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1. 发明专利

JP2012505108A Vehicle and aircraft seat of the shock absorbing mechanism equipped with a foot protection 审中-公开
公开(公告)号：JP2012505108A
公开(公告)日：2012-03-01
申请号：JP2011530628
申请日：2009-02-26
申请人：モビウスプロテクションシステムズリミテッド
发明人：デヴィドエンゲル , モシェヤコブバウム , アナンハサン , シャイミンデル
IPC分类号： B60N2/42 , B60R21/02 , B64D11/06 , B64D25/04 , F16F7/12
CPC分类号： B60N2/4242 , B60N2/24 , B60N2/42709 , B64D11/0619 , B64D11/0689 , F16F7/128 , Y10T29/49615
摘要： The present invention discloses a method and apparatus for minimizing accelerations during impacts such as those encountered in motor vehicle accidents, helicopter and airplane crashes, explosions, and the like. The preferred embodiment takes the form of a helical spring-like member (100), designed to experience plastic deformation over a desired deformation length, under a given impact load threshold. The spring-like member is preferably installed in a mechanical linkage that is flattened under impact, straining the spring-like member in a predictable fashion. The operating characteristics of this system [namely the stress-strain curve, and thus the deformation length, impact load threshold, and acceptable load range for the system to be protected] can be easily controlled by varying the device dimensions and installation configuration.

2. 发明专利

JP2010247789A Impact-absorbing structure and method for producing the same 有权
标题翻译：冲击吸收结构及其制造方法
公开(公告)号：JP2010247789A
公开(公告)日：2010-11-04
申请号：JP2009102091
申请日：2009-04-20
申请人： Mitsubishi Heavy Ind Ltd , 三菱重工業株式会社
发明人： TANAKA TOYOMI , MARUYAMA HIROYOSHI , KANEMASU MASAYUKI
IPC分类号： B62D29/04 , B62D21/15 , B64D25/04 , F16F7/12
CPC分类号： B64C1/062 , B29C65/483 , B29C65/5057 , B29C66/721 , B29C70/086 , B29C70/865 , B29C70/88 , B29K2063/00 , B29K2067/00 , B29K2067/06 , B29K2069/00 , B29K2075/00 , B29K2077/00 , B29K2077/10 , B29K2079/08 , B29K2101/10 , B29K2101/12 , B29K2105/06 , B29K2277/10 , B29K2305/00 , B29K2307/00 , B29K2307/02 , B29K2309/04 , B29K2309/08 , B29K2707/04 , B29K2995/0089 , B29L2031/3076 , B29L2031/608 , Y02T50/43 , Y02T50/433 , Y10T156/10
摘要： PROBLEM TO BE SOLVED: To provide an impact-absorbing structure superior in impact-absorbing capacity. SOLUTION: The impact-absorbing structure includes: a pair of flat, plate-like face plates 19 arranged to oppose each other with a predetermined distance therebetween; a core member arranged between the face plates 19 and fixed to the face plates 19; and a composite-material tube 7 arranged between the face plates 19, at the core member side, the impact-absorbing member extending in one direction and fracturing progressively due to an impact compression force acting in the one direction. The composite-material tube 7 is fixed to the face plates 19 at one portion constituting a bonded region A and is allowed to move relative to the face plates 19 at a remaining portion constituting a non-bonded region B. COPYRIGHT: (C)2011,JPO&INPIT
摘要翻译：要解决的问题：提供冲击吸收能力优异的冲击吸收结构。解决方案：冲击吸收结构包括：一对扁平的板状面板19，它们以彼此间隔预定距离彼此相对布置; 芯片构件，布置在面板19之间并固定到面板19; 以及配置在面板19之间的复合材料管7，在芯构件侧，冲击吸收构件沿一个方向延伸并且由于沿一个方向作用的冲击压缩力而逐渐压裂。复合材料管7在构成接合区域A的一部分处固定到面板19，并且允许其在构成非接合区域B的剩余部分处相对于面板19移动。版权所有（ C）2011，JPO＆INPIT

3. 发明专利

JP4260124B2 Aircraft seat 有权
标题翻译：空值
公开(公告)号：JP4260124B2
公开(公告)日：2009-04-30
申请号：JP2005056172
申请日：2005-03-01
申请人：小糸工業株式会社
发明人：文吾浅見 , 浩平鈴木
IPC分类号： B64D25/04 , A47C7/40 , A47C7/62 , B60N3/00
CPC分类号： B64D11/0649 , A47C7/40 , B60N2/686 , B60N3/004 , B64D11/0638 , B64D11/064 , Y02T50/46

4. 发明专利

JP2006123802A Landing shock absorbing device 审中-公开
标题翻译：降落式吸收装置
公开(公告)号：JP2006123802A
公开(公告)日：2006-05-18
申请号：JP2004316172
申请日：2004-10-29
申请人： Fuji Heavy Ind Ltd , 富士重工業株式会社
发明人： NARABASHI TOSHIYUKI
IPC分类号： B64D25/04 , B60R21/16
摘要： PROBLEM TO BE SOLVED: To provide a landing shock absorbing device capable of protecting an occupant by effectively absorbing landing shock by a simple structure.
SOLUTION: This device is provided with seat holding and lowering means (a rail member 1, a slide member 2 and a shear pin 3, etc.) for holding a seat 10 at a prescribed position and lowering the seat 10 on which the occupant P sits from the prescribed position when the prescribed landing shock is applied, and an air bag 4 for supporting the seat 10 from a lower side. When the prescribed landing shock is applied, the shear pin 3 is broken, the seat 10 is lowered, and the seat 10 is supported by the air bag 4 from the lower side with the air bag deformed, and thereby the landing shock applied to the occupant P is reduced.
COPYRIGHT: (C)2006,JPO&NCIPI
摘要翻译：要解决的问题：提供一种能够通过简单的结构有效地吸收着陆冲击来保护乘员的着陆减震装置。解决方案：该装置设置有用于将座椅10保持在规定位置的座椅保持和降低装置（轨道构件1，滑动构件2和剪切销3等），并且在其上降低座椅10，当施加规定的着陆冲击时，乘客P从规定的位置坐下，以及用于从下侧支撑座椅10的气囊4。当施加规定的着陆冲击时，剪切销3被破坏，座椅10下降，并且座椅10由安全气囊变形而从下侧被气囊4支撑，从而将着陆冲击施加到乘员P减少。版权所有（C）2006，JPO＆NCIPI

5. 发明专利

JP2004509017A Seat that converts to a bed 审中-公开
公开(公告)号：JP2004509017A
公开(公告)日：2004-03-25
申请号：JP2002528558
申请日：2001-09-19
申请人：マクドネル、ウィリアム・アールMCDONNELL,William,R.
发明人：マクドネル、ウィリアム・アール
IPC分类号： B60N2/34 , A47C17/04 , B64D11/06 , B64D25/04
CPC分类号： B64D11/0641 , B60N2/34 , B64D11/00153 , B64D11/0606 , Y02T50/46
摘要：容易且つ迅速に従来の座席から寝台へ、及びその逆の変換が可能な旅客設備。支持構造（９）が、座席パッド（１３）及び座席パッド拡張部（１５）を支持し、更に、背もたれ（５）を回転可能に支持する。この座席パッド拡張部（１５）及び背もたれ（５）は、変換可能な座席が寝台に変換された場合に、変換可能な座席の前にある座席列の支持構造（９）によって、部分的に支持される。第３の寝台（２１、２３）が、座席パッド（１３、１５）によって形成された下部の寝台の下に展開されてもよい。

6. 发明专利

JP2000505385A 失效
公开(公告)号：JP2000505385A
公开(公告)日：2000-05-09
申请号：JP52876997
申请日：1997-02-07
IPC分类号： B60N2/42 , B60N2/427 , B64D25/04

7. 发明专利

JPH0867191A SEAT 失效
公开(公告)号：JPH0867191A
公开(公告)日：1996-03-12
申请号：JP20509194
申请日：1994-08-30
申请人： MITSUBISHI HEAVY IND LTD
发明人： MIZUTANI SAORI
IPC分类号： B60N2/42 , B64D25/04
摘要： PURPOSE: To diverge a shock in landing and to provide no damage to the human body by providing a seat body having center of gravity at its rear rather than a revolving shaft, and means for fixing the seat body for preventing rotation and for releasing the fixing on acting force exceeding tolerance on the seat body. CONSTITUTION: A strain gage 7 is not necessarily installed on all seats. The seat bodies having no strain gage 7 receive a signal sent from a control pack 15. Igniting a blasting cap 13 releases a stopper bolt 5. Center of gravity then moves to the front of an airframe when force is applied from the rear of the airframe, resulting in rotating the seat body to give a backward state since the center of gravity of the seat body is backwardly located rather than a revolving shaft 4. Thus the seat body faces the force-applied direction, resulting in that a passenger constantly receives force with the entire back through a backrest 6b. In addition, a shock received from the airframe is diverged by rotating the seat body.

8. 发明专利

JPH07187087A SEAT UNDER FRAME 失效
公开(公告)号：JPH07187087A
公开(公告)日：1995-07-25
申请号：JP10006694
申请日：1994-05-13
申请人： SICMA AERO SEAT
发明人： RUNE MARUSHIYA ROBEERU
IPC分类号： B60N2/42 , B64D25/04
摘要： PURPOSE: To provide a seat underframe which can vary the amount of energy absorption without varying the relative positions, shapes and dimensions of components of the underframe itself. CONSTITUTION: This invention relates to a seat underframe for a passenger aircraft. The underframe includes at least one element forming a front leg, at least one element forming a rear leg, and energy absorption means 32 which is actuated when a movable part of the seat moves relative to other parts of the seat or the floor of a cabin with the seat subjected to deceleration above a predetermined value. The energy absorption means includes a male part which enters an aperture 2 in a female part when plastically deformed by a force, and either the female part or the male part is attached on and directly associated with the movable part, while the other part, i.e., the male part or the female part, is attached on and directly associated with the other parts of the seat or the floor.

9. 发明专利

JPH04215598A ANTI-G SEAT DEVICE 失效
公开(公告)号：JPH04215598A
公开(公告)日：1992-08-06
申请号：JP40166290
申请日：1990-12-12
申请人： MITSUBISHI HEAVY IND LTD
发明人： SANO HIROSHIGE
IPC分类号： B64D25/04
摘要： PURPOSE:To enhance the anti-G performance of a seat device used in the maneu vering system of an aircraft by determining the optimum amount of seat curva ture from a seat back curvature judging region preparation program made out on the basis of the individual acceleration environment medical data for the pilot concerned, the information about machine body motions, and the accel eration. CONSTITUTION:The individual acceleration environment medical data 25 for the pilot is fed to a computer 6, and a judgement critera 15 are prepared according to a judging region preparation program 16. When an aircraft is put in the flight state and a control rod 18 is pulled toward the pilot in order to apply a G, the angle amount is passed to a seat curvature determination program 13 as a control rod/stabilator command 1. The G generated is calculated presumatively from the attitude angle 2, altitude 4, speed 5, etc., fed from an inertia navigation device 3 and the acceleration 12. The result from calculation is fed to a servo valve 11 as a curvature command 10, and the oil pressure 20 is sent to a servo cylinder 8, and the back 19 of the seat 17 is curved with a least amount of curving which does not cause the pilot 7 to lose consciousness.

10. 发明专利

JPH01254496A SEAT DEVICE 失效
公开(公告)号：JPH01254496A
公开(公告)日：1989-10-11
申请号：JP8226288
申请日：1988-04-05
申请人： MITSUBISHI HEAVY IND LTD
发明人： INOUE KAZUO
IPC分类号： B60N2/48 , B60N2/90 , B64D25/04 , G09B9/10
摘要： PURPOSE:To facilitate holding of the head part of a pilot and to improve safety, by providing a head rest which is situated in a manner that it is movable from a seat body toward the head part of a pilot by an actuator by means of a signal from a heat part position detector. CONSTITUTION:When acceleration is generated through the maneuver of an aircraft, a signal from a differently mounted acceleration sensor 6 is outputted to a signal controller 7. In which case, the signal controller 7 outputs an output signal, responding to a distance between a pilot 1 and a head rest 3 obtained by a head part position detector 4, to a control valve 8. Working fluid is properly fed and discharged to and from an actuator 5 with the aid of actuating source 15 to move forward and backward the head rest 3. The head rest 3 is positioned right after the head part of the pilot 1 to hold this relation state. This constitution facilitates holding of the head part of the pilot 1 and enables improvement of safety, permits execution of accurate operation to sight a target during the maneuver of an aircraft, and allows sharp improvement of operation of an aircraft.

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