Mast lockout systems for tiltrotor aircraft

Patent metadata

Field	Value
Publication number	US-10875640-B2
Application number	US-201815897310-A
Country	US
Kind code	B2
Filing date	Feb 15, 2018
Priority date	Feb 15, 2018
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A mast lockout system for a tiltrotor aircraft having a proprotor assembly. The system includes a mast coupled to and rotatable with the proprotor assembly. A proprotor gearbox having a proprotor gearbox housing is operable to transmit torque and rotation energy to the mast. A lock assembly has first and second lock members. The first lock member is coupled to and rotatable with the mast. The second lock member is coupled to the proprotor gearbox housing. The lock assembly has a first position in which the first and second lock members are disengaged, thereby allowing rotation of the proprotor assembly. The lock assembly has a second position in which the first and second lock members are engaged, thereby preventing rotation of the proprotor assembly. The lock assembly is actuatable between the first and second positions.

First claim

What is claimed is:

1. A mast lockout system for a tiltrotor aircraft having a proprotor assembly, the system comprising:
a mast coupled to and rotatable with the proprotor assembly;
a proprotor gearbox having a proprotor gearbox housing, the proprotor gearbox operable to transmit torque and rotation energy to the mast; and
a lock assembly having first and second lock members, the first lock member coupled to and rotatable with the mast, the second lock member coupled to the proprotor gearbox housing;
wherein, the lock assembly has a first position in which the first and second lock members are disengaged, thereby allowing rotation of the proprotor assembly;
wherein, the lock assembly has a second position in which the first and second lock members are engaged, thereby preventing rotation of the proprotor assembly; and
wherein, the lock assembly is actuatable between the first and second positions.

2. The system as recited in claim 1 wherein the lock assembly further comprises a piston that is actuatable to shift the lock assembly between the first and second positions.

3. The system as recited in claim 2 wherein the piston further comprises a hydraulically actuated piston operable to shift the lock assembly between the first and second positions.

4. The system as recited in claim 1 wherein the first lock member is coupled to an exterior of the mast.

5. The system as recited in claim 1 wherein the first lock member is coupled to the mast by a splined connection to prevent relative rotation therebetween.

6. The system as recited in claim 1 wherein the first lock member further comprises a collar assembly that is coupled to the mast and at least one lock pin coupled to and radially outwardly extending from the collar assembly.

7. The system as recited in claim 6 further comprising a radial bearing coupled to the lock pin.

8. The system as recited in claim 6 wherein the at least one lock pin further comprises at least two oppositely disposed lock pins.

9. The system as recited in claim 8 further comprising a radial bearing coupled to each of the lock pins.

10. The system as recited in claim 1 wherein the second lock member is coupled to an exterior of the proprotor gearbox housing.

11. The system as recited in claim 1 wherein the second lock member further comprises a generally cylindrical inner piston housing and a generally cylindrical outer piston housing having a generally cylindrical piston disposed therebetween, the piston having at least one v-block operable to receive and align at least a portion of the first lock member therein.

12. The system as recited in claim 11 wherein the at least one v-block further comprises at least two oppositely disposed v-blocks each operable to receive and align at least a portion of the first lock member therein.

13. The system as recited in claim 11 further comprising a generally cylindrical guide coupled to the proprotor gearbox housing and disposed within the second lock member, the piston coupled to the guide by a splined connection to prevent relative rotation therebetween.

14. The system as recited in claim 11 wherein the piston defines first and second chambers with the inner and outer piston housings, the first and second chambers operable to receive and discharge a fluid to actuate the piston, thereby shifting the lock assembly between the first and second positions.

15. A mast lockout system for a tiltrotor aircraft having a proprotor assembly, the system comprising:
a mast coupled to and rotatable with the proprotor assembly;
a proprotor gearbox having a proprotor gearbox housing, the proprotor gearbox operable to transmit torque and rotation energy to the mast;
a first lock member including a collar assembly rotatable with and coupled to an exterior of the mast and at least one lock pin radially outwardly extending therefrom; and
a second lock member including a generally cylindrical inner piston housing and a generally cylindrical outer piston housing having a generally cylindrical piston disposed therebetween, the inner and outer piston housings coupled to an exterior of the proprotor gearbox housing, the piston having at least one v-block;
wherein, the second lock member has a first position in which the first and second lock members are disengaged, thereby allowing rotation of the proprotor assembly;
wherein, the second lock member has a second position in which the lock pin of the first lock member is received within and aligned by the v-block of the second lock member, thereby preventing rotation of the proprotor assembly; and
wherein, the piston is hydraulically actuatable to shift the second lock member between the first and second positions.

16. The system as recited in claim 15 wherein the lock pin is operable to slide against the v-block as the second lock member engages the first lock member to rotationally clock the proprotor assembly.

17. The system as recited in claim 15 further comprising a radial bearing coupled to the lock pin, the radial bearing operable to rotate against the v-block as the second lock member engages the first lock member to rotationally clock the proprotor assembly.

18. The system as recited in claim 15 wherein the at least one lock pin further comprises at least two oppositely disposed lock pins and wherein the at least one v-block further comprises at least two oppositely disposed v-blocks each operable to receive and align one of the lock pins.

19. The system as recited in claim 18 further comprising a radial bearing coupled to each of the lock pins and wherein each of the radial bearings is operable to rotate against one of the v-blocks as the second lock member engages the first lock member to rotationally clock the proprotor assembly.

20. A tiltrotor aircraft having rotary and non rotary flight modes, in the rotary flight mode, the tiltrotor aircraft operating at least two proprotor assemblies each having a plurality of proprotor blades, in the non rotary flight mode, the proprotor assemblies are rotationally locked and rotationally clocked for folding of the proprotor blades, for each proprotor assembly the aircraft comprising:
a mast coupled to and rotatable with the proprotor assembly;
a proprotor gearbox having a proprotor gearbox housing, the proprotor gearbox operable to transmit torque and rotation energy to the mast; and
a lock assembly having first and second lock members, the first lock member coupled to and rotatable with the mast, the second lock member coupled to the proprotor gearbox housing;
wherein, the lock assembly has a first position in which the first and second lock members are disengaged, thereby allowing rotation of the proprotor assembly;
wherein, the lock assembly has a second position in which the first and second lock members are engaged, thereby preventing rotation of the proprotor assembly; and
wherein, the lock assembly is actuatable between the first and second positions.

Assignees

• Textron Innovations Inc

Inventors

• Speller Charles Hubert
• Schank Troy Cyril

Classifications

• B64C27/50 Primary

  Blades foldable to facilitate stowage of aircraft · CPC title

• B64C27/14

  Direct drive between power plant and rotor hub · CPC title

• B64C29/0033

  the propellers being tiltable relative to the fuselage · CPC title