42 that extend around an axis 45 as shown in FIG. 5. Anti-rotation notches 44 are extend into the clutch plates 28 from the outer diameter 42. Evacuation channels 46 are formed in a face or surface 48 of the clutch plates 28 facing along the axis 45 about which the friction plates 28 rotate.

(14) The evacuation channels 46 of the clutch plates 28 illustratively extend from the inner diameter 41 to the outer diameter 42 of each plate 28 and are shaped/sized to carry a foamed cleaning solution radially outward away from the axis 45 as shown in FIG. 5. The evacuation channels 46 may carry dirt/debris, cleaning agents, flushing agents, etc away from the axis 45 and away from engagement surfaces of the clutch plates 28. Accordingly, the engagement surfaces of the clutch plates 28 may be relatively free for contact with other clutch components when the clutch 20 is transferring rotation from a driving shaft to a driven shaft.

(15) During operation of the clutch 20 used for powered assisted lift is formed to include evacuation channel features 46 on the surface of the clutch plates 28 can aide in providing the function of moving air across the surfaces and to aide in evacuating debris. These evacuation channels 46 may provide a way to allow cleaning solution to be administered within the housing or case 22 of the clutch 20. The effect may include enhanced performance during operation and may extend the service life of the clutch 20 as well; whilst reducing the debris collected inside the housing or case 22.

(16) During operation of the clutch 20 a significant amount of debris can collect inside the case or housing 22 of the clutch. A method 100 to clean the clutch 20 and extend the service life using nucleated foam or other cleaning agents is provided in this disclosure. The method 100 to clean can incorporate the use of a service cart to rotate the clutch 20 while installed in the aircraft 10. The design of the clutch 20 having ports to air cool the clutch 20 during operation provides an inlet and outlet 32, 34 that may be used for facilitating the cleaning process.

(17) Turning specifically to FIG. 4, a method 100 for cleaning the high power clutch 20 is shown. In a step 110 of the method 100, a user may close the clutch outlet 34 off from atmosphere so that agents dispensed into the clutch 20 are retained in the clutch 20. In a step 112, a user may couple a cleaning agent sourcespecifically a nucleated foamed cleaning agent source 50to the clutch inlet 32. In a step 114, the user may dispense cleaning agent into the clutch 20 in order to put cleaning agent in contact with clutch plates 28.

(18) With cleaning agent in the clutch 20, in a step 115 of the method 100, a user may decouple the cleaning agent source from the clutch inlet 32. Then, in a step 116 a user may close the clutch inlet 32 to substantially close inside of the clutch case 22 from its surroundings. In a step 118, a user may rotate components of the clutch 20 to clean the clutch by causing the cleaning agent to move around the clutch 20. A service cart (not shown) may be used to drive rotation of the clutch components during cleaning.

(19) Upon interaction of cleaning agent with the clutch plates 28 and other components of the clutch 20, in a step 120 of method 100, a user may open clutch inlet 32 and/or clutch outlet 34. In a step 121, a user may couple a flushing agent source to the clutch inlet 32. In a step 122, a user may dispense water or another flushing agent from the flushing agent source into clutch 20 through clutch inlet 32. In a step 124, a user may rotate clutch components while flushing agent is in and/or is being dispensed into the clutch 20 to flush cleaning agent from components of the clutch 20.

(20) After flushing, in a step 126 of the method 100, a user may decouple the flushing agent source from the clutch inlet 32 as suggested in FIG. 4. In a step 128 of the method 100, a user may rotate clutch components to dry clutch components after cleaning and/or flushing.

(21) The method 100 includes a number of steps that may be performed in the order shown or in other various orders. It is contemplated that not all the steps shown in the method 100 are required but rather the method 100 could be performed upon actions related to only a few of the steps described. In addition, other steps not shown can be added to the steps shown in the method 100 while remaining within the contemplated scope of the method. It is appreciated that while the clutch 20 of the present disclosure is incorporated into a propulsion system 14 for an aircraft 10, the teachings of the present disclosure may be suitable for use in other systems that include clutches.

(22) While the disclosure has been illustrated and described in detail in the foregoing drawings and description, the same is to be considered as exemplary and not restrictive in character, it being understood that only illustrative embodiments thereof have been shown and described and that all changes and modifications that come within the spirit of the disclosure are desired to be protected.