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US4099892A Expired / Lapsed US ⏱️ 0.0 years remaining

Helicopter rotors

Assignee: Westland Group PLC
•
Filing: 1977-05-09
•
Granted: 1978-07-11
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Expires: 1997-05-09
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Abstract

Abstract A helicopter rotor includes a rotor hub and a plurality of rotor blades, the rotor hub comprising, for each rotor blade, a flexure member extending generally radially from the hub and being flexible in a blade flap plane. A feathering hinge is located at an outer end of the flexure member and includes a cylindrical portion mounted on an extension of the flexure member and resilient means arranged to permit blade lead and lag movements of the cylindrical portion during operation. In a described embodiment, the cylindrical portion is mounted on axially spaced apart bearings comprising an inner part spherical bearing having a geometrical center and an outer parallel bearing, and a resilient elastomer ring is interposed between the outer bearing and the cylindrical portion so as to permit pivotal movement of the cylindrical portion about the geometrical center of the inner bearing.

Inventors

  • 👤 Alfred Charles Martin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 15:12
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; B64C27/33

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 115 words
A helicopter rotor including a rotor hub and a plurality of rotor blades, the rotor hub comprising, for each rotor blade, a flexure member extending generally radially from the hub and being flexible in a blade flap plane, a feathering hinge located at an outer end of the flexure member and including a generally cylindrical portion rotatably mounted on axially spaced-apart inner and outer bearings on an extension of the flexure member, said inner bearing comprising a part-spherical bearing having a geometrical center, and resilient means associated with said outer bearing and arranged so as to permit, during operation, blade lead and lag movements of said cylindrical portion about the center of the inner bearing.
Claim 2
Dependent Claim 115 words
A helicopter rotor including a rotor hub and a plurality of rotor blades, the rotor hub comprising, for each rotor blade, a flexure member extending generally radially from the hub and being flexible in a blade flap plane, a feathering hinge located at an outer end of the flexure member and including a generally cylindrical portion rotatably mounted on axially spaced-apart inner and outer bearings on an extension of the flexure member, said inner bearing comprising a part-spherical bearing having a geometrical center, and resilient means associated with said outer bearing and arranged so as to permit, during operation, blade lead and lag movements of said cylindrical portion about the center of the inner bearing.
Claim 3
Dependent Claim 16 words
A helicopter rotor as claimed in claim 1, wherein said resilient means comprizes an elastomer ring.
Claim 4
Dependent Claim 29 words
A helicopter rotor as claimed in claim 2, wherein said elastomer ring is interposed between an outside surface of the bearing and an inside surface of the cylindrical portion.
Claim 5
Dependent Claim 18 words
A helicopter rotor as claimed in claim 1, wherein the flexure member is constructed of fibre-reinforced plastics material.
Claim 6
Dependent Claim 33 words
A helicopter rotor as claimed in claim 4, wherein said outer end of the flexure member is tubular in cross-section and is flared first outwardly then inwardly with respect to its longitudinal axis.
Claim 7
Dependent Claim 21 words
A helicopter rotor as claimed in claim 5, wherein metal sleeves are bonded to inner and outer surfaces of the extension.
Claim 8
Dependent Claim 30 words
A helicopter rotor as claimed in claim 6, wherein a thrust bearing is located between an outer extension of the inner sleeve and the cylindrical portion of the feathering hinge.

References Cited (Backward Citations)

US2949967A Cited
US3026942A Cited
US3231222A Cited
US3297094A Cited
US3545880A Cited
US3610774A Cited
US3926536A Cited
US3762834A Cited
US3807896A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-07-10 1982-01-09 1982-07-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-07-10 1986-01-09 1986-07-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-07-10 1990-01-09 1990-07-11 $7700.00 Window Closed / Lapsed

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