-
公开(公告)号:AU2003257607A1
公开(公告)日:2005-03-29
申请号:AU2003257607
申请日:2003-08-29
Applicant: KAWADA KOGYO KK , NAT AEROSPACE LAB
Inventor: SAITO SHIGERU , KOBIKI NOBORU , TANABE YASUTADA , AKASAKA TSUYOSHI
IPC: B64C27/00 , B64C27/473 , B64C27/615 , B64C5/10
-
公开(公告)号:DE60006044T2
公开(公告)日:2004-07-08
申请号:DE60006044
申请日:2000-07-26
Applicant: TOYOTA MOTOR CO LTD , KAWADA KOGYO KK
Inventor: UEHARA YASUO , TANABE YASUTADA , SUZUKI TOSHIAKI
-
公开(公告)号:DE60006044D1
公开(公告)日:2003-11-27
申请号:DE60006044
申请日:2000-07-26
Applicant: TOYOTA MOTOR CO LTD , KAWADA KOGYO KK
Inventor: UEHARA YASUO , TANABE YASUTADA , SUZUKI TOSHIAKI
-
公开(公告)号:EP1666355A4
公开(公告)日:2010-11-03
申请号:EP03818545
申请日:2003-08-29
Applicant: KAWADA KOGYO KK , JAPAN AEROSPACE EXPLORATION
Inventor: TANABE YASUTADA , AKASAKA TAKESHI , SAITO SHIGERU , KOBIKI NOBORU
IPC: B64C27/473 , B64C5/10 , B64C27/00 , B64C27/615
CPC classification number: B64C27/001 , B64C27/473 , B64C27/615 , B64C2027/7266 , B64C2027/7277 , Y02T50/34
-
公开(公告)号:EP1666356A4
公开(公告)日:2011-12-28
申请号:EP04732435
申请日:2004-05-12
Applicant: KAWADA KOGYO KK
Inventor: TANABE YASUTADA , TOTSUKA CHIHARU , AKASAKA TSUYOSHI , OKAMOTO MASATO
CPC classification number: A63H27/02 , B64C39/028 , B64C39/10 , B64C2201/028 , B64C2201/141 , B64C2201/146 , B64C2201/165 , Y10S244/903
-
公开(公告)号:JP2004024299A
公开(公告)日:2004-01-29
申请号:JP2002181164
申请日:2002-06-21
Applicant: Kawada Kogyo Kk , 川田工業株式会社
Inventor: TANABE HIROSHI , TOKUNAGA SHIYOUKAN , TANABE YASUTADA
Abstract: PROBLEM TO BE SOLVED: To suppress output of an actuator low even in the case that maximum rocking angle is relatively large. SOLUTION: A motion base for rocking a seat 2 for a person comprises a placement based 1, a movable base 3 for loading the seat 2, a support member 4 which is placed on the placement base 1 and supports the movable base 3 capable of swinging around two rocking axes A1, A2 passing below a gravity center position G of an assembly of the seat 2 a person is sitting and the movable base 3 and crossing perpendicularly to each other. Also it comprises motor driven actuators 6, 7 for rocking the movable base 3 against the placement base 1 around the rocking axes A1, A2, and tension coil springs 10 to 17 put in between the movable base 3 and the placement base 1 and opposing to a moment increasing according to the rocking of the movable base 3 around the rocking axes A1, A2. COPYRIGHT: (C)2004,JPO
-
公开(公告)号:JP2001191995A
公开(公告)日:2001-07-17
申请号:JP2000001685
申请日:2000-01-07
Applicant: KAWADA KOGYO KK , NAT AEROSPACE LAB
Inventor: TANABE YASUTADA , SAITO SHIGERU
IPC: B64C27/72 , B64C27/467 , H02N2/00 , H02P9/00
Abstract: PROBLEM TO BE SOLVED: To reduce the BVI noise of a helicopter effectively. SOLUTION: For reducing the BVI noise of the rotor blades 2 of the helicopter, a spoiler 3 capable of being reciprocated nearly in the vertical direction between a protruded position and an unprotruded position from the upper face and the lower face of each rotor blade 2 is provided between the front edge and the rear edge of the rotor blade 2. An actuator 4 reciprocating the spoiler 3 is provided for each spoiler 3 on a rotor system 1 including the rotor blades 2 and rotated relative to the airframe of the helicopter, and the actuator 4 is operated to reciprocate the spoiler 3 in response to the rotation timing or frequency of the rotor blade 2.
-
公开(公告)号:JP2005067398A
公开(公告)日:2005-03-17
申请号:JP2003299869
申请日:2003-08-25
Applicant: Kawada Kogyo Kk , Masato Okamoto , 正人 岡本 , 川田工業株式会社
Inventor: TANABE YASUTADA , TOTSUKA CHIHARU , AKASAKA TAKASHI , OKAMOTO MASATO
CPC classification number: A63H27/02 , B64C39/028 , B64C39/10 , B64C2201/028 , B64C2201/141 , B64C2201/146 , B64C2201/165 , Y10S244/903
Abstract: PROBLEM TO BE SOLVED: To realize miniaturization and light weight of a small pilotless plane suitable for hand throw staring or the like and portable by one person. SOLUTION: The small pilotless plane is provided with: all flying wing type main wing 1 being a camber wing type having an approximately flat lower surface, being thin toward a wing end in a tapered shape, having a wing front edge having a retreat angle and having a tailless type aerodynamincal surface of low aspect ratio; movable flaps 2 extending to both left and right sides at a rear edge part of the main wing over the approximately whole width and having a camber angle in at least horizontal flying; vertical stabilizer plates 3 arranged at both ends of the main wing; and two propellers 5 arranged on an upper surface of the main wing. COPYRIGHT: (C)2005,JPO&NCIPI
Abstract translation: 要解决的问题:实现适合于手扔等的便携式的小型无人驾驶飞机的小型化和轻量化。
解决方案:小型无人驾驶飞机设有:所有飞翼型主翼1是具有大致平坦的下表面的外倾翼型,朝向翼尖端呈锥形减薄,具有翼前边缘,其具有 具有低长宽比的无尾型气蚀表面; 在主翼翼的后边缘部分的大致整个宽度上延伸到左右两侧的活动翼片2和至少水平飞行的外倾角; 布置在主翼两端的垂直稳定板3; 以及布置在主翼的上表面上的两个螺旋桨5。 版权所有(C)2005,JPO&NCIPI
-
公开(公告)号:JP2002202820A
公开(公告)日:2002-07-19
申请号:JP2000399979
申请日:2000-12-28
Applicant: KAWADA KOGYO KK
Inventor: TANABE YASUTADA , SHIMADA TERUO
Abstract: PROBLEM TO BE SOLVED: To optionally set and vary characteristics of a reaction force applied to an input part. SOLUTION: This system is equipped with an actuator 1 which has a servomotor rotating a screw shaft of a ball screw mechanism and supplies a reaction force to the input part while displacing the input part by the relative movement between a screw shaft and a ball nut through the operation of the servomotor, a load cell 4d which outputs an external force signal showing the strength of the external force applied to the input part, a potentiometer 1g which outputs a position signal showing the position of the input part, a driver 2a which operates the servomotor so that the difference between a position command signal and the position signal is eliminated, a reaction force controller 2b which generates and outputs the position command signal according to the difference between the signal generated by adding a position signal made variable in value according to a reaction force/displacement gradient command signal, a speed signal found from the position signal through differentiation processing and made adjustable in value according to an attenuation factor command signal, and a stationary reaction force command signal and the external force signal, and a computer 3 which outputs the reaction force/displacement gradient command signal, the attenuation factor command signal, and stationary reaction force command signal according to arbitrary settings.
-
公开(公告)号:JP2004106602A
公开(公告)日:2004-04-08
申请号:JP2002268995
申请日:2002-09-13
Applicant: Kawada Kogyo Kk , 川田工業株式会社
Inventor: TANABE YASUTADA , SHIMADA TERUO
Abstract: PROBLEM TO BE SOLVED: To enhance reliability by reducing sensors which may cause trouble, and to make a control device inexpensive by simplifying the control.
SOLUTION: This base isolation device reduces vibration of a wheelchair 2 mounted on an automobile. The device is provided with a ball screw type electric base isolation mechanism 6 provided on a floor 1 of the automobile to vertically move the wheelchair 2 and having driving force suitable for weight of the wheelchair 2 and a sitting person, an acceleration sensor 11 for detecting upper and lower acceleration of the wheelchair 2, and a base isolation mechanism control device 12 to impart an acceleration signal from the acceleration sensor 11 as a position command signal to the base isolation mechanism 6 to cancel the vertical movement of the wheelchair 2 according to vertical movement of the floor 1 of the automobile.
COPYRIGHT: (C)2004,JPO
-
-
-
-
-
-
-
-
-