Rotor hub damper for a rotorcraft

Patent metadata

Field	Value
Publication number	US-9765825-B2
Application number	US-201314135670-A
Country	US
Kind code	B2
Filing date	Dec 20, 2013
Priority date	Dec 20, 2013
Publication date	Sep 19, 2017
Grant date	Sep 19, 2017

Abstract

A damper for a rotor hub for a rotorcraft can include a housing, a piston resiliently coupled to the housing with a first elastomeric member and a second elastomeric member, a plurality of conical members, a fluid, and an orifice.

First claim

The invention claimed is:

1. A damper for a rotor hub for a rotorcraft, the damper comprising:
a housing;
a piston resiliently coupled to the housing with a first elastomeric member and a second elastomeric member;
a plurality of conical members coupled between the housing and the piston in a compressive state, such that a relative motion between the piston and the housing causes the plurality of conical members to flex by a compressive load change, the compressive load change being produced by the relative motion between the piston and the housing;
a fluid; and
an orifice;
wherein the first elastomeric member, the second elastomeric member, the piston, the housing, and the conical members form inner chambers between the conical members and the piston and outer chambers between the conical members and the housing, each of the inner chambers and outer chambers comprising an at least partially conical shape;
wherein flexure of the conical members pumps the fluid through the orifice;
wherein the inner chambers are located radially between the conical members and the piston; and
wherein the inner chambers have a higher pressure of fluid than the outer chambers.

2. The damper according to claim 1 , wherein the plurality of conical members are stacked in an alternating arrangement.

3. The damper according to claim 1 , wherein the plurality of conical members include a first conical member having an inner portion abutted to a shoulder of the piston.

4. The damper according to claim 1 , wherein the plurality of conical members include a second conical member having an outer portion abutted to a shoulder of the housing.

5. The damper according to claim 1 , wherein the damper has a spring rate derived from the first elastomeric member, the second elastomeric member, and the plurality of conical members.

6. The damper according to claim 1 , wherein the damper has a damping rate derived from at least the fluid being forced through the orifice during a translation of the piston relative to the housing.

7. The damper according to claim 1 , wherein the plurality of conical members are metal.

8. The damper according to claim 1 , wherein the rotor hub is a main rotor hub.

9. The damper according to claim 1 , wherein the rotor hub is a tail rotor hub.

10. The damper according to claim 1 , wherein the housing is coupled to a rotor grip of a rotor blade.

11. The damper according to claim 1 , wherein the piston is coupled to a yoke of the rotor hub.

12. The damper according to claim 1 , wherein the piston has an elongated portion that extends through an opening in each of the plurality of conical members.

13. The damper according to claim 12 , wherein the orifice is an inner channel formed by a clearance between an inner portion of at least one of the plurality of conical members and the elongated portion of the piston.

14. The damper according to claim 1 , wherein the orifice is an outer channel formed by a clearance between an outer portion of at least one of the plurality of conical members and the housing.

15. The damper according to claim 1 , wherein the orifice includes a plurality of inner channels fluidly connecting the inner chambers, and include a plurality of outer channels fluidly connecting the outer chambers.

16. The damper according to claim 15 , further comprising:
a plurality of fluid passages providing fluid communication between the outer chambers and the inner chambers.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Stamps Frank B
• Sottiaux Daniel P

Classifications

• B64C27/39

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

• B60G15/066

  the spring being different from a coil spring (B60G15/065 takes precedence) · CPC title

• B64D35/04

  characterised by the transmission driving a plurality of propellers or rotors · CPC title

• F16D3/80 Primary

  in which a fluid is used (fluid couplings allowing continuous slip F16D31/00 - F16D35/00) · CPC title

• B64C27/51 Primary

  Damping of blade movements · CPC title