Patent US4630864A successfully refreshed from Google Patents.
US4630864A
Expired / Lapsed
US
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Aircraft seats
Assignee: Canon Inc
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Filing: 1984-11-23
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Granted: 1986-12-23
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Expires: 2004-11-23
Abstract
Abstract A lightweight aircraft seat based on resin preimpregnated carbon fibre comprises a bluff rectangular spar (20) integrally secured to J-tubes (26) and a diaphragm (31) spanning between the J-tubes. The spar (20) is located in a recess (16) in a leg (22) of I-section also of carbon fibre. A curvilinar front portion (24) of the seat of core and skin construction and of constant profile is cantilevered forwardly and upwardly from the spar (20). The J-tubes (26) are formed with attachment points (27), (28), (30) for seat belts, a seat back (41) and armrests.
Inventors
- 👤 Ian C. Toll
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 09:32
CPC Classifications
B; B64; B64D; B64D11/00; B64D11/06; B64D11/0619; B64D11/0639; B64D11/064; B64D11/0649; Y; Y10; Y10S; Y10S297/00; Y10S297/02
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
174 words
A seat frame assembly for an aircraft seat comprising a single laterally extending spar, at least one leg assembly to support the spar from the aircraft floor, a plurality of generally J-shaped seat supports extending from one side of the spar at laterally spaced locations with their cranked rear ends directed upwardly to locate pivoting seat backs and seat cushion support means between the or each pair of seat supports, characterised in that: (a) the seat supports extend unilaterally from the spar, and the spar and seat supports are formed with a skin of carbon fibre reinforced plastics and reinforcing cores of expanded material that prevent buckling of the spar and seat supports under load; (b) the spar is of generally rectangular section with its width greater than its depth to present a flat upper surface; (c) the apex of the or each leg assembly is formed with a cut-out in which the spar is located; and (d) the seat cushion support means is a diaphragm supported upon the spar and the seat supports.
Claim 2
Dependent Claim
174 words
A seat frame assembly for an aircraft seat comprising a single laterally extending spar, at least one leg assembly to support the spar from the aircraft floor, a plurality of generally J-shaped seat supports extending from one side of the spar at laterally spaced locations with their cranked rear ends directed upwardly to locate pivoting seat backs and seat cushion support means between the or each pair of seat supports, characterised in that: (a) the seat supports extend unilaterally from the spar, and the spar and seat supports are formed with a skin of carbon fibre reinforced plastics and reinforcing cores of expanded material that prevent buckling of the spar and seat supports under load; (b) the spar is of generally rectangular section with its width greater than its depth to present a flat upper surface; (c) the apex of the or each leg assembly is formed with a cut-out in which the spar is located; and (d) the seat cushion support means is a diaphragm supported upon the spar and the seat supports.
Claim 3
Dependent Claim
16 words
An assembly according to claim 1, wherein the cores are of rigid heat-resistant foamed plastics material.
Claim 4
Dependent Claim
16 words
An assembly according to claim 1, wherein the cores are of a material of honey-comb construction.
Claim 5
Dependent Claim
36 words
An assembly according to claim 1, wherein the diaphragm is of rigid material formed integrally with the seat supports and spar and upwardly curved at its rear end in conformity with the shape of the J-tubes.
Claim 6
Dependent Claim
43 words
An assembly according to claim 4, wherein the seat back also has a diaphragm of rigid material and extended length that in the assembled condition overlaps with the seat pan diaphragm so that the seat is isolated from the row of seats behind.
Claim 7
Dependent Claim
24 words
An assembly according to claim 5, wherein a pad of reinforcing material is moulded into the diaphragm in its upwardly curved rear end region.
Claim 8
Dependent Claim
39 words
An assembly according to claim 6, wherein the seat cushion support means further comprises a front portion of curvilinear profile cantilevered forwardly and upwardly from the front upper edge of the spar and presenting a continuous upper surface therewith.
Claim 9
Dependent Claim
39 words
An assembly according to claim 7, wherein the seat supports, spar and diaphragm are assembled from green resin-impregnated carbon fibre material and autoclaved at not more than 400° C. to cure the resin and form a rigid unitary structure.
Claim 10
Dependent Claim
41 words
An assembly according to claim 8, wherein the or each leg is formed from carbon fibre reinforced plastics material and is generally of I-section with the web portion of the I consisting of a core faced with carbon fibre reinforced plastics.
Claim 11
Dependent Claim
15 words
An assembly according to claim 9, wherein the core is of rigid heat-resistant plastics material.
Claim 12
Dependent Claim
16 words
An assembly according to claim 1, further comprising a seat cushion sitting directly on the diaphragm.
Claim 13
Dependent Claim
111 words
A combined seat frame and cushion support for an aircraft seat comprising a single laterally extending spar of non-circular cross-section presenting a flat upper surface and formed from a core of expanded material and a skin of carbon fibre reinforced plastics, a plurality of rearwardly extending seat supports of carbon fibre reinforced plastics material secured to the spar at laterally spaced locations, a seat cushion support diaphragm on and spanning between the seat supports and the spar and of a profile defined by the seat supports, and one or more legs with each leg being formed at its apex with a recess in which the spar is located and rigidly secured.
Claim 14
Dependent Claim
111 words
A combined seat frame and cushion support for an aircraft seat comprising a single laterally extending spar of non-circular cross-section presenting a flat upper surface and formed from a core of expanded material and a skin of carbon fibre reinforced plastics, a plurality of rearwardly extending seat supports of carbon fibre reinforced plastics material secured to the spar at laterally spaced locations, a seat cushion support diaphragm on and spanning between the seat supports and the spar and of a profile defined by the seat supports, and one or more legs with each leg being formed at its apex with a recess in which the spar is located and rigidly secured.
Claim 15
Dependent Claim
135 words
A combined seat frame and cushion support for an aircraft seat comprising an integrally moulded structure in carbon fibre including a spar presenting a flat upper surface, rearwardly facing J-shaped seat supports secured to the spar at laterally spaced locations, a diaphragm spanning between the seat supports to define an uninterrupted top surface with the spar and cantilevered therefrom to deform elastically in respose to the normal weight of an occupant and to undergo progressive inelastic deformation with energy absorption in response to a heavy down load, and a front portion of curvilinear profile cantilevered forwardly and upwardly from the spar with which it also defines an uninterrupted top surface and terminated in a downwardly curved nose, said front portion also undergoing progressive inelastic deformation with energy absorption in response to a heavy down load.
Claim 16
Dependent Claim
135 words
A combined seat frame and cushion support for an aircraft seat comprising an integrally moulded structure in carbon fibre including a spar presenting a flat upper surface, rearwardly facing J-shaped seat supports secured to the spar at laterally spaced locations, a diaphragm spanning between the seat supports to define an uninterrupted top surface with the spar and cantilevered therefrom to deform elastically in respose to the normal weight of an occupant and to undergo progressive inelastic deformation with energy absorption in response to a heavy down load, and a front portion of curvilinear profile cantilevered forwardly and upwardly from the spar with which it also defines an uninterrupted top surface and terminated in a downwardly curved nose, said front portion also undergoing progressive inelastic deformation with energy absorption in response to a heavy down load.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-12-22 | 1990-06-23 | 1990-12-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-12-22 | 1994-06-23 | 1994-12-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-12-22 | 1998-06-23 | 1998-12-23 | $7700.00 | Window Closed / Lapsed |