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US4509898A Expired / Lapsed US ⏱️ 0.0 years remaining

Helicopter rotors

Assignee: Westland Group PLC
•
Filing: 1983-06-20
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Granted: 1985-04-09
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Expires: 2003-06-20
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Abstract

Abstract A helicopter rotor includes attachment means for attaching a rotor hub to a tubular rotor drive shaft in a manner establishing a primary thrust load path and further attachment means adapted to provide a normally passive secondary thrust load path and operative automatically to retain the rotor hub in the event of a failure in the primary thrust load path. In the described embodiments the further attachment means comprise a multi-part collet consisting of a plurality of identical collet parts located internally of the drive shaft. Each collet part has an external frusto-conical surface one end for location adjacent a mating surface formed internally of the drive shaft, and a radially extending flange portion at its other end for attachment to an end surface of the drive shaft.

Inventors

  • 👤 Alan Gormer

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 09:13
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; Y; Y10; Y10T; Y10T403/00; Y10T403/16

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 87 words
A helicopter rotor comprising a rotor hub, a plurality of rotor blades supported by said rotor hub and extending radially therefrom, a tubular rotor drive shaft disposed within said rotor hub, primary attachment means operatively interconnecting said hub and tubular rotor drive shaft to provide a primary thrust load path, and secondary attachment means disposed internally of said drive shaft comprising a multi-part collect including a plurality of identical collect parts for retaining the rotor hub in the event of failure of the primary thrust load path.
Claim 2
Dependent Claim 87 words
A helicopter rotor comprising a rotor hub, a plurality of rotor blades supported by said rotor hub and extending radially therefrom, a tubular rotor drive shaft disposed within said rotor hub, primary attachment means operatively interconnecting said hub and tubular rotor drive shaft to provide a primary thrust load path, and secondary attachment means disposed internally of said drive shaft comprising a multi-part collect including a plurality of identical collect parts for retaining the rotor hub in the event of failure of the primary thrust load path.
Claim 3
Dependent Claim 52 words
A rotor as claimed in claim 1, wherein each collet part includes an external sloping surface at one end for location adjacent a mating frusto-conical surface formed internally of the drive shaft and a radially extending flange portion at its other end for attachment to an end surface of the drive shaft.
Claim 4
Dependent Claim 25 words
A rotor as claimed in claim 2, and including a collet retainer ring located internally of the collet parts and retained by a cap member.
Claim 5
Dependent Claim 23 words
A rotor as claimed in claim 3, wherein said cap member is annular to accommodate a protruding axially extending pitch change actuator shaft.
Claim 6
Dependent Claim 26 words
A rotor as claimed in claim 2, wherein the sloping surface of each collet part is spaced-apart from the mating frusto-conical surface of the drive shaft.

References Cited (Backward Citations)

US2464463A Cited
GB841942A Cited
US3761199A Cited
US3972491A Cited
US4201513A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1988-04-08 1988-10-08 1989-04-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1992-04-08 1992-10-08 1993-04-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1996-04-08 1996-10-08 1997-04-09 $7700.00 Window Closed / Lapsed

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