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1. 发明专利

JP2012096588A Seat structure for aircraft 审中-公开
标题翻译：飞机座椅结构
公开(公告)号：JP2012096588A
公开(公告)日：2012-05-24
申请号：JP2010243923
申请日：2010-10-29
申请人： Toyota Motor Corp , トヨタ自動車株式会社
发明人： UEGAKI KENJI
IPC分类号： B64D25/02 , B64C1/12
摘要： PROBLEM TO BE SOLVED: To provide a seat structure for an aircraft that can achieve proper impact absorption even if the aircraft has a narrow interior cabin.SOLUTION: Regarding a small fixed-wing tractor-aircraft, impact absorbers 30-32 lining up in two lines at both sides of a fuselage around areas from a front side of a fire wall 40 to a backward side of a rear seat 22 are arranged. The impact absorbers 30-32 are connected to a main frame 50 of the fuselage via load transmission members 60-62 connected to an outer fuselage 70. A fairing 55 is provided over the impact absorbers 30-32 on a lower surface of the fuselage, where a surface layer structured to be worn out or fallen away at the time of impact is serially formed.
摘要翻译：要解决的问题：即使飞机具有狭窄的内部舱室，也可提供能够实现适当冲击吸收的飞机座椅结构。
解决方案：关于小型固定翼拖拉机，冲击吸收器30-32在机身两侧排列成两排，从防火墙40的前侧到后座的后侧 22排列。冲击吸收器30-32通过连接到外部机身70的负载传递构件60-62连接到机身的主框架50.整流罩55设置在机身下表面上的冲击吸收器30-32之上，其中构造成在冲击时被磨损或掉落的表面层被顺序地形成。版权所有（C）2012，JPO＆INPIT

2. 发明专利

JP3052368B2 失效
公开(公告)号：JP3052368B2
公开(公告)日：2000-06-12
申请号：JP29306890
申请日：1990-10-29
IPC分类号： B64D10/00 , B64D25/02

3. 发明专利

JP2577260B2 失效
公开(公告)号：JP2577260B2
公开(公告)日：1997-01-29
申请号：JP25170189
申请日：1989-09-27
申请人： ROCKWELL INTERNATIONAL CORP
发明人： UIRIAMU JEI ADAMUZU , ROBAATO II ZEGURAA , KONRATSUDO BII MONSON
IPC分类号： B60R21/12 , B64D25/02 , B64D25/06 , B64D25/10

5. 发明专利

JP5403148B2 Aircraft seat part structure 有权
公开(公告)号：JP5403148B2
公开(公告)日：2014-01-29
申请号：JP2012504251
申请日：2010-03-12
申请人：トヨタ自動車株式会社
发明人：賢治上柿
IPC分类号： B64D11/06 , B64D25/02 , F16F7/08 , F16F7/12
CPC分类号： B64D11/0689 , B60N2/24 , B60N2/4242 , B60N2/42709 , B60N2/42736 , B64D11/0619 , Y02T50/46

6. 发明专利

JPWO2011111226A1 航空機座席部構造有权
公开(公告)号：JPWO2011111226A1
公开(公告)日：2013-06-27
申请号：JP2012504251
申请日：2010-03-12
申请人：トヨタ自動車株式会社
发明人：上柿　賢治 , 賢治上柿
IPC分类号： B64D11/06 , B64D25/02 , F16F7/08 , F16F7/12
CPC分类号： B64D11/0689 , B60N2/24 , B60N2/4242 , B60N2/42709 , B60N2/42736 , B64D11/0619 , Y02T50/46
摘要：本発明は、室内空間の狭い航空機においても適切な衝撃吸収ストロークを確保することを可能とした航空機の座席部構造を提供することを課題としている。乗員51が搭乗する座席50を含む乗員スペースを機体下部側から取り囲む乗員保護部材であるサバイバルタブ1を配置し、好ましくは、衝撃時には、これが機体上方側へと移動可能となるようリンク機構4、5、衝撃吸収作動部9により保持している。

7. 发明专利

JPH0663167A BALLOON TYPE LIFE-SAVING DEVICE 失效
公开(公告)号：JPH0663167A
公开(公告)日：1994-03-08
申请号：JP22981091
申请日：1991-06-04
申请人： SHIOIRI HIROSHI
发明人： SHIOIRI HIROSHI
IPC分类号： A62B1/00 , B64D17/00 , B64D25/02
摘要： PURPOSE:To accommodate a person in a balloon for life-saving, sport, business or the like by incorporating inner and outer bladders in a balloon and by defining a space for accommodating a person, in the inner bladder. CONSTITUTION:A balloon incorporates an inner bladder 2, an outer bladder 3 and a accommodation chamber 4 for an escaping victim or the like defined in the inner bladder 2. The inner bladder 2 is formed of more than one layer of balloon shape membrane members at the innermost side of the balloon, and the accommodation chamber 4 is defined in the inside of the inner bladder 2. The outer bladder 3 is formed of more than one layer of membrane members and an air space defined between these membrane members and the outer periphery of the inner bladder 2. The accommodation chamber 4 defined in the inside of the bladder 2 is formed of membrane members joined to the membrane members constituting the inner bladder 2, and is recessed into the inner bladder 2 from an entrance for the chamber. Further, means for forcibly forming and holding the shape of the accommodation chamber 4 is provided between the outermost one of the membrane members forming the accommodation chamber and the innermost one of the membrane members forming the inner bladder 2.

8. 发明专利

JPH04224437A PROTECTION DEVICE FOR AIRPLANE PASSENGER 失效
公开(公告)号：JPH04224437A
公开(公告)日：1992-08-13
申请号：JP40671690
申请日：1990-12-26
申请人： MITSUBISHI HEAVY IND LTD
发明人： OKANO MASAAKI
IPC分类号： B60R21/16 , B64D25/02
摘要： PURPOSE:To protect an airplane passenger surely in the event of crash and the like by forming an air bag, which is inflatable to fill the inside of the airplane, from a plurality of sack-shaped films in continuity up and down and to the left and light, and inflating this air bag through delivery of air when any abnormality of the plane body is sensed. CONSTITUTION:The condition of an airplane is judged by a control device on the basis of information concerning the state of plane body given from a sensor, and when any danger exists, an appropriate signal is sent to an air feeding/discharging device 2. Now this device 2 begins feeding the air into an air bag 1. The air bag 1 is inflated from below in sequence. Air blows out from small hole provided at the outer extreme of the air bag 1, and thereby passenger is supplied with air and also the pressure is adjusted. When control device 3 senses that the plane body has stopped due to landing on the ground or water, a discharge signal is sent to the air feeding/charging device 2 to perform air discharge, and the air bag 1 is shrunk quickly.

9. 实用新型

JPS59143857U JPS59143857U - 失效
公开(公告)号：JPS59143857U
公开(公告)日：1984-09-26
申请号：JP3763383
申请日：1983-03-16
IPC分类号： B60R22/48 , B60Q1/50 , B60Q9/00 , B64D25/02 , B64D25/06 , B60R21/10

10. 实用新型

JPS5043437U 失效
公开(公告)号：JPS5043437U
公开(公告)日：1975-05-01
申请号：JP9882173
申请日：1973-08-22
IPC分类号： B60R22/26 , A62B35/00 , B60N2/06 , B60N2/20 , B60N2/42 , B60N2/90 , B64D25/02 , B60R21/10

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