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61. 发明申请

WO2022200714A1 SYSTEME DE TRANSPORT DE PASSAGER PROPULSE PAR UN LANCEUR SPATIAL A SIEGE A INCLINAISON VARIABLE BASEE SUR LE FACTEUR DE CHARGE 审中-公开
公开(公告)号：WO2022200714A1
公开(公告)日：2022-09-29
申请号：PCT/FR2022/050485
申请日：2022-03-17
申请人： ARIANEGROUP SAS
发明人： PRAMPOLINI, Marco , DUTHEIL, Jean-Philippe , BOUE, Yoan
IPC分类号： B64G1/60 , B64G1/14 , B64G1/46 , B64G1/54 , B64D11/06 , B64G1/00
摘要： L'invention concerne un système de transport (1) destiné à être installé sur un lanceur spatial (100, figure 1) comprenant : • - un aéronef (2) qui comprend des moyens de propulsions configurés pour propulser l'aéronef (2) dans une direction de vol, et au moins un siège (4) destiné à recevoir un passager qui est mobile en rotation autour d'un axe (Θ) perpendiculaire à la direction de vol de l'aéronef (2), un capteur d'accélération étant installé sur chaque au moins un siège (4) pour mesurer l'accélération de chaque au moins un siège (4); • - une interface passager pour chaque au moins un siège (4) qui comprend un écran (51) destiné à afficher des images au passager installé sur ledit au moins un siège (4), l'écran (51) étant couplé audit au moins un siège (4) de sorte à rester fixe par rapport audit au moins un siège (4); • - une unité de commande (6) qui est reliée au capteur d'accélération et audit au moins un siège (4), l'unité de commande (6) étant configurée pour calculer un facteur de charge subi par le passager installé sur le au moins un siège (4) à partir de l'accélération dudit au moins un siège (4), l'unité de commande (6) étant configurée pour contrôler la rotation du au moins un siège (4) durant le fonctionnement du système de transport (1) afin de maintenir la position du siège (4) fixe par rapport au facteur de charge subi par le passager tout au long du vol.

62. 发明公开

EP2883798A1 Method for computing self-contamination processes of a spacecraft 有权转让
标题翻译： Verfahren zur Berechnung der Selbstverunreinigungsprozesse eines Raumfahrzeugs
公开(公告)号：EP2883798A1
公开(公告)日：2015-06-17
申请号：EP13005781.3
申请日：2013-12-12
申请人： Airbus DS GmbH
发明人： Heitzer, Jörg
IPC分类号： B64G1/22 , B64G1/46 , B64G1/52 , B64G1/66
CPC分类号： G06F17/5009 , B64G1/226 , B64G1/52 , B64G9/00 , G06F17/10
摘要： The invention relates to a method for computing self-contamination processes of a spacecraft by means of a data processing device comprising the following steps: receiving a first set of input parameters comprising general definitions of the spacecraft, receiving a second set of input parameters comprising control parameters for the spacecraft orbital data, physics, numeric, computing a self-contamination process of the spacecraft based on the received first and second sets of input data by calculating an analytical solution of a basic equation for calculating a deposit of molecules outgassed from surfaces of the spacecraft in a single computation step with the data processing device, and outputting the calculated deposit.
摘要翻译：本发明涉及一种用于通过数据处理装置计算航天器的自身污染过程的方法，该方法包括以下步骤：接收第一组输入参数，包括航天器的一般定义，接收第二组输入参数，包括控制用于航天器轨道数据，物理学，数字的参数，基于所接收的第一和第二组输入数据计算航空器的自身污染过程，通过计算用于计算从表面脱气的分子沉积物的基本方程式的分析解，在与数据处理装置的单个计算步骤中的航天器，并输出计算的存款。

63. 发明公开

EP0229163A4 SPACE LIVING QUARTERS HAVING ARTIFICIAL GRAVITY ENVIRONMENT. 失效
标题翻译：具有人工硬件环境的公寓单元。
公开(公告)号：EP0229163A4
公开(公告)日：1987-11-25
申请号：EP86904591
申请日：1986-06-26
申请人： ALLEN SEBREE J
发明人： ALLEN SEBREE J
IPC分类号： B64G1/46 , B64G1/60
CPC分类号： B64G1/60 , B64G1/46

64. 发明专利

JPH0761400A GRAVITY ENVIRONMENT SIMULATOR 失效
公开(公告)号：JPH0761400A
公开(公告)日：1995-03-07
申请号：JP21400893
申请日：1993-08-30
申请人： MITSUBISHI HEAVY IND LTD
发明人： TSUJIOKA MITSUTOSHI
IPC分类号： B64G1/46 , B64G7/00
摘要： PURPOSE:To perform simulation of arbitrary gravity environment through detec tion and correction of gravity environment on the sample side by an inertia navigation device, in a gravity environment simulator to perform an operation test of a sample through the change of gravity environment by means of a space device. CONSTITUTION:A sample system 20 comprises an on-mount calculator 1; and an inertia navigation device 3 and an inertia navigation device output before compensation is transmitted to a simulator system calculator 5 through a terminal 2 for output compensation by means of a signal line 9. The output before compensation is transmitted to the on-mount calculator 1 by the calculator 5 as a compensated inertia navigation device output compensated to arbitrary environment through the terminal 2 for output compensation by means of the signal line 10 and a simulator system actuator 7 is controlled to bring a sample into set gravity environment. Meanwhile, a sample system actuator 4 is controlled by calculator 1 based on the signal and the sample is operated under set arbitrary gravity environment, whereby simulation under arbitrary gravity environment is practicable.

65. 发明专利

JPH04237699A LIQUID HANDLING SYSTEM 失效
公开(公告)号：JPH04237699A
公开(公告)日：1992-08-26
申请号：JP379891
申请日：1991-01-17
申请人： MITSUBISHI HEAVY IND LTD
发明人： OHASHI ISAO
IPC分类号： B64G1/46 , F25D1/00
摘要： PURPOSE:To facilitate is repairing of a cooling water pool in a space machine. CONSTITUTION:A liquid handling system consists of a system which suctions and fills cooling water due to a reservoir 1, a pressurizing line 4 of nitrogen gas GN2 which operates bulkhead in the reservoir 1, an exhaust line 5, a cooling water supply line 6, and a cooling water discharge line 7 and a storage tank 3 which supplies and exhausts gas which has the same components as atmospheric air in a space machine.

66. 发明专利

JPH02246989A ENVIRONMENT MAINTAINING DEVICE 失效
公开(公告)号：JPH02246989A
公开(公告)日：1990-10-02
申请号：JP6586889
申请日：1989-03-20
申请人： MITSUBISHI HEAVY IND LTD
发明人： EITO TORU , MATSUMOTO HIROYO , MINEMOTO MASAKI
IPC分类号： A62B11/00 , B01D53/22 , B01D53/26 , B01D69/00 , B63C11/00 , B63G8/36 , B64D13/00 , B64G1/46
摘要： PURPOSE:To allow the selective permeation of the gaseous CO2 and steam contained in the air supplied on a primary side to a secondary side by sealing a soln. having high solubility and diffusibility to the gaseous CO2 and the steam between two sheets of thin films having excellent gas permeability and providing a pressure difference between the primary side and the secondary side of the thin films. CONSTITUTION:The soln. having the excellent solubility and diffusibility to the gaseous CO2 and the steam is sealed between 5 the thin films having the characteristics to allow the high permeation of gases but do not allow the permeation of liquid. The circulating air 3 in the hermetic space is introduced to a supply gas cell 6 segmented by the liquid film 5 of the film module 4. The secondary side of the liquid film 5 is in contact with a permeated gas cell 7 and this cell is maintained under a reduced pressure by a vacuum pump 8. The gaseous CO2 and steam contained in the circulating air 3 introduced into the cell 6 permeate to the cell 7 side while the gas and steam are selectively dissolved and diffused in the liquid film 5 by the pressure difference between both sides of the liquid film 5 as a driving power; thereafter, the gas and steam is taken out as a permeated gas 9 via a vacuum pump 8.

67. 发明专利

JPH01204900A MAGNETIC COUPLING TYPE SPACECRAFT PLATFORM 失效
公开(公告)号：JPH01204900A
公开(公告)日：1989-08-17
申请号：JP3009488
申请日：1988-02-12
申请人： NAT AEROSPACE LAB
发明人： 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
IPC分类号： B64G1/46 , B64G1/10 , B64G1/12 , B64G1/60 , F16C32/04
摘要： 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.

68. 发明专利

JPS5442907B2 失效
公开(公告)号：JPS5442907B2
公开(公告)日：1979-12-17
申请号：JP10413976
申请日：1976-08-31
IPC分类号： A01K1/03 , B64G1/46

69. 发明专利

JPS53142800A MAGNETIC MOMENT GRADUATION SYSTEM OF ARTIFICIAL SATELLITE 失效
公开(公告)号：JPS53142800A
公开(公告)日：1978-12-12
申请号：JP5621077
申请日：1977-05-16
申请人： HITACHI LTD
发明人： SATOU KIJIYUU
IPC分类号： B64G1/46 , B64G1/10
摘要： PURPOSE:To allow the minute adjustment of the magnetic moment value of an artificial satellite, by utilizing interaction between a permanent magnet and a magnetic substance magnetically induced by means of the magnet.

70. 实用新型

JPS53148499U 失效
公开(公告)号：JPS53148499U
公开(公告)日：1978-11-22
申请号：JP5270077
申请日：1977-04-27
IPC分类号： B64G1/46 , B64G1/10

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