Propeller assembly pitch change apparatus

• US 8,851,849 B2
• Filed: 11/26/2010
• Issued: 10/07/2014
• Est. Priority Date: 01/05/2010
• Status: Active Grant

• Current Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce PLC (Rolls-Royce Holdings Plc)
• Inventors: Swift, Andrew, Morgan, Antony
• Primary Examiner(s): Look, Edward
• Assistant Examiner(s): ADJAGBE, MAXIME M
• Application Number:
  US12/954,782
• Publication Number:
  US 20110164980A1
• Time in Patent Office: 1,411 Days
• Field of Search: 416/26, 416/27, 416/44, 416/46, 416/164, 416/165, 416/140, 92/24, 92/26, 92/27, 92/28
• US Class Current: 416/165
• CPC Class Codes: B64C 11/32 mechanical
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A pitch change apparatus is provided for a propeller assembly having a row of propeller blades which rotate around an axis of the assembly. The apparatus has a unison ring which is coaxial with the propeller assembly. The unison ring is movable to drive respective mechanisms for varying the pitch of the blades. The apparatus further has a plurality of pitch lock assemblies circumferentially distributed around the unison ring. Each pitch lock assembly has a free state which allows movement of the unison ring and a locked state which prevents or limits movement of the unison ring and thus prevents or limits variation of the pitch of the blades. The pitch lock assembly moves from the free to the locked state when the assembly receives a signal to lock the blades.

Claims

1. A pitch change apparatus for a propeller assembly having a row of propeller blades which rotate around an axis of the assembly, the apparatus comprising:

a unison ring which is coaxial with the propeller assembly, the unison ring being movable to drive respective mechanisms for varying the pitch of the blades, and

a plurality of pitch lock assemblies circumferentially distributed around the unison ring;

wherein each pitch lock assembly has a free state which allows movement of the unison ring and a locked state which prevents or limits movement of the unison ring and thus prevents or limits variation of the pitch of the blades, the pitch lock assembly moving from the free to the locked state when the assembly receives a signal to lock the blades.

2. A pitch change apparatus according to claim 1, wherein the pitch lock assemblies are maintained in the free state by the pressure of hydraulic fluid received from a hydraulic fluid supply, the signal to lock the blades being a drop of hydraulic pressure in the supply.

3. A pitch change apparatus according to claim 1, wherein each pitch lock assembly is mounted to a support element by a respective fastening system which allows movement of the pitch lock assembly relative to the support element, the fastening system biasing the pitch lock assembly into engagement with the support element such that, in the locked state, movement of the unison ring in a first direction corresponding to the direction of the bias is prevented by the engagement of the pitch lock assembly with the support element, while movement of the unison ring in the opposing second direction against the bias is permitted;

whereby, if a pitch lock assembly inadvertently enters the locked state when the other pitch lock assemblies are in the free state, the locked pitch lock assembly can allow movement of the unison ring in the second direction.

4. A pitch change apparatus according to claim 3, wherein the movement of the unison ring in the second direction corresponds to variation of the pitch of the blades towards coarse.

5. A pitch lock assembly of the pitch change apparatus of claim 1.

6. A propeller assembly having a pitch change apparatus according to claim 1.

7. An engine arrangement having:

a first propeller assembly having a pitch change apparatus according to claim 1,

a gear assembly that drives the first assembly, and

a power drive shaft that connects to the gear assembly at a side thereof to drive the gear assembly;

wherein the first propeller assembly is connected to the gear assembly at said side thereof, the first propeller assembly and the pitch change apparatus being coaxial with the power drive shaft.

8. A gas turbine engine having an engine arrangement according to claim 7, the engine comprising in flow series:

(i) a generator section which includes one or more turbine subsections, one or more respective generator drive shafts extending axially forwardly from the turbine subsections to one or more corresponding generator compressor subsections, and (ii) a power turbine section, the power drive shaft extending axially from the power turbine section to drive the gear assembly.

20. A pitch change apparatus according to claim 1, wherein the unison ring is movable axially to drive respective mechanisms for varying the pitch of blades.

9. A pitch change apparatus for a propeller assembly having a row of propeller blades which rotate around an axis of the assembly, the apparatus comprising:

a drive element movable to drive respective mechanisms for varying the pitch of the blades, and

a plurality of pitch lock assemblies, each pitch lock assembly having a free state which allows movement of the drive element and a locked state which limits movement of the drive element and thus limits variation of the pitch of the blades, the pitch lock assembly moving from the free to the locked state when the assembly receives a signal to lock the blades;

wherein each pitch lock assembly has a respective connection member which joins the pitch lock assembly to the drive element, the connection members allowing a predetermined amount of movement of the drive element relative to the connection members, the predetermined amount of movement corresponding to a predetermined amount of variation in the pitch of the blades, so that, in the free state, the pitch lock assemblies allow movement of the connection members and hence allow movement of the drive element, and, in the locked state, the pitch lock assemblies prevent movement of the connection members relative to the pitch lock assemblies and hence limit the drive element to the predetermined amount of movement.

10. A pitch change apparatus for a propeller assembly having a row of propeller blades which rotate around an axis of the assembly, the apparatus comprising:

a unison ring which is coaxial with the propeller assembly, the unison ring being movable to drive respective mechanisms for varying the pitch of the blades, and

a plurality of pitch lock assemblies circumferentially distributed around the unison ring;

wherein each pitch lock assembly has a free state which allows movement of the unison ring and a locked state which prevents or limits movement of the unison ring and thus prevents or limits variation of the pitch of the blades, the pitch lock assembly moving from the free to the locked state when the assembly receives a signal to lock the blades,

wherein each pitch lock assembly has a respective connection member which joins the pitch lock assembly to the unison ring so that, in the free state, the pitch lock assemblies allow movement of the connection members and hence allow movement of the unison ring, and

wherein, in the locked state, the pitch lock assemblies prevent movement of the connection members relative to the pitch lock assemblies and hence prevent or limit movement of the unison ring.

11. A pitch change apparatus according to claim 10, wherein the pitch lock assemblies are maintained in the free state by the pressure of hydraulic fluid received from a hydraulic fluid supply, the signal to lock the blades being a drop of hydraulic pressure in the supply.

12. A pitch change apparatus according to claim 10, wherein the connection members, in the locked state, allow a predetermined amount of movement of the unison ring relative to the connection members, the predetermined amount of movement corresponding to a predetermined amount of variation in the pitch of the blades.

13. A pitch change apparatus according to claim 10, wherein each pitch lock assembly is mounted to a support element by a respective fastening system which allows movement of the pitch lock assembly relative to the support element, the fastening system biasing the pitch lock assembly into engagement with the support element such that, in the locked state, movement of the unison ring in a first direction corresponding to the direction of the bias is prevented by the engagement of the pitch lock assembly with the support element, while movement of the unison ring in the opposing second direction against the bias is permitted;

whereby, if a pitch lock assembly inadvertently enters the locked state when the other pitch lock assemblies are in the free state, the locked pitch lock assembly can allow movement of the unison ring in the second direction.

14. A pitch change apparatus according to claim 13, wherein the movement of the unison ring in the second direction corresponds to variation of the pitch of the blades towards coarse.

15. A pitch lock assembly of the pitch change apparatus of claim 10.

16. A propeller assembly having a pitch change apparatus according to claim 10.

17. An engine arrangement having:

a first propeller assembly having a pitch change apparatus according to claim 10,

a gear assembly that drives the first assembly, and

a power drive shaft that connects to the gear assembly at a side thereof to drive the gear assembly;

wherein the first propeller assembly is connected to the gear assembly at said side thereof, the first propeller assembly and the pitch change apparatus being coaxial with the power drive shaft.

18. A gas turbine engine having an engine arrangement according to claim 17, the engine comprising in flow series:

(i) a generator section which includes one or more turbine subsections, one or more respective generator drive shafts extending axially forwardly from the turbine subsections to one or more corresponding generator compressor subsections, and (ii) a power turbine section, the power drive shaft extending axially from the power turbine section to drive the gear assembly.

19. A pitch change apparatus according to claim 10, wherein the unison ring is movable axially to drive respective mechanisms for varying the pitch of blades.