Propeller pitch change mechanism

• US 5,431,539 A
• Filed: 10/28/1993
• Issued: 07/11/1995
• Est. Priority Date: 10/28/1993
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Carvalho, Paul A.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Lee, Michael S.
• Application Number:
  US08/147,236
• Time in Patent Office: 621 Days
• Field of Search: 416/157 R, 416/165, 416/168 R, 416/168 A, 416/164
• US Class Current: 416/168.00R
• CPC Class Codes: B64C 11/32 mechanical
• CPC Class Codes: F01D 7/00 Rotors with blades adjustable in operation; Control thereof for reversing F01D1/30
• CPC Class Codes: F02K 1/66 using reversing fan blades
• CPC Class Codes: F02K 3/06 with front fan
• CPC Class Codes: F05D 2220/36 specially adapted for the fan of turbofan engines

Abstract

The pitch change mechanism for a variable pitch propeller blade or Advanced Ducted Propulsor (ADP) interconnecting the pitch change actuator and the propeller blades of the type that includes a trunnion attached to the root of the propeller blade, the connecting mechanism includes in one embodiment a translating ball screw nut interconnecting the trunnion through a yoke and a cooperating sliding pin and arm connector. In another embodiment where a hydraulic piston is included in the pitch change actuator the cylindrical housing supports a plurality of circumferentially spaced pins that are in sliding relationship with a rod attached to the trunnion. The trunnions in both embodiments are extended to make the interconnections. Means are provided to prevent the blades from binding up during pitch change movements. This invention eliminates the heretofore utilized sliding anti-rotation spline and the multiple linkage connectors.

Claims

1. A propulsor having a plurality of variable pitch blades including actuator means for varying the pitch of said blades about its longitudinal axis, said blades including a hub for supporting said blade for rotational movement about the axis of the propulsor and the longitudinal axes of said blades, each blade having a root end, a trunnion extending from said root end, connection means interconnecting said actuator means and said trunnion of each blade including a pin, said connection means for rotating said blades about said longitudinal axis, said connection means disposed in linear sliding relationship with said trunnion for transmitting rectilinear motion relative to said trunnion, whereby said connection means and said pin rotate each of said blades in unison about said longitudinal axis for obtaining pitch change movement.

2. A propulsor as claimed in claim 1 wherein said connection means includes an annular yoke disposed coaxially relative to said axis of said propulsor, arms circumferentially spaced in said yoke and extending axially toward said trunnion and there being an arm for each trunnion and slidably connected to said pin whereby said arm moves axially relative to said pin upon pitch change movement.

3. A propulsor as claimed in claim 2 including a spherical bearing in an aperture formed in said arm and a central opening in said spherical bearing operatively connected to said pin.

4. A propulsor as claimed in claim 3 including a clevis attached to said trunnion and supporting said pin in radial alignment relative to said axis of said propulsor.

5. A propulsor as claimed in claim 4 wherein said actuator means includes a ball screw that is rotatable in clockwise and counter clockwise directions, and a ball screw nut operatively connected to said ball screw for rectilinear movement, said yoke attached to said ball screw nut to be positioned rectilinearly with said ball screw nut for effectuating pitch change movement.

6. A propulsor as claimed in claim 1 wherein said actuator means includes a movable hollow cylinder and a fixed piston mounted in said hollow cylinder, said hollow cylinder closed at either end and defining with said fixed piston a pair of opposing fluid receiving chambers, fluid connection means for selectively admitting and bleeding fluid from said fluid receiving chambers for moving said cylinder rectilinearly, a plurality of circumferentially spaced pins attached to said cylinder, said connection means operatively connected to said pins in sliding relationship for rotating said blades in unison about said longitudinal axis for pitch change movement, whereby said pins move axially relative to said connection means when said blades are changing pitch.

7. A propulsor as claimed in claim 6 wherein said cylinder is rotated circumferentially around said axis of the propulsor when said blades are changing pitch.

8. A propulsor as claimed in claim 7 wherein said connection means includes a rod end attached to each of said trunnions, said rod end operatively connected to said pins and being in sliding relationship relative thereto whereby said pin moves axially relative to said rod end when said blades changes pitch.

9. A propulsor as claimed in claim 8 including a spherical bearing mounted in an aperture formed in said rod, and said pin fitting into a central opening formed in said spherical bearing.

10. A propulsor as claimed in claim 4 wherein said actuator means includes a hydraulic actuator including a moveable cylinder closed on either end defining a chamber, a fixed piston disposed in said chamber defining a pair of opposing sub-chambers, means for admitting fluid into and bleeding fluid from said sub-chambers for moving said cylinder rectilinearly, said yoke attached to said cylinder to be positioned rectilinearly with said cylinder for effectuating pitch change movement.

11. A propulsor as claimed in claim 1 wherein said actuator means includes a movable hollow cylinder and a fixed piston mounted in said hollow cylinder, said hollow cylinder closed at either end and defining with said fixed piston a pair of opposing fluid receiving chambers, fluid connection means for selectively admitting and bleeding fluid from said fluid receiving chambers for moving said cylinder rectilinearly, a yoke operatively connected to said cylinder, a plurality of circumferentially spaced pins attached to said yoke, said connection means operatively connected to said pins in sliding relationship for rotating said blades in unison about said longitudinal axis for pitch change movement, whereby said pins and said connection means move axially relative to each other when said blades are changing pitch.

12. A propulsor as claimed in claim 11 wherein said connection means includes a rod end attached to each of said trunnions, said rod end operatively connected to said pins and being in sliding relationship relative thereto whereby said pin and said rod end moves axially relative to each other when said blades changes pitch.

13. A propulsor as claimed in claim 12 including a spherical bearing mounted in an aperture formed in said rod, and said pin fitting into a central opening formed in said spherical bearing.