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1. 发明授权

US5597428A Method of sealing containers 失效
标题翻译：密封容器的方法
公开(公告)号：US5597428A
公开(公告)日：1997-01-28
申请号：US454408
申请日：1995-05-30
申请人： Tadahiro Matsumoto , Hiroyuki Takahashi , Kouzaburo Matsuzawa
发明人： Tadahiro Matsumoto , Hiroyuki Takahashi , Kouzaburo Matsuzawa
IPC分类号： B65B7/28 , B29C65/00 , B29C65/18 , B65B7/16
CPC分类号： B29C66/83411 , B29C65/18 , B29C66/0242 , B29C66/53461 , B29C66/73921 , B65B7/164 , B29C66/7394 , B29C66/81465
摘要： A method for and an apparatus of sealing containers are disclosed. Before causing thermal fusion of a thermoplastic resin sheet or film and a flange of a container, the flange and thermoplastic resin sheet or film and the flange are pre-heated by respective container and sheet material pre-heaters.
摘要翻译：公开了一种密封容器的方法和装置。在引起热塑性树脂片或膜与容器的凸缘的热熔融之前，凸缘和热塑性树脂片或膜和凸缘由相应的容器和片材预热器预热。

2. 发明申请

US20100062702A1 DEFROSTER NOZZLE 有权
标题翻译： DEFROSTER喷嘴
公开(公告)号：US20100062702A1
公开(公告)日：2010-03-11
申请号：US12530132
申请日：2008-02-21
申请人： Kazuhiro Ueda , Tadahiro Matsumoto , Takehiko Iwamura
发明人： Kazuhiro Ueda , Tadahiro Matsumoto , Takehiko Iwamura
IPC分类号： B60S1/54
CPC分类号： B60H1/3407 , B60H1/00564 , B60H1/242
摘要： Provided is a defroster nozzle 4 which blows out air to an inner surface of a windshield 2 of a vehicle 1. The defroster nozzle 4 includes center-duct 45 forming member 41 and two end-portion-duct forming members 50. The center-duct 45 forming member 41 forms a center duct through which the air circulates, and has a center ventilation outlet 47 through which the air in the center duct is blown out to the inner surface of the windshield 2. The two end-portion-duct 54 forming members 50 are coupled respectively to two joint end portions 42, on outer sides in the vehicle width direction, of the center-duct forming member 41. Each end-portion-duct forming member 50 forms an end-portion duct which communicates with the center duct, and each end-portion-duct forming member 50 has an end-portion ventilation outlet 55 through which the air in the end-portion duct is blown out to the inner surface of the windshield 2. Each of the end-portion-duct forming members 50 is coupled to the center-duct forming member 41 so as to be capable of tilting relative to the center-duct forming member 41.
摘要翻译：设有将空气吹出到车辆1的挡风玻璃2的内表面的除霜喷嘴4.除霜器喷嘴4包括中心管45形成部件41和两个端部部分导管形成部件50.中心管 45形成构件41形成空气循环的中心管道，并且具有中心通风出口47，中心管道中的空气通过该中心通风出口吹送到挡风玻璃2的内表面。两个端部管道54形成构件50分别连接到中心管形成构件41的车宽方向的外侧的两个接合端部42.每个端部管道形成构件50形成与中心管道形成构件41连通的端部管道每个端部管道形成构件50具有端部通风出口55，端部管道中的空气通过该端部通风出口55吹送到挡风玻璃2的内表面。每个端部管道成形构件50联接到中心管形成构件41能够相对于中心管形成构件41倾斜。

3. 发明授权

US06513230B2 Coil apparatus and manufacturing method for the same 有权
公开(公告)号：US06513230B2
公开(公告)日：2003-02-04
申请号：US09885883
申请日：2001-06-20
申请人： Keiji Inoue , Jun Nagai , Tadahiro Matsumoto
发明人： Keiji Inoue , Jun Nagai , Tadahiro Matsumoto
IPC分类号： H01F706
CPC分类号： H01F27/263 , H01F27/2804 , Y10T29/4902 , Y10T29/49073 , Y10T29/4913
摘要： A core-coupling unit includes a top cover and a bottom cover each having a U-shape. The core-coupling unit clamps a pair of core members in a coupled state with the top cover and the bottom cover being coupled with each other. The top cover is provided with apertures formed in respective legs of the top cover, and the bottom cover is provided with projections formed on respective legs of the bottom cover, the projections mating with the apertures so as to prevent removal. Play-gaps are provided between each projection and respective front and rear edges of the aperture. Lips are provided on the covers for maintaining the positions of the core members in the backward and forward directions. The top and bottom covers are moved backward and forward relative to each other while the core members are clamped, whereby the core members are moved together with the respective top and bottom covers, thereby performing core-rubbing.

4. 发明授权

US08795042B2 Defroster nozzle 有权
标题翻译：除霜喷嘴
公开(公告)号：US08795042B2
公开(公告)日：2014-08-05
申请号：US12530132
申请日：2008-02-21
申请人： Kazuhiro Ueda , Tadahiro Matsumoto , Takehiko Iwamura
发明人： Kazuhiro Ueda , Tadahiro Matsumoto , Takehiko Iwamura
IPC分类号： B60H1/00 , B60H1/34 , B60S1/54
CPC分类号： B60H1/3407 , B60H1/00564 , B60H1/242
摘要： Provided is a defroster nozzle 4 which blows out air to an inner surface of a windshield 2 of a vehicle 1. The defroster nozzle 4 includes center-duct 45 forming member 41 and two end-portion-duct forming members 50. The center-duct 45 forming member 41 forms a center duct through which the air circulates, and has a center ventilation outlet 47 through which the air in the center duct is blown out to the inner surface of the windshield 2. The two end-portion-duct 54 forming members 50 are coupled respectively to two joint end portions 42, on outer sides in the vehicle width direction, of the center-duct forming member 41. Each end-portion-duct forming member 50 forms an end-portion duct which communicates with the center duct, and each end-portion-duct forming member 50 has an end-portion ventilation outlet 55 through which the air in the end-portion duct is blown out to the inner surface of the windshield 2. Each of the end-portion-duct forming members 50 is coupled to the center-duct forming member 41 so as to be capable of tilting relative to the center-duct forming member 41.
摘要翻译：设置有将空气吹送到车辆1的挡风玻璃2的内表面的除霜喷嘴4.除霜器喷嘴4包括中心管45形成部件41和两个端部部分导管形成部件50.中心管 45形成构件41形成空气循环的中心管道，并且具有中心通风出口47，中心管道中的空气通过该中心通风出口吹送到挡风玻璃2的内表面。两个端部管道54形成构件50分别连接到中心管形成构件41的车宽方向的外侧的两个接合端部42.每个端部管道形成构件50形成与中心管道形成构件41连通的端部管道每个端部管道形成构件50具有端部通风出口55，端部管道中的空气通过该端部通风出口55吹送到挡风玻璃2的内表面。每个端部管道成形构件50联接到中心管形成构件41能够相对于中心管形成构件41倾斜。

5. 发明授权

US5047106A Method for fabricating a flexbeam of a helicopter rotor blade 失效
标题翻译：制造直升机转子叶片柔性梁的方法
公开(公告)号：US5047106A
公开(公告)日：1991-09-10
申请号：US422222
申请日：1989-10-16
申请人： Tadahiro Matsumoto , Kiyoshi Nishikawa
发明人： Tadahiro Matsumoto , Kiyoshi Nishikawa
IPC分类号： B64C27/35 , B29C70/34 , B29D99/00 , B64C27/33
CPC分类号： B29D99/0025 , B29C70/345 , B64C27/33
摘要： A flexbeam for rotor blades of a helicopter comprises a flapping flexible structure forming a mast mounting and flapping part, a flexible structure forming a feathering and lead-lag motion part coupled with the flapping flexible structure, and a rotor blade mounting part located at the free end of the flexible structure and adapted to be coupled with a rotor blade. The feathering and lead-lag motion part comprises an elongated central member made of a composite fiber material, and a pair of elongated frame members disposed along the longitudinal sides of the central member. The frame members are each made of loops of unidirectional composite fiber material and has a Y-shaped cross section. The feathering and lead-lag motion part is fabricated by integrally joining the central member and the frame members along the longitudinal sides of the latter. The Y-shaped cross section has a pair of parallel ribs extending away from the central member. The above construction enables easy fabrication and reduction of weight of the flexbeam.

6. 发明授权

US5927755A Knee bolster structure 失效
标题翻译：膝关节结构
公开(公告)号：US5927755A
公开(公告)日：1999-07-27
申请号：US16270
申请日：1998-01-30
申请人： Shigeki Matsuo , Tadahiro Matsumoto , Hiroyuki Nagae , Yoshiharu Sonoda
发明人： Shigeki Matsuo , Tadahiro Matsumoto , Hiroyuki Nagae , Yoshiharu Sonoda
IPC分类号： B60R21/045 , B60R21/04
CPC分类号： B60R21/045
摘要： The knee bolster structure to be mounted on an instrument panel 13 comprises a panel 2 and a stay 3 for supporting the panel 2, while the stay 3 is composed of a stay main body 4 and patch 5 so disposed on the stay main body 4 as to cover the stay main body 4. In a vehicle collision, the stay 3 is deformed starting from notches 8 respectively formed in the stay main body 4 but, during the deformation of the stay 3, the leading end side 11 of a top plate 9 provided in the patch 5 is butted against the bottom surface 6 of the stay main body 4, thereby being able to prevent stresses from being concentrated onto the notches 8. Also, since the wall portions 7 of the stay main body 4 are held by the side walls 10 of the patch 5, they are prevented from being opened outwardly. Due to this structure, the drag of the stay 3 or the knee bolster structure can be stabilized, so that shock energy caused in the vehicle collision can be absorbed efficiently.
摘要翻译：要安装在仪表板13上的膝垫结构包括面板2和用于支撑面板2的撑杆3，而支柱3由搁置主体4和如此设置在支撑主体4上的贴片5组成，在车辆碰撞中，轿厢3从分别形成在拉杆主体4上的切口8开始变形，但是在拉杆3的变形期间，顶板9的前端侧11 在贴片5上设置有与支柱主体4的底面6抵接的结构，能够防止应力集中在凹口8上。此外，由于保持箱主体4的壁部7由补片5的侧壁10，防止其向外打开。由于这种结构，可以使撑杆3或膝垫结构的阻力稳定，从而能够有效地吸收车辆碰撞引起的冲击能。

7. 发明授权

US5820157A Air bag mounting in a vehicle 失效
标题翻译：气囊安装在车内
公开(公告)号：US5820157A
公开(公告)日：1998-10-13
申请号：US679150
申请日：1996-07-12
申请人： Tadahiro Matsumoto
发明人： Tadahiro Matsumoto
IPC分类号： B60K37/00 , B60R21/20 , B60R21/205 , B60R21/217 , B60R21/16
CPC分类号： B60R21/205
摘要： An instrument panel 1 has opening 2 formed therein for accommodating an air bag mounting for a vehicle. The vehicle air bag, and a structure element 4 is provided in the inside of the opening. A mount portion 9 of an air bag unit 6 is fixed to a bracket 5 of the structure element 4 with bolts 10. The air bag unit 6 has mount portions 8 at its opposite sides, at which the air bag unit 6 is fixed with bolts 18 to brackets 13 mounted at opposite sides of the opening 2. The brackets 13 are made of steel plate, and have upper and lower ends connected to the instrument panel with screws 14 via reinforcing bosses 15 or reinforcing elements 12.
摘要翻译：仪表板1在其中形成有用于容纳用于车辆的气囊安装的开口2。车辆安全气囊和结构元件4设置在开口的内部。气囊单元6的安装部9用螺栓10固定在结构体4的支架5上。气囊单元6的相对侧具有安装部8，气囊单元6用螺栓固定 18到安装在开口2的相对侧的托架13.支架13由钢板制成，并且上端和下端通过加强凸台15或加强元件12用螺钉14连接到仪表板。

8. 发明授权

US5301885A Method and apparatus for fabricating unidirectional materials for helicopter parts 失效
标题翻译：制造用于直升机部件的单向材料的方法和装置
公开(公告)号：US5301885A
公开(公告)日：1994-04-12
申请号：US633958
申请日：1990-12-26
申请人： Tadahiro Matsumoto
发明人： Tadahiro Matsumoto
IPC分类号： B64C27/35 , B29C53/58 , B29C70/16 , B29C70/34 , B29L31/08 , B64C27/46 , B64C27/473 , B65H54/64
CPC分类号： B64C27/473 , B29C53/587 , B29C70/347 , B29L2031/3088 , B64C2027/4736
摘要： A unidirectional material for helicopter parts is fabricated by winding a composite-material roving delivered from a feeding mechanism of a filament winding device around and between a plurality of pins provided on a mandrel rotating about the longitudinal axis thereof, the roving feeding mechanism being moved in a traversing manner such that the feeding path of the roving becomes a figure eight figure, whereby the roving is thus wound to form a tubular mesh of obliquely crossing and staggered helixes of the roving around the mandrel. The material has an improved strength in a transverse direction of the mandrel.
摘要翻译：用于直升机部件的单向材料通过缠绕从细丝缠绕装置的进给机构传送的复合材料粗纱围绕设置在围绕其纵向轴线旋转的心轴上的多个销之间和之间缠绕，粗纱进给机构被移动使得粗纱的进给路径成为图8的横移方式，由此粗纱被卷绕形成围绕心轴的粗纱的斜交和交错的螺旋形的管状网。该材料在心轴的横向具有改进的强度。

9. 发明授权

US4892461A Flexbeam for rotor blades of helicopter and method for fabrication thereof 失效
标题翻译：直升机转子叶片的挠性梁及其制造方法
公开(公告)号：US4892461A
公开(公告)日：1990-01-09
申请号：US294259
申请日：1989-01-05
申请人： Tadahiro Matsumoto , Kiyoshi Nishikawa
发明人： Tadahiro Matsumoto , Kiyoshi Nishikawa
IPC分类号： B64C27/35 , B29C70/34 , B29D99/00 , B64C27/33
CPC分类号： B29D99/0025 , B29C70/345 , B64C27/33
摘要： A flexbeam for rotor blades of a helicopter comprises a flapping flexible structure forming a mast mounting and flapping part, a flexible structure forming a feathering and lead-lag motion part coupled with the flapping flexible structure, and a rotor blade mounting part located at the free end of the flexible structure and adapted to be coupled with a rotor blade. The feathering and lead-lag motion part comprises an elongated central member made of a composite fiber material, and a pair of elongated frame members disposed along the longitudinal sides of the central member. The frame members are each made of loops of unidirectional composite fiber material and has a Y-shaped cross section. The feathering and lead-lag motion part is fabricated by integrally joining the central member and the frame members along the longitudinal sides of the latter. The Y-shaped cross section has a pair of parallel ribs extending away from the central member. The above construction enables easy fabrication and reduction of weight of the flexbeam.

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