Modular rotor craft rotor hub system

Patent metadata

Field	Value
Publication number	US-9796469-B2
Application number	US-201414245113-A
Country	US
Kind code	B2
Filing date	Apr 4, 2014
Priority date	Apr 4, 2014
Publication date	Oct 24, 2017
Grant date	Oct 24, 2017

Abstract

A rotor arm assembly for use in a rotor craft rotor hub system includes a pitch shaft and a plurality of discrete bearings coupled to the pitch shaft. The plurality of bearings are elastomeric bearings configured to facilitate movement of the rotor arm assembly about a plurality of degrees of freedom. A respective one of the plurality of bearings is configured to accommodate a single degree of freedom.

First claim

What is claimed is:

1. A rotor arm assembly for use in a rotor craft rotor hub system, said rotor arm assembly comprising:
a pitch shaft, wherein said pitch shaft comprises a first portion aligned with a pitch axis and a perpendicular second portion aligned with a flap axis;
a pitch shaft cover coupled about said pitch shaft;
a pitch housing coupled to said pitch shaft cover such that at least a portion of said pitch housing is coupled between said pitch shaft cover and said pitch shaft; and
a plurality of discrete elastomeric bearings coupled to said pitch shaft, wherein said plurality of discrete elastomeric bearings include:
a pair of flap bearings coupled to said second portion, wherein said pair of flap bearings is configured to facilitate movement of the rotor arm assembly in a first degree of freedom about the flap axis; and
an inboard pitch bearing coupled inboard of said second portion, and an outboard pitch bearing coupled at an outboard distal end of said first portion, said outboard pitch bearing being concentric with said inboard pitch bearing, wherein said inboard pitch bearing and said outboard pitch bearing are configured to facilitate movement of the rotor arm assembly in a second degree of freedom about the pitch axis, wherein the flap axis and the pitch axis are oriented perpendicularly relative to each other.

2. The rotor arm assembly in accordance with claim 1 further comprising a thrust bearing coupled to said first portion between said inboard and said outboard pitch bearings, wherein said thrust bearing is an elastomeric bearing configured to react to centrifugal thrust loads and facilitate movement about the pitch axis.

3. The rotor arm assembly in accordance with claim 2 wherein said pitch housing is configured to house at least a portion of said first portion of said pitch shaft, wherein said outboard pitch bearing and said thrust bearing are coupled between said pitch housing and said pitch shaft; and
a lead-lag link coupled to said pitch housing, said lead-lag link comprising a lead-lag bearing configured to facilitate movement about a lead-lag axis.

4. The rotor arm assembly in accordance with claim 1 , further comprising an inboard pitch housing coupled to said pitch shaft cover and configured to extend about a portion of said pitch shaft.

5. A rotor hub system for a rotor craft, said rotor hub system comprising:
a center body configured to rotate about a rotational axis;
a plurality of rotor arm assemblies configured to couple to said center body, each of said plurality of rotor arm assemblies comprising:
a pitch shaft, wherein said pitch shaft comprises a first portion aligned with a pitch axis and a perpendicular second portion aligned with a flap axis;
a pitch shaft cover coupled about said pitch shaft;
a pitch housing coupled to said pitch shaft cover such that at least a portion of said pitch housing is coupled between said pitch shaft cover and said pitch shaft; and
a plurality of discrete elastomeric bearings coupled to said pitch shaft, wherein said plurality of discrete elastomeric bearings include:
a pair of flap bearings coupled to said second portion, wherein said pair of flap bearings is configured to facilitate movement of the rotor arm assembly in a first degree of freedom about the flap axis; and
an inboard pitch bearing coupled inboard of said second portion, and an outboard pitch bearing coupled at an outboard distal end of said first portion, said outboard pitch bearing being concentric with said inboard pitch bearing, wherein said inboard pitch bearing and said outboard pitch bearing are configured to facilitate movement of the rotor arm assembly in a second degree of freedom about the pitch axis, wherein the flap axis and the pitch axis are oriented perpendicularly relative to each other.

6. The rotor hub system in accordance with claim 5 , wherein said plurality of discrete elastomeric bearings comprises
a thrust bearing coupled to said first portion between said inboard and said outboard pitch bearings, wherein said thrust bearing is an elastomeric bearing configured to react to centrifugal thrust loads and facilitate movement about the pitch axis.

7. The rotor hub system in accordance with claim 6 wherein said pitch housing is configured to house at least a portion of said first portion of said pitch shaft, wherein said outboard pitch bearing and said thrust bearing are coupled between said pitch housing and said pitch shaft; and
a lead-lag link coupled to said pitch housing, said lead-lag link comprising a lead-lag bearing configured to facilitate movement about a lead-lag axis.

8. The rotor hub system in accordance with claim 6 , wherein a load path is sequentially defined through said lead-lag link, said pitch housing, said thrust bearing, said outboard pitch bearing, said pitch shaft, and said pair of flap bearings.

9. The rotor hub system in accordance with claim 5 , wherein the plurality of rotor arm assemblies comprises a plurality of first rotor arm assemblies coupled to said center body and at least one second rotor arm assembly uncoupled from said center body, wherein one of said first rotor arm assemblies is replaceable on said center body by said second rotor arm assembly without removing remaining said plurality of first rotor arm assemblies from said center body, wherein said plurality of first rotor arm assemblies are equivalent to said second rotor arm assembly.

10. A method of assembling a rotor arm assembly for use in a rotor craft, said method comprising:
providing a pitch shaft that includes a first portion and a second portion perpendicular to the first portion;
coupling a pitch shaft cover about the pitch shaft;
coupling a pitch housing to the first portion such that at least a portion of the pitch housing is coupled between the pitch shaft cover and the first portion;
coupling a pair of flap bearings to the second portion, wherein the pair of flap bearings are configured to facilitate movement of the rotor arm assembly in a first degree of freedom about a flap axis;
coupling an inboard pitch bearing to the first portion inboard of the second portion; and
coupling an outboard pitch bearing at an outboard distal end of the first portion and concentric with the inboard pitch bearing, wherein the inboard pitch bearing and the outboard pitch bearing are configured to facilitate movement of the rotor arm assembly in a second degree of freedom about a pitch axis oriented perpendicularly relative to the flap axis, wherein the pair of flap bearings, the inboard pitch bearing, and the outboard pitch bearing are discrete elastomeric bearings.

11. The method in accordance with claim 10 , wherein coupling a pair of flap bearings further comprises coupling a pair of flap bearings configured to facilitate movement of the rotor arm assembly about only the flap axis; and wherein coupling an inboard and an outboard pitch bearing further comprises coupling an inboard and an outboard pitch bearing that are configured to facilitate movement of the rotor arm assembly about only the pitch axis.

12. The method in accordance with claim 10 further comprising coupling a thrust bearing to the pitch shaft between the inboard and the outboard pitch bearings, wherein the thrust bearing is an elastomeric bearing configured to react centrifugal thrust loads and facilitate movement of the rotor arm assembly about the pitch axis.

13. The method in accordance with claim 12 further comprising:
coupling a lead-lag link to the pitch housing, wherein the lead-lag link includes a lead-lag bearing configured to facilitate movement about a lead-lag axis, and wherein coupling the outboard pitch

Assignees

• Boeing Co

Inventors

• Loftus Jr Robert T
• Hill Jeremy Clay
• Opie Saul

Classifications

• B64C27/54

  Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement · CPC title

• B64C27/39 Primary

  with individually articulated blades, i.e. with flapping or drag hinges · CPC title

• B64C27/35 Primary

  having elastomeric joints · CPC title

• Y10T29/49332

  Propeller making · CPC title