Bearingless gimbaled rotor hubs and swashplates

Patent metadata

Field	Value
Publication number	US-11891168-B2
Application number	US-202117396095-A
Country	US
Kind code	B2
Filing date	Aug 6, 2021
Priority date	Jun 11, 2018
Publication date	Feb 6, 2024
Grant date	Feb 6, 2024

Abstract

A gimbal joint may employ a plurality of wear sleeves, each disposed between a pin or pin receptive bore of a first structure and a corresponding bore or pin of a second structure and between another pin or bore of the second structure and a corresponding bore or pin of a third structure. Each of these structures may be adapted to rotate in a single plane, with one structure adapted to also tilt about a first axis, and one other structure adapted to tilt about a second axis. Each integral flanged wear sleeve may comprise a right circular hollow cylindrical body portion, which may be interiorly sized to be retained on one of the pins and externally sized to be retained in one of the pin receptive bores, and a flange portion may radiate from one end of the cylindrical body portion.

First claim

What is claimed is:

1. A gimbal joint comprising:
a first plurality of integral flanged wear sleeves, each integral flanged wear sleeve disposed between one pin of opposing pin portions of an integral trunnion and a corresponding pin receptive bore of an integral coupling, the integral trunnion defining an integral internally splined central driveshaft or mast coupling bore portion configured to mate with a rotor driveshaft or mast end and spline the integral trunnion to a mast or driveshaft of an aircraft for movement along the mast or driveshaft perpendicular to a single plane and adapted to rotate in the single plane and the integral coupling adapted to move along the mast or driveshaft, rotate in the single plane and tilt relative to the single plane about a first axis parallel to the single plane;
a second plurality of integral flanged wear sleeves, each disposed between another pin or pin receptive bore of the integral trunnion and a corresponding pin receptive bore or pin of a pillow or mounting block, the block adapted to rotate in the single plane and tilt relative to the single plane about a second axis parallel to the single plane and perpendicular to the first axis;
each integral flanged wear sleeve comprising:
a right circular hollow cylindrical body portion interiorly sized to be retained on one of the pins and externally sized to be retained in one of the pin receptive bores; and
a flange portion radiating from an outer end of the cylindrical body portion, the flange portion having a diameter larger than a diameter of the pin receptive bores and bearing on a face of a respective structure.

2. The gimbal of claim 1 , wherein at least one of the flanged wear sleeves further comprises:
a low friction coating or lining disposed on at least an outer surface of the body portion;
a low friction coating or lining disposed on an inner surface of the body portion of the at least one flanged wear sleeve; and/or
a low friction coating or lining disposed on an inner face of a flange portion of the at least one flanged wear sleeve.

3. The gimbal joint of claim 1 , wherein each pin further comprises a longitudinal bore, and the gimbal joint further comprises a fastener secured in each longitudinal bore, bearing on, and tensioned against, the respective wear sleeve flange, replaceably retaining the respective wear sleeve on the respective pin and in the respective pin receptive bore.

4. The gimbal joint of claim 1 , wherein the right circular hollow cylindrical body portion is interiorly sized to be retained on one of the pins and externally sized to be rotatably retained in one of the pin receptive bores.

5. The gimbal joint of claim 1 , wherein the right circular hollow cylindrical body portion is interiorly sized to be rotatably retained on one of the pins and externally sized to be retained in one of the pin receptive bores.

6. The gimbal joint of claim 1 , wherein:
the integral coupling is ring-shaped, defines integral pin receptive bore portions configured for rotatably pinning to the integral trunnion via the trunnion pins, and defines integral coupling pin portions;
the pillow or mounting block comprises a plurality of pillow blocks, each pillow block defining a coupling pin receptive bore and secured to, or an integral part of, a rotor yoke of the aircraft; and
one of each of the first or second plurality of integral flanged wear sleeves is disposed in each coupling ring pin receptive bores and in each pillow block pin receptive bore, over respective trunnion drive pins or coupling ring drive pins, rotatably retaining the respective trunnion drive pin with respect to the respective coupling ring pin receptive bore, or the respective coupling ring drive pin with respect to the respective pillow block pin receptive bore, coupling the integral trunnion to the rotor yoke of the aircraft.

7. The gimbal joint of claim 1 , wherein:
the pillow or mounting block comprises a plurality of mounting blocks, each mounting block defining a mounting pin and secured to, or an integral part of, a rotor yoke of the aircraft;
the integral coupling is a ring-shaped integral ring coupling and defines a plurality of integral pin receptive bore portions configured for rotatably pinning to the integral trunnion via the trunnion pins and rotatably pinning to the mounting blocks via respective mounting pins; and
one of each of the first or second plurality of integral flanged wear sleeves is disposed in each integral ring coupling pin receptive bores over a respective trunnion drive pin or mounting block pins, rotatably retaining the respective trunnion drive pin or mounting block pin with respect to the respective integral ring coupling pin receptive bore, coupling the integral trunnion to the mounting blocks and thereby to a rotor yoke of the aircraft.

8. An aircraft gimbal comprising:
an integral trunnion comprising:
an annular body portion defining a central splined central driveshaft or mast coupling bore configured to mate with a rotor driveshaft or mast end and spline the integral trunnion to the mast or driveshaft for movement along the mast or driveshaft, perpendicular to a single plane; and
a plurality of opposing integral trunnion drive pin portions extending from the annular body portion;

a pair of blocks configured to be secured to, or is an integral part of, a rotor yoke;
an integral coupling defining:
opposing trunnion pin receptive bores; and

a plurality of integral flanged wear sleeves, one integral flanged wear sleeve disposed in each of the integral coupling trunnion pin receptive bores, over a respective trunnion drive pin, rotatably retaining the respective trunnion drive pin with respect to the respective integral coupling trunnion pin receptive bore, each integral flanged wear sleeve comprising:
a right circular hollow cylindrical body portion interiorly sized to be retained on one of the trunnion drive pin portions of the trunnion and externally sized to be rotatably retained in one of the pillow block trunnion pin receptive bores and/or one of the drive coupling trunnion pin receptive bores; and
a flange portion radiating from an outer end of the cylindrical body portion, the flange portion having a diameter larger than a diameter of the pillow block trunnion pin receptive bores and the drive coupling trunnion pin receptive bores, bearing on a face of a respective pillow block or a respective face of the drive coupling.

9. The gimbal of claim 8 , wherein at least one of the flanged wear sleeves further comprise:
a low friction coating or lining disposed on at least an outer surface of the body portion;
a low friction coating or lining disposed on an inner surface of the body portion of the at least one flanged wear sleeve; and/or
a low friction coating or lining disposed on an inner face of a flange portion of the at least one flanged wear sleeve.

10. The gimbal of claim 8 , wherein each drive pin portion of the integral trunnion further comprises a longitudinal bore, and the rotor hub gimbal further comprises a fastener secured in each trunnion drive pin longitudinal bore and bearing on, and tensioned against, the respective wear sleeve flange, replaceably retaining the respective wear sleeve on the respective integral trunnion drive pin and replaceably retaining the flanged wear sleeve and integral trunnion in place.

11. The gimbal of claim 8 , wherein:
the integral coupling is ring-shaped and further defines integral coupling pin portions;
the blocks are pillow blocks, each pillow block defining a coupling pin receptive bore; and
one integral flanged wear sleeves is disposed in each pillow block pin receptive bore, over respective integral coupling ring d

Assignees

• Textron Innovations Inc

Inventors

• Baldwin Tyler Wayne
• Cravener Kyle Thomas

Classifications

• B64C27/41 Primary

  with flapping hinge or universal joint, common to the blades · CPC title

• F16C11/02

  Trunnions; Crank-pins (fastening crank-pins to webs, crank-pins integral with cranks F16C3/06, F16C3/22) · CPC title

• F16C17/02

  for radial load only · CPC title

• F16C33/20

  Sliding surface consisting mainly of plastics (F16C33/22 - F16C33/28 take precedence) · CPC title

• F16D3/2052

  having two pins · CPC title