IP Library Granted Patent US 8,636,472
Granted Patent B2
US 8,636,472 · App. 13/071,366 · Granted Jan 28, 2014

Blade damper, and a rotor fitted with such a damper

Inventors: Charles Louis (Aix en Provence, FR); Matthieu Ferrant (Aix en Provence, FR)
Assignee: Eurocopter
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Quick Facts
Patent No.
US 8,636,472
App. No.
13/071,366
Granted
Jan 28, 2014
Kind
B2
Abstract

The present invention relates to a damper ( 10 ) provided with an inner end strength member ( 20 ) and an outer end strength member ( 30 ) that are tubular and coaxial, a return member ( 40 ) being arranged between the inner end strength member ( 20 ) and the outer end strength member ( 30 ). The return member ( 40 ) includes an intermediate strength member ( 43 ) coaxial with the inner and outer end strength members ( 20, 30 ), said return member ( 40 ) having first and second return means ( 41, 42 ), said first return means ( 41 ) being arranged between the outer end strength member ( 30 ) and said intermediate strength member ( 43 ), said second return means ( 42 ) being arranged between the inner end strength member ( 20 ) and said intermediate strength member ( 43 ).

Claims (11)

1. A damper provided with an inner end strength member and an outer end strength member that are tubular and coaxial, a return member being arranged between the inner end strength member and the outer end strength member, wherein said return member includes an intermediate strength member coaxial with the inner and outer end strength members, said return member having first return means and second return means, said first return means being arranged between the outer end strength member and said intermediate strength member, said second return means being arranged between the inner end strength member and said intermediate strength member, one end strength member being secured to first connection means, said intermediate strength member being secured to second connection means, and the other end strength member being secured to third connection means.

2. A damper according to claim 1 , wherein the outer end strength member surrounds said first return means and said intermediate strength member, at least in part.

3. A damper according to claim 1 , wherein the intermediate strength member surrounds said second return means and said inner end strength member, at least in part.

4. A damper according to claim 1 , wherein the first return means have first stiffness and damping characteristics, the second return means having second stiffness and damping characteristics, and the first characteristics differ from the second characteristics.

5. A rotor provided with a hub and a plurality of blades, wherein the rotor includes at least one damper according to claim 1 , each damper being provided with an inner end strength member and an outer end strength member that are tubular and coaxial, a return member being arranged between the inner and outer end strength members, said return member including an intermediate strength member coaxial with the inner and outer end strength members, said return member having first return means and second return means, said first return means being arranged between the outer end strength member and said intermediate strength member, said second return means being arranged between the inner end strength member and said intermediate strength member, one of said inner end, outer end, and intermediate strength members being connected to the hub, another of said inner end, outer end, and intermediate strength members being connected to a first blade, and another of said inner end, outer end, and intermediate strength members being connected to a second blade adjacent to said first blade.

6. A rotor according to claim 5 , wherein one end strength member of a damper is secured to said hub, the other end strength member is connected to a first blade, and the intermediate strength member is connected to a second blade adjacent to said first blade.

7. A rotor according to claim 6 , wherein said outer end strength member of a damper is secured to said hub, the inner end strength member being connected to said first blade.

8. A rotor according to claim 5 , wherein one end strength member of a damper is secured to a first blade, the other end strength member is connected to a second blade adjacent to said first blade, and the intermediate strength member is connected to said hub.

9. A rotor according to claim 5 , wherein one end strength member of a damper is secured to a first blade, the other end strength member is connected to said hub, and the intermediate strength member is connected to a second blade adjacent to said first blade.

10. A rotor according to claim 5 , wherein one end strength member of a damper is secured to a first blade, the other end strength member is connected to a second blade adjacent to said first blade, and the intermediate strength member is connected to said hub.

11. A rotor according to claim 5 , wherein an intermediate strength member of a damper is secured to a first blade, one end strength member is connected to said hub, the other end strength member being connected to a second blade adjacent to said first blade.

Assignments (2)
CHANGE OF NAME Recorded May 2, 2014
From: EUROCOPTER
To: AIRBUS HELICOPTERS
Reel/Frame 032813/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 24, 2011
From: LOUIS, CHARLES; FERRANT, MATTHIEU
To: EUROCOPTER
Reel/Frame 026018/0846 →
Priority Claims (1)
FR 10 01252 · Mar 29, 2010 · national
Continuity (1)
Related Publication 20110236209A1 · Sep 29, 2011