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US4714409A Expired / Lapsed US ⏱️ 0.0 years remaining

Helicopter rotor

Assignee: Westland Group PLC
•
Filing: 1986-10-02
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Granted: 1987-12-22
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Expires: 2006-10-02
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Abstract

Abstract A helicopter rotor includes a plurality of rotor blades attached to a rotor hub by flexure members adapted during operation to permit pitch changes and flap and lag movements of the rotor blades. Each flexure member comprises a plurality of longitudinally extending reinforcing plates which in cross section extend generally radially from a geometric center of the flexure member and are enclosed in a resilient matrix material.

Inventors

  • 👤 Samuel J. M. Denison
  • 👤 David P. Bashford

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 13:12
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32; B64C27/33

Claims Analysis

Total Claims: 13
Claim 1
Independent Claim 83 words
A helicopter rotor including a rotor hub for rotation about an axis and a plurality of radially extending rotor blades each attached to the hub by an elongated flexure member to permit pitch changes and flap and lag movements of the attached rotor blade, wherein each flexure member includes a plurality of longitudinally extending reinforcing plates which in cross section extend generally radially for 360° around a geometric centre of the flexure member, said reinforcing plates being enclosed in a resilient matrix material.
Claim 2
Dependent Claim 83 words
A helicopter rotor including a rotor hub for rotation about an axis and a plurality of radially extending rotor blades each attached to the hub by an elongated flexure member to permit pitch changes and flap and lag movements of the attached rotor blade, wherein each flexure member includes a plurality of longitudinally extending reinforcing plates which in cross section extend generally radially for 360° around a geometric centre of the flexure member, said reinforcing plates being enclosed in a resilient matrix material.
Claim 3
Dependent Claim 17 words
A rotor as claimed in claim 1, wherein said reinforcing plates are arranged in diametrically opposed pairs.
Claim 4
Dependent Claim 18 words
A rotor as claimed in claim 1, wherein said reinforcing plates are distributed uniformly around said geometric centre.
Claim 5
Dependent Claim 28 words
A rotor as claimed in claim 1, wherein reinforcing plate comprises a pre-cured fibre reinforced laminate including a plurality of pre-impregnated fibre layers embedded in a matrix material.
Claim 6
Dependent Claim 17 words
A rotor as claimed in claim 4, wherein the fibres of the fibre layers are unidirectional fibres.
Claim 7
Dependent Claim 39 words
A motor as claimed in claim 5, wherein the fibres of some layers extend generally parallel to the longitudinal axis of the reinforcing plate and the fibres of other layers extend at ±45 degrees to the longitudinally extending fibres.
Claim 8
Dependent Claim 18 words
A rotor as claimed in claim 4 wherein the reinforcing plate matrix material is a thermo-setting epoxy resin.
Claim 9
Dependent Claim 19 words
A rotor as claimed in claim 1, wherein each reinforcing plate tapers downwardly in thickness from an outer edge.
Claim 10
Dependent Claim 15 words
A rotor as claimed in claim 1, wherein the resilient matrix material comprises an elastomer.
Claim 11
Dependent Claim 33 words
A rotor as claimed in claim 1, wherein the flexure member is elliptical in cross section and arranged with the minor axis aligned with the direction of flap movement of the rotor blade.
Claim 12
Dependent Claim 31 words
A rotor as claimed in claim 10, wherein the flexure member is tapered with both the minor and major axes reducing dimensionally with increasing radial distance from the axis of rotation.
Claim 13
Dependent Claim 18 words
A rotor as claimed in claim 1, wherein the flexure member is formed integral with the rotor hub.

References Cited (Backward Citations)

US3261407A Cited
US3384185A Cited
US3669566A Cited
US3762834A Cited
US4182597A Cited
US4111605A Cited
DE2823389A1 Cited
US4345876A Cited
US4352631A Cited
US4349317A Cited
US4455123A Cited
US4650401A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-12-21 1991-06-22 1991-12-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-12-21 1995-06-22 1995-12-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-12-21 1999-06-22 1999-12-22 $7700.00 Window Closed / Lapsed

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