Patent US4720060A successfully refreshed from Google Patents.
US4720060A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Anti-resonant suspension device having six degrees of freedom for a helicopter
Assignee: Airbus Group SAS
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Filing: 1986-06-27
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Granted: 1988-01-19
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Expires: 2006-06-27
Abstract
Abstract The device comprises four identical assemblies evenly spaced apart about the vertical axis of a speed reducer (1), offset 90° from each other and each comprising an isotropic flexible beam (4) carrying a beating weight (14) and connected by its ends to the fuselage, this beam being perpendicular to the vertical axis, and rigid triangulation means (9, 10) connecting the speed reducer (1) to the beam (4) so as transmit its forces and its moments to the beam in a plane parallel to an offset from said vertical axis of the speed reducer (1).
Inventors
- 👤 Victor Y. Yana
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 17:54
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/001; B64C2027/002; B64C2027/005; Y; Y10; Y10S; Y10S416/00; Y10S416/50
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
196 words
An anti-resonant suspension device of a lift rotor speed reducer assembly for a fuselage of a helicopter, comprising: pivot members at four locations equally spaced about the rotor speed reducer assembly; a triangular member having an apex pivotally connected to each one of said pivot members, each said triangular member having a base portion with a first base pivot and a second base pivot, each of said second base pivots connected to a base portion of the rotor speed reducer assembly; a first suspension arm suspended between a first bearing and a second bearing; a second suspension arm suspended between said second bearing and a third bearing; a third suspension arm suspended between said third bearing and a fourth bearing; a fourth suspension arm suspended between said first bearing and said fourth bearing, each of said first, second, third and fourth bearings having a base portion connected to the fuselage, each of said suspension arms having an isotropic flexible portion and a rigid portion; a support lever including a beating weight connected to each rigid portion of each suspension arm, each first base pivot of each of said triangular members being connected to a suspension arm.
Claim 2
Dependent Claim
196 words
An anti-resonant suspension device of a lift rotor speed reducer assembly for a fuselage of a helicopter, comprising: pivot members at four locations equally spaced about the rotor speed reducer assembly; a triangular member having an apex pivotally connected to each one of said pivot members, each said triangular member having a base portion with a first base pivot and a second base pivot, each of said second base pivots connected to a base portion of the rotor speed reducer assembly; a first suspension arm suspended between a first bearing and a second bearing; a second suspension arm suspended between said second bearing and a third bearing; a third suspension arm suspended between said third bearing and a fourth bearing; a fourth suspension arm suspended between said first bearing and said fourth bearing, each of said first, second, third and fourth bearings having a base portion connected to the fuselage, each of said suspension arms having an isotropic flexible portion and a rigid portion; a support lever including a beating weight connected to each rigid portion of each suspension arm, each first base pivot of each of said triangular members being connected to a suspension arm.
Claim 3
Dependent Claim
128 words
An anti-resonant suspension device according to claim 1, wherein: each of said triangular members includes a first and second bar contained in a plane parallel to a vertical axis of the rotor speed reducer assembly, the first bar extending from one of said pivot members to one of said suspension arms and the second bar extending from said suspension arm to the base portion of the rotor speed reducer assembly, a connection formed between each of first bars of said triangular member and the corresponding suspension bar including ball articulations allowing an angular movement of the connection in any direction about the center of rotation so as to transmit to the flexible arm only forces which are parallel to a plane defined by each of the triangular members.
Claim 4
Dependent Claim
137 words
An anti-resonant suspension device according to claim 1 wherein: each of said triangular members includes a rigid plate lying in a plane parallel to a vertical axis of the rotor speed reducer assembly, said rigid plate having the shape of a right triangle having a hypotenuse extending from said suspension arm to an upper part of the speed reducer, one side of the right angle of the triangle extending from a suspension arm to the base portion of the rotor speed reducer assembly, a connection between the triangular plate and the corresponding flexible arm including a ball articulation allowing for an angular movement of the connection in any direction about a center of rotation of the ball articulation so as to transmit to the suspension arm only forces parallel to a plane defined by each triangular plate.
Claim 5
Dependent Claim
16 words
An anti-resonant suspension device according to claim 3 wherein: said ball articulations include laminated spherical bearings.
Claim 6
Dependent Claim
16 words
An anti-resonant suspension device according to claim 2 wherein: said ball articulations include laminated spherical bearings.
Claim 7
Dependent Claim
36 words
An anti-resonant suspension device according to claim 2 wherein: said support lever extends obliquely from the rigid portion of each suspension arm and is adjustable along the length of each rigid portion of each suspension arm.
Claim 8
Dependent Claim
36 words
An anti-resonant suspension device according to claim 3 wherein: said support lever extends obliquely from the rigid portion of each suspension arm and is adjustable along the length of each rigid portion of each suspension arm.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-01-18 | 1991-07-20 | 1992-01-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-01-18 | 1995-07-20 | 1996-01-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-01-18 | 1999-07-20 | 2000-01-19 | $7700.00 | Window Closed / Lapsed |