Hub for rotary wing aircraft

• US 5,620,305 A
• Filed: 03/20/1995
• Issued: 04/15/1997
• Est. Priority Date: 03/20/1995
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: McArdle, Francis H.
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): Sgantzos, Mark
• Application Number:
  US08/406,576
• Time in Patent Office: 757 Days
• Field of Search: 416/102, 416/134 A, 416/140, 416/148
• US Class Current: 416/134.00A
• CPC Class Codes: B64C 27/45 with a feathering hinge only

Abstract

A rotor hub for a rotary wing aircraft is described which allows the use of more than three blades on the rotor head while providing all of the required functional features. The rotor head is constructed using a central barrel to which is attached a plurality of blade attachment points on its exterior surface. The pitch arm actuating points are located inside of the hub barrel, extending from the outer surface into the hub barrel through arcuate slots in the barrel. The hub is particularly adapted for use with tilt rotor rotary wing aircraft and provides a negative Delta 3 blade pitch input in response to wind gusts and abrupt pilot control inputs.

Claims

1. A hub for a rigid rotor rotary wing aircraft for mounting a plurality of rotating airfoil blades for rotation about a rotor shaft spin axis, said hub comprising:

a hub shell having a central opening therethrough having a central axis, the central axis of said central opening lying along the rotor shaft spin axis, said shell being attached to said rotor shaft for rotation therewith;

a plurality of inner members attached to said hub shell for rotation therewith, one of said inner members being provided for each of said blades, said inner members having a blade pitch axis approximately orthogonal to said rotor shaft spin axis;

a plurality of outer members, each outer member enclosing one of said inner members and rotatable about said blade pitch axis with respect to said inner member;

a plurality of pitch housings, each of said pitch housings being attached to the inboard end of one of said outer members nearest said hub for rotation therewith, said pitch housings having a pitch arm extending into the central opening in said hub shell;

a first bearing mounted between each of said inner members and its respective outer member for supporting the outer member for rotation about the blade pitch axis;

a second bearing mounted between each of said pitch housings and its respective inner member for supporting said pitch housing for rotation about the blade pitch axis; and

blade attachment means at the outboard end each of said outer members for attaching a rotor blade thereto.

2. The hub according to claim 1 wherein each of said inner members have a flexure beam between its inboard and outboard ends to compensate for different coning angles of individual blades.

3. The hub according to claim 1 wherein said inner and outer members are generally cone shaped, the inner surface of said outer member being substantially concentric with the outer surface of said inner member.

4. The hub according to claim 2 wherein said outer member is generally cone shaped, the inner surface of said outer member substantially surrounding the outer surface of said inner member.

5. The hub according to claim 1 wherein said first and second bearings are elastomeric bearings.

6. The hub according to claim 2 wherein said first and second bearings are elastomeric bearings.

7. The hub according to claim 1 wherein the number of airfoil blades is more than three.

8. The hub according to claim 2 wherein the number of airfoil blades is more than three.

9. The hub according to claim 1 wherein said hub shell is attached to said rotor shaft by means of an elastomeric bearing, said elastomeric bearing providing universal movement of said hub about said rotor shaft spin axis.

10. The hub according to claim 2 wherein said hub shell is attached to said rotor shaft by means of an elastomeric bearing, said elastomeric bearing providing universal movement of said hub about said rotor shaft spin axis.

11. The hub according to claim 9 wherein said elastomeric bearing comprises at least two elastomeric bearings, said bearings being spaced apart along the rotor shaft spin axis.

12. The hub according to claim 10 wherein said elastomeric bearing comprises at least two elastomeric bearings, said bearings being spaced apart along the rotor shaft spin axis.

13. The hub according to claim 3 wherein said first and second bearings are elastomeric bearings.

14. The hub according to claim 4 wherein said first and second bearings are elastomeric bearings.

15. The hub according to claim 13 wherein said hub shell is attached to said rotor shaft by means of an elastomeric bearing, said elastomeric bearing providing universal movement of said hub about said rotor shaft spin axis.

16. The hub according to claim 15 wherein said elastomeric bearing comprises at least two elastomeric bearings, said bearings being spaced apart along the rotor shaft spin axis.

17. The hub according to claim 14 wherein said hub shell is attached to said rotor shaft by means of an elastomeric bearing, said elastomeric bearing providing universal movement of said hub about said rotor shaft spin axis.

18. The hub according to claim 17 wherein said elastomeric bearing comprises at least two elastomeric bearings, said bearings being spaced apart along the rotor shaft spin axis.