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1. 发明专利

JP2009279174A Walking aid device 有权
标题翻译：行车辅助设备
公开(公告)号：JP2009279174A
公开(公告)日：2009-12-03
申请号：JP2008134085
申请日：2008-05-22
申请人： Honda Motor Co Ltd , 本田技研工業株式会社
发明人： ASHIHARA ATSUSHI , IKEUCHI YASUSHI , FUJIHIRA TORU , NISHIMURA YOICHI , KUDO HIROSHI , HIMOKU YUTAKA , SHISHIDO MAKOTO , NODA TATSUYA , MATSUDA HIROSHI , MATSUOKA YOSHIHISA , YOKOYAMA RYUZO , NINOMIYA EIJI , KOSHIISHI TAKESHI
IPC分类号： A61H3/00
CPC分类号： A61H3/008 , A47C9/025 , A61H3/00 , A61H2201/1215 , A61H2201/1436 , A61H2201/1633 , A61H2201/1642 , A61H2201/165 , A61H2201/1676 , A61H2201/5061 , A61H2201/5071 , B25J9/0006
摘要： PROBLEM TO BE SOLVED: To permit a user to sit on a sitting member and rest without straining the legs in an walking aid device with the sitting member 1 for the user P to sit on astride, a leg link 2 connected to the sitting member and having a joint portion 5 in the middle, and a driving source 9 driving the joint portion. SOLUTION: The walking aid device has a locking mechanism 14 locking the joint portion 5 of the leg link 2, and an operating means 15 to operate the locking mechanism 14. When an operating switch 15a forming the operating means 15 is turned on, the driving source 9 is controlled so as to increase the jacking-up power of the sitting member 1 with the amount of descent of the sitting member 1 and the rate of change of the jacking-up power of the sitting member 1 with respect to the amount of descent of the sitting member 1 is controlled so as to increase over time. When the rate of change is increased to a prescribed value, the locking mechanism 14 is operated. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：为了允许用户坐在坐着的人身上并休息，而不会使腿部在步行辅助装置中受伤，座位构件1用于使用者P跨越，一个腿连杆2连接到并且在中间具有接合部分5，以及驱动接合部分的驱动源9。解决方案：助行器具具有锁定腿部连杆2的接合部分5的锁定机构14和操作装置15以操作锁定机构14.当形成操作装置15的操作开关15a被打开时，驱动源9被控制，以便随着座位构件1的下降量和座椅构件1的上升功率的变化率相对于座椅构件1的上升功率的增加而增加了座位构件1的顶起力控制座椅构件1的下降量随着时间的推移而增加。当变化率增加到规定值时，操作锁定机构14。版权所有（C）2010，JPO＆INPIT

2. 发明专利

JP2009279173A Walking aid device 有权
标题翻译：行车辅助设备
公开(公告)号：JP2009279173A
公开(公告)日：2009-12-03
申请号：JP2008134084
申请日：2008-05-22
申请人： Honda Motor Co Ltd , 本田技研工業株式会社
发明人： IKEUCHI YASUSHI , ASHIHARA ATSUSHI , FUJIHIRA TORU , NISHIMURA YOICHI , KUDO HIROSHI , HIMOKU YUTAKA , SHISHIDO MAKOTO , NODA TATSUYA , MATSUDA HIROSHI , MATSUOKA YOSHIHISA , YOKOYAMA RYUZO , NINOMIYA EIJI , KOSHIISHI TAKESHI
IPC分类号： A61H3/00
摘要： PROBLEM TO BE SOLVED: To use a walking aid device in common as a chair, which is provided with a sitting member 1 for a user P to sit on like straddling, a leg link 2 connected to the sitting member 1 and having a joint part 5 in the middle, and a drive source 9 for driving the joint part, and allows the leg link in the direction of pushing the sitting member upward by driving of the joint part by the drive source so that at least a part of the weight of the user is supported by the leg link via the sitting member. SOLUTION: A support member 14 which can come into contact with a wall W is installed to the sitting member 1. When the support member 14 comes into contact with the wall W, the drive source 9 is controlled so as to strengthen the pushing-up force of the sitting member 1 according to the lowering amount of the sitting member 1, and the ratio of the change of the pushing-up force of the sitting member 1 to the lowering amount of the sitting member 1 is controlled to increase with time. When the ratio of the change increases to a predetermined value, the joint part 5 is locked. COPYRIGHT: (C)2010,JPO&INPIT
摘要翻译：要解决的问题：为了使用作为椅子的步行辅助装置，其具有用于使用者P坐在一起的座椅的坐姿构件1，连接到坐姿构件1的腿连杆2并具有中间的接合部5和用于驱动接合部的驱动源9，并且通过驱动源的接合部的驱动使座椅向上推动座椅的方向的腿连杆，使得至少一部分用户的重量通过座椅构件由腿部连杆支撑。解决方案：可将与壁W接触的支撑构件14安装在座椅构件1上。当支撑构件14与壁W接触时，控制驱动源9以便加强坐姿构件1根据座位构件1的下降量的上推力，坐姿构件1的上推力的变化与坐下构件1的下降量的比例被控制为增加随着时间的推移。当变化率增加到预定值时，接合部分5被锁定。版权所有（C）2010，JPO＆INPIT

3. 发明专利

JPH06255587A AIRCRAFT 失效
公开(公告)号：JPH06255587A
公开(公告)日：1994-09-13
申请号：JP4826593
申请日：1993-03-09
申请人： HONDA MOTOR CO LTD
发明人： INOUE KAZUO , FUJINO MICHITADA , OTSUKA HIRONARI , FUJIHIRA TORU
IPC分类号： B64C1/00 , B64C1/06 , B64C1/26 , B64C25/00
摘要： PURPOSE:To improve the boarding-alighting performance of a crew and passengers, the loading-unloading performance of cargo, the comfortableness of a cabin, and the like respectively in an aircraft with primary structural members formed of composite material by forming main wings into forward wings on the basis of the constitution without a canard. CONSTITUTION:The primary part of an aircraft 1 is formed of forward main wings 3 fitted with a sweep-forward angle to a fuselage 2, a vertical tail fitted to the rear part of the fuselage 2, and a horizontal tail 5 fitted to the upper part of the vertical tail 4. The main wings 3 are disposed in the high-wing state, and plural engines 6 are mounted to the root upper parts of the right and left wings 3. The fuselage 2 is largely divided into the sections 7-9 of a nose, a cabin and an after fuselage from the front, and a nose gear 11 and a pair of main gears 12 are disposed thereunder. The main gears 12 are formed to be short-legged. The form of forward wings is thus adopted to the main wings in the aircraft of short-legged high-wing layout, and fuselage-wing connecting parts are disposed behind the cabin.

4. 发明专利

JP2001293738A METHOD FOR MANUFACTURING STRUCTURE MADE OF COMPOSITE MATERIAL AND STRUCTURE MADE OF COMPOSITE MATERIAL MANUFACTURED THEREBY 失效
公开(公告)号：JP2001293738A
公开(公告)日：2001-10-23
申请号：JP2000113439
申请日：2000-04-14
申请人： HONDA MOTOR CO LTD
发明人： FUJIHIRA TORU
IPC分类号： B64C1/12 , B29C43/18 , B29C70/34 , B29L31/30
摘要： PROBLEM TO BE SOLVED: To provide a method for manufacturing a structure made of a composite material constitued of a three-dimensional curved surface part and a cylindrical part, capable of achieving the weight reduction and cost reduction of a product, and the structure made of the composite material manufactured by this method. SOLUTION: In the method for manufacturing the structure made of the composite material constituted of the three-dimensional curved part and the cylindrical part, (a) an outside skin comprising a composite material prepreg is laid on a mold and (b) a honeycomb core is placed on the part forming the three-dimensional curved part of the outside skin and (c) an inside skin comprising the composite material prepreg is superposed on the honeycomb and (d) a preformed stringer member and a preformed frame member both of which comprise the composite material prepreg are arranged on the part forming a cylindrical part of the inside skin and (e) these member are molded under heating and pressure.

5. 发明专利

JPH05286493A 失效
公开(公告)号：JPH05286493A
公开(公告)日：1993-11-02
申请号：JP11431392
申请日：1992-04-08
申请人： HONDA MOTOR CO LTD
发明人： MATSUO SHIRO , FUJIHIRA TORU
IPC分类号： B64C1/08
摘要： PURPOSE:To reduce the number of parts and weight and improve assembly performance by installing a strip shaped joint member for joining each fuselage section and a fixing means for fixing the strip shaped joint member on the fuselage section and allowing the joint position of each fuselage section to nearly coincide with the position of a partitioning wall structure, with respect to the machine axis direction. CONSTITUTION:A fuselage 1 consists of three sectional divided bodies: nose part 6, cabin part 7, and an aft part 8, and the pressure partitioning walls 12 and 13 are arranged before and behind the cabin part 7. The nose part 6 and the cabin part 7 are abutted, and the cabin part 7 and the aft part 8 are similarly abutted, and strip shaped joint members 15 and 15 are wound on the periphery of both the edge surfaces of the joint part. Each strip shaped joint member 15 is half divided and consists of the upper part strap 15a and the lower part strap 15b, and fixed from the above and the below. Further, the position of the strip shaped joint member 15 is the same position for the pressure partitioning wall 12 at the front and the position of the pressure partitioning wall 13 at the rear, and stepped parts 16 and 16 are formed on the outer skin member 14 of the edge surface of the joint part, and fixed by an adhesive.

6. 发明专利

JPH08174726A SHOCK-ABSORBING STRUCTURE 失效
公开(公告)号：JPH08174726A
公开(公告)日：1996-07-09
申请号：JP32310194
申请日：1994-12-26
申请人： HONDA MOTOR CO LTD
发明人： YOSHIZAKI YUICHI , FUJIHIRA TORU
IPC分类号： B64C1/18 , B29C70/10 , B32B3/12 , B32B5/00 , B32B27/04 , F16F7/12
摘要： PURPOSE: To provide a shock-absorbing structure effective for reducing esp. a peak load when an impact load is applied to, for example, a structure under a floor of an airplane. CONSTITUTION: In a part under a floor of an airplane, a keel 1 extending crosswise and a rib 2 extending longitudinally are made of a fiber-reinforced plastic and crossed at a crossed part 3, and a notch 5 and bulge parts 6 are formed on the upper end of the rib 2 corresponding to the crossed part 3. The bulge part 6 is shaped into a circle or a long ellipse having a minor axis in the direction of a load. The notch 5 and the bulge parts 6 can be provided in the keel 1.

7. 发明专利

JPH05286496A 失效
公开(公告)号：JPH05286496A
公开(公告)日：1993-11-02
申请号：JP11431292
申请日：1992-04-08
申请人： HONDA MOTOR CO LTD
发明人： MATSUI NOBUO , IDE TOSHIHARU , FUJIHIRA TORU
IPC分类号： B64C3/18 , B29C65/00 , B29C65/50 , B64C1/26
摘要： PURPOSE:To facilitate assembly and reduce weight and improve torsional rigidity by allowing a wing spar and a rib to be equipped with a web part and a joint flange part and joining the joint flange part of the wing spar and the joint flange part of the rib by a joint member. CONSTITUTION:At the king part K of the longitudinal web part, 12w of a wing spar 12, joint flange parts 12f and 12f are installed, and the upper and lower parts of the longitudinal web part 15w on a rib 15 side are formed to the joint flange parts 15f and 15f. Joint is performed by an obverse side joint member 17 and a reverse side joint member 18 which are attached on the obverse and reverse surfaces of the flange surface of both the joint flange parts 12f and 15f. The reverse side joint member 18 fits the reverse surfaces of the joint flange parts 12f and 15f on both the sides by nipping the web part 15w. An obverse side joint member 17 does not project to the outer surface because of the step differences (m) and (n). The web parts 12w and 15w are joined even by an L figure-shaped metal fitting 20. Accordingly, the reaction forces generated on the wing spars 12 and 13 are transmitted to the rib 15 through the joint members 17 and 18, and torsional rigidity is increased.

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