US4580945A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Helicopter gimbal rotor
Assignee: RTX Corp
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Filing: 1984-09-27
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Granted: 1986-04-08
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Expires: 2004-09-27
Abstract
Abstract Rotor tilt is permitted by two spherical elastomeric bearings, one above a hub member and one below, that have coincident centers at a tilt point (P) on the rotorshaft axis which is below the rotor plane. Positive rotor thrust is reacted by the upper bearing and negative rotor thrust is reacted by the lower bearing. Techniques for assembling the rotor system, precompressing the bearings, and limiting tilt are also disclosed.
Inventors
- 👤 Gordon G. Miller
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 22:37
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
102 words
A helicopter rotor system including a rotorshaft and blades defining a rotor plane that nominally intersects the rotorshaft axis at a point (Q), characterized by: first bearing means attached to the rotorshaft and pivotable about a point (P) which is below the point (Q) on the rotorshaft axis; second bearing means attached to the rotorshaft vertically offset from the first bearing means and pivotable about the point (P); a hub member to which the blades are attached and between the first and second bearing means for allowing the rotor plane to tilt about the point (P) with respect to the rotorshaft axis.
Claim 2
Dependent Claim
102 words
A helicopter rotor system including a rotorshaft and blades defining a rotor plane that nominally intersects the rotorshaft axis at a point (Q), characterized by: first bearing means attached to the rotorshaft and pivotable about a point (P) which is below the point (Q) on the rotorshaft axis; second bearing means attached to the rotorshaft vertically offset from the first bearing means and pivotable about the point (P); a hub member to which the blades are attached and between the first and second bearing means for allowing the rotor plane to tilt about the point (P) with respect to the rotorshaft axis.
Claim 3
Dependent Claim
77 words
A helicopter rotor system according to claim 1, characterized in that: the first bearing means is a first spherical laminated elastomeric element (34) having an outer race (40) slidable over the rotorshaft against a stop and an inner race (39) for engaging the hub member; and the second bearing means is a second spherical laminated elastomeric element (32) having an outer race (38) slidable over the rotorshaft and an inner race (37) for engaging the hub member.
Claim 4
Dependent Claim
39 words
A helicopter rotor system according to claim 2, characterized by: force means for bearing down upon the outer race of the second laminated elastomeric element in the direction of the first laminated elastomeric element to precompress the elastomer laminates.
Claim 5
Dependent Claim
46 words
A helicopter rotor system according to claim 2 characterized in that the outer edge of the outer race (38) and a facet of the hub element (28) are focused at the point (P) and cooperate to slidingly engage at excessive tilt angles to limit rotor tilt.
References Cited (Backward Citations)
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Cited
US2633925A
Cited
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Cited
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Cited
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Cited
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Cited
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Cited
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Cited
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Cited
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Cited
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Cited
US4477225A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-04-07 | 1989-10-07 | 1990-04-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-04-07 | 1993-10-07 | 1994-04-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-04-07 | 1997-10-07 | 1998-04-08 | $7700.00 | Window Closed / Lapsed |