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公开(公告)号:JPH01204900A
公开(公告)日:1989-08-17
申请号:JP3009488
申请日:1988-02-12
Applicant: NAT AEROSPACE LAB
Inventor: NITTA KEIJI , AZUMA HISAO , OTSUBO KOJI , OGUCHI MITSUO , TANEMURA TOSHIHARU , NAKAJIMA ATSUSHI , NAKAMURA YOSHIHIRO , YOSHIMURA SHOICHI , INOUE YASUTOSHI , MATSUMOTO KOTARO , KIBE SEISHIROU , FUJIMORI YOSHINORI , EGUCHI KUNIHISA
Abstract: PURPOSE:To make a spacecraft platform constructible as one structural body without giving any adverse effect on environmental conditions in both elements by connecting the rotating element at the outside to the nonrotating element at the inside through magnetic force in a noncontact state. CONSTITUTION:A spacecraft platform is constituted of a nonrotating element 1 at a central part capable of offering microgravity for space environmental utilization such as the rearing of flora and fauna in space, various astronomical observations, science and engineering experiments and so on, and both rotating elements 5, 6 to generate artificial gravity and offer such environment as making a human being active so comfortably over a long period of time. In this case, the nonrotating element 1 and the rotating elements 5, 6 are coupled together in noncontact by a magnetic coupling part 7. This noncontact part 7 is made into a structure coupled with a rotary coupling part 14 magnetically in and around a nonrotating coupling part 13 or a part of the nonrotating element 1 via a void 15, and thereby it is constituted so as to have both relatively rotated by a motor 16.
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公开(公告)号:JPS63170198A
公开(公告)日:1988-07-14
申请号:JP299087
申请日:1987-01-09
Applicant: NAT AEROSPACE LAB , MITSUBISHI ELECTRIC CORP
Inventor: FUJIMORI YOSHINORI , TOMITA MASAYUKI
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公开(公告)号:JPS62205900A
公开(公告)日:1987-09-10
申请号:JP4998086
申请日:1986-03-07
Applicant: NAT AEROSPACE LAB , MITSUBISHI ELECTRIC CORP
Inventor: FUJIMORI YOSHINORI , HAMAGUCHI TATSUYA
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公开(公告)号:JPS63170197A
公开(公告)日:1988-07-14
申请号:JP298987
申请日:1987-01-09
Applicant: NAT AEROSPACE LAB , MITSUBISHI ELECTRIC CORP
Inventor: FUJIMORI YOSHINORI , NAKAGAWA JUN
IPC: B64G1/22 , H01L29/417
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