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US4568244A Expired / Lapsed US ⏱️ 0.0 years remaining

Fiber reinforced/epoxy matrix composite helicopter rotor main hub plate

Assignee: RTX Corp
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Filing: 1983-03-22
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Granted: 1986-02-04
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Expires: 2003-03-22
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Abstract

Abstract A helicopter hub main retention plate is described made up of graphite and glass fiber reinforced epoxy resin. The graphite fiber reinforcement is in-plane isotropically laid continuous graphite fibers and the glass fiber reinforcement comprises segments of fiberglass continuously and circumferentially wound around the areas of retention. Such materials and configuration provide crack resistance, damage tolerance, and integrity inspectability to the retention plate.

Inventors

  • 👤 George J. Wehnert
  • 👤 Francis E. Byrnes, Jr.
  • 👤 Peter C. Ogle

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 15:19
CPC Classifications
B; B64; B64C; B64C27/00; B64C27/32

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 85 words
A helicopter hub main retention plate comprising a fiber reinforced epoxy resin matrix having a plurality of layers of: a. graphite fiber reinforcement comprising in-plane isotropically laid continuous graphite fibers, b. glass fiber reinforcement comprising a plurality of glass fiber segments circumferentially wound around a central axis in a plane substantially parallel to the plane of the graphite fiber reinforcement, said layers of graphite and glass fiber reinforcement symmetrically interleaved so as to produce crack resistance, damage tolerance, and integrity inspectability to the retention plate.
Claim 2
Dependent Claim 85 words
A helicopter hub main retention plate comprising a fiber reinforced epoxy resin matrix having a plurality of layers of: a. graphite fiber reinforcement comprising in-plane isotropically laid continuous graphite fibers, b. glass fiber reinforcement comprising a plurality of glass fiber segments circumferentially wound around a central axis in a plane substantially parallel to the plane of the graphite fiber reinforcement, said layers of graphite and glass fiber reinforcement symmetrically interleaved so as to produce crack resistance, damage tolerance, and integrity inspectability to the retention plate.

References Cited (Backward Citations)

US4195967A Cited
US4257738A Cited
DE3037824A1 Cited
US4156583A Cited
US4293276A Cited
US4342540A Cited
US4321013A Cited
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US4427340A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1989-02-03 1989-08-05 1990-02-04 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1993-02-03 1993-08-05 1994-02-04 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1997-02-03 1997-08-05 1998-02-04 $7700.00 Window Closed / Lapsed

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