发明公开
- 专利标题： Aircraft seat track fitting
- 专利标题（中）： 飞机座椅轨道配件
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申请号： EP03078247.8申请日： 1998-12-08
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公开(公告)号： EP1405786A2公开(公告)日： 2004-04-07
- 发明人: Gobeil, Richard W. , Palmer, Richard B.
- 申请人： McDonnell Douglas Corporation
- 申请人地址： 15460 Laguna Canyon Road, MC 1640-2101 Irvine, California 92618 US
- 专利权人： McDonnell Douglas Corporation
- 当前专利权人： McDonnell Douglas Corporation
- 当前专利权人地址： 15460 Laguna Canyon Road, MC 1640-2101 Irvine, California 92618 US
- 代理机构： Land, Addick Adrianus Gosling
- 优先权： US987659 19971209
- 主分类号： B64C1/20
- IPC分类号： B64C1/20 ; B64D11/06 ; B64C1/18 ; B60N2/015 ; F16B19/05 ; F16B21/02
摘要：
A fastener (78) in an interlocking assembly system for an aircraft cabin comprises
a longitudinally extending shaft (80) having first and second portions (84,86), wherein the first portion (84) is larger in lateral cross-section than the second portion (86), wherein said shaft (80) further includes a first ring (88) proximate an end of the first portion (84) opposite the second portion (86) and a second ring (90) proximate an end of the second portion (86) opposite the first portion (84), and wherein the first ring (88) is larger in lateral cross-section than the first portion (84) and the second ring (90) is larger in lateral cross-section than the second portion (86); and
an annular ferrule (82) defining a lengthwise extending channel extending between opposed first and second ends, wherein said annular ferrule (82) also defines a slit (83) which permits said annular ferrule (82) to elastically deform as said ferrule (82) is advanced over the second ring (90) so as to mount said ferrule (82) upon the second portion (86) of said shaft (80) such that the first end of said ferrule (82) is proximate the first portion (84) of said shaft (80) and the second end of said ferrule (82) is proximate the second ring (90) of said shaft (80), and wherein a portion of the channel adjacent the first end of said ferrule (82) is smaller in lateral cross-section than the first portion (84) and the portion of the channel adjacent the second end of said ferrule (82) is smaller than the second ring (90) such that said ferrule (82) is retained upon the second portion (86) of said shaft (80).
a longitudinally extending shaft (80) having first and second portions (84,86), wherein the first portion (84) is larger in lateral cross-section than the second portion (86), wherein said shaft (80) further includes a first ring (88) proximate an end of the first portion (84) opposite the second portion (86) and a second ring (90) proximate an end of the second portion (86) opposite the first portion (84), and wherein the first ring (88) is larger in lateral cross-section than the first portion (84) and the second ring (90) is larger in lateral cross-section than the second portion (86); and
an annular ferrule (82) defining a lengthwise extending channel extending between opposed first and second ends, wherein said annular ferrule (82) also defines a slit (83) which permits said annular ferrule (82) to elastically deform as said ferrule (82) is advanced over the second ring (90) so as to mount said ferrule (82) upon the second portion (86) of said shaft (80) such that the first end of said ferrule (82) is proximate the first portion (84) of said shaft (80) and the second end of said ferrule (82) is proximate the second ring (90) of said shaft (80), and wherein a portion of the channel adjacent the first end of said ferrule (82) is smaller in lateral cross-section than the first portion (84) and the portion of the channel adjacent the second end of said ferrule (82) is smaller than the second ring (90) such that said ferrule (82) is retained upon the second portion (86) of said shaft (80).
公开/授权文献
- EP1405786A3 Aircraft seat track fitting 公开/授权日：2004-08-25
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