序号 | 专利名 | 申请号 | 申请日 | 公开(公告)号 | 公开(公告)日 | 发明人 |
---|---|---|---|---|---|---|
101 | VORRICHTUNG ZUM EXPERIMENTIEREN UNTER WELTRAUMBEDINGUNGEN | EP16158496.6 | 2016-03-03 | EP3064439A1 | 2016-09-07 | RITSCHEL, Christian; BOHNHARDT, Tobias; PAWEK, Christoph |
Die Erfindung betrifft eine Vorrichtung zum Experimentieren unter Weltraumbedingungen, umfassend einen Fallturm (2), eine Fallkapsel (3) und eine Auswerte- und Steuereinheit (4), wobei die Vorrichtung (1) mindestens einen von der Auswerte- und Steuereinheit (4) ansteuerbaren Elektromagneten (8) als Halteeinrichtung (6) aufweist, wobei die Halteeinrichtung (6) zusätzlich mindestens einen Permanentmagneten (7) aufweist, der die Fallkapsel (3) am Fallturm (2) hält, wobei die Auswerte- und Steuereinheit (4) und der Elektromagnet (8) derart ausgebildet sind, dass durch Ansteuerung des Elektromagneten (8) durch die Auswerte- und Steuereinheit (4) der Elektromagnet (8) ein Magnetfeld erzeugt, das das Magnetfeld des Permanentmagneten (7) derart abschwächt, dass die Fallkapsel (3) nicht mehr durch den Permanentmagneten (7) gehalten wird. |
||||||
102 | Banc de test pour senseur stellaire, et procédé de test | EP14169910.8 | 2014-05-26 | EP2813434A2 | 2014-12-17 | Mignot, Jean; Martinez, Pierre Emmanuel |
L'invention concerne un banc (1) de test d'un senseur stellaire, caractérisé en ce qu'il comprend : |
||||||
103 | Dispositif et procédé de stimulation de capteur optoélectronique | EP13180852.9 | 2013-08-19 | EP2703298A1 | 2014-03-05 | Vidal, Philippe |
L'invention vise un dispositif de stimulation d'un capteur optoélectronique, ledit dispositif comportant un afficheur matriciel (10) adapté à afficher des images à N couleurs doté avec une fréquence d'affichage 1/T (T étant la période théorique d'affichage des images colorées), N étant supérieur ou égal à 2, une électronique de contrôle (11) dudit afficheur (10), des moyens de génération de l'image à envoyer à l'afficheur (10), Le dispositif est tel que : |
||||||
104 | Fallturm, sowie Beschleunigungskapsel und Nutzlastträger für selbigen | EP13156172.2 | 2013-02-21 | EP2631184A1 | 2013-08-28 | Lämmerzahl, Claus Prof. Dr.; von Kampen, Peter |
Die Erfindung betrifft einen Fallturm (1) mit einem sich in dem Turm erstreckenden Innenraum (5) und einem Nutzlastträger (25) für Experimentieraufbauten, der in dem Innenraum (5) in senkrechter Richtung derart beweglich ist, dass während der Bewegung wenigstens zeitweise ein Zustand reduzierter Schwerkraft herrscht, einer zum Umschließen des Nutzlastträgers (25) ausgebildeten Beschleunigungskapsel. Erfindungsgemäß ist die Beschleunigungskapsel (7) mittels eines Linearantriebs (9) senkrecht geregelt bewegbar, und umfasst der Fallturm (1) eine Koppeleinrichtung (21, 23), welche dazu eingerichtet ist, den Nutzlastträger (25) und die Beschleunigungskapsel (7) kraft- und/oder formschlüssig zu koppeln, wenn die von dem Linearantrieb (9) geregelte Antriebskraft entgegen der Schwerkraft einen Wert größer null annimmt, und voneinander zu entkoppeln, wenn die von dem Linearantrieb (9) geregelte Antriebskraft entgegen der Schwerkraft einen Wert kleiner oder gleich null annimmt. |
||||||
105 | Spacecraft development testbed system | EP12174045.0 | 2012-06-28 | EP2546150A2 | 2013-01-16 | Vavrina, Matthew Aaron; Vian, John Lyle |
A method and apparatus comprising a location reference system (110) and a control module (108). The location reference system (110) is configured to generate location information for a number of mobile platforms (106) in an environment. The control module (108) is configured to receive the location information for the number of mobile platforms (106) from the location reference system (110). The control module (108) is further configured to generate command signals for the number of mobile platforms (106) using the location information. The control module (108) is further configured to send the command signals to the number of mobile platforms (106) to operate the number of mobile platforms (106) in the environment such that operation of the number of mobile platforms (106) emulates the operation of a number of spacecraft systems (101) in a non-Earth terrestrial environment. |
||||||
106 | SYSTEM AND METHOD FOR INHIBITING CORROSION OF METAL CONTAINERS AND COMPONENTS | EP99916575.6 | 1999-04-08 | EP1071520A1 | 2001-01-31 | MODI, Paresh, R. |
A method and system for inhibiting corrosion of aluminum and other metal-containing components and structures exposed to water are disclosed. In one embodiment, the silicate solution is used as a test fluid medium for structural testing of aluminum-alloy or other metal container structures including propellant tanks (14), in which a structure filled with the medium is then subjected to various structural load testing. In another embodiment, the silicate solution is used as a test medium for proof pressure hydrostatic or load testing of launch vehicle (10) booster tanks. The silicate film (18) protects the underlying base metal surface against corrosion during these tests. The film (18) also protects the base metal surface in normal atmospheric conditions from exposure to humidity and other atmospheric moisture after removal of the test medium from the propellant tank (14) following completion of testing. | ||||||
107 | Method and apparatus for integration and testing of satellites | EP99122058.3 | 1999-11-17 | EP1006049A3 | 2000-10-11 | Anderson, Joseph F.; Renken, Raymond H. |
A satellite integration and testing system and method in which a satellite (12) is assembled and many tests are performed on it in a single test chamber (10), thereby avoiding multiple setup and tear-down operations required if multiple test chambers are used, and avoiding the need to move the satellite between test chambers. |
||||||
108 | Method and apparatus for integration and testing of satellites | EP99122058.3 | 1999-11-17 | EP1006049A2 | 2000-06-07 | Anderson, Joseph F.; Renken, Raymond H. |
A satellite integration and testing system and method in which a satellite (12) is assembled and many tests are performed on it in a single test chamber (10), thereby avoiding multiple setup and tear-down operations required if multiple test chambers are used, and avoiding the need to move the satellite between test chambers. |
||||||
109 | Dispositif d'entraînement en rotation d'un bras d'une centrifugeuse de grandes dimensions | EP97402359.0 | 1997-10-07 | EP0835806A1 | 1998-04-15 | Lhenry, Bernard |
L'arbre d'entraînement de la centrifugeuse est relié à une couronne dentée en prise avec une pluralité de pignons. Les pignons sont entraînés chacun en rotation par un système d'entraînement comportant au moins un moteur asynchrone (12), un système d'alimentation du moteur asynchrone (12) en courant électrique comprenant, reliés à un bus (18) à courant continu, une source de courant continu (19, 20) un onduleur (17) réalisant le contrôle vectoriel du moteur asynchrone (12), un moyen de stockage d'énergie (21), de préférence sous la forme d'une batterie d'accumulateurs et une résistance électrique (25) de dissipation d'énergie, lors des freinages de la centrifugeuse. L'invention s'applique en particulier aux centrifugeuses pour l'entraînement de pilotes d'aéronefs. |
||||||
110 | Structure de positionnement et de stabilisation d'un objet en un point donné à l'intérieur d'un repère tridimensionnel | EP93400551.3 | 1993-03-03 | EP0559560B1 | 1997-01-08 | Bousquet, Jean-Claude; Maupetit, Bernard; Auroux, Michel; Goninet, Gérard |
111 | Dispositif d'entraînement en rotation d'un bras de centrifugeuse et procédé d'alimentation en énergie d'un tel dispositif | EP89400972.9 | 1989-04-10 | EP0337863B1 | 1993-10-27 | Perdriat, Jacques |
112 | Spherical fluid bearing apparatus | EP91122392.3 | 1991-12-30 | EP0501042A1 | 1992-09-02 | Diggins, Paul E. |
The apparatus (10) comprises at least one spherically segmented bearing assembly (30) arranged about the periphery of the device (12) so as to maintain the center of rotation of the device within the assembly coincident with the center of mass of the device. A fluid source (40) provides fluid to the spherically segmented bearing assemblies (30). |
||||||
113 | Procédé de création, notamment dans le champ gravitationnel terrestre, de conditions de microgravité, et appareil de mise en oeuvre de ce procédé | EP88401198.2 | 1988-05-18 | EP0292379B1 | 1992-07-22 | Mesland, Dick |
114 | Motion simulator | EP89310075.0 | 1989-10-03 | EP0421029A1 | 1991-04-10 | Lordo, Robert E.; McSparran, Lloyd W. |
A flight motion simulator (10) includes a unit under test (16) supported on a stationary frame (12) for angular and translational movement along pitch (28), roll (26), and yaw axes (30). A rotor element (25) is secured to the unit under test and has a spherical configuration. Magnetic bearings (24) supported by the stationary frame (12) support the rotor element (25) in three degrees of freedom of movement. A drag-cup induction motor (86) is mounted on the frame (12) and connected to the unit under test to generate three degrees of freedom of movement by generating a rotating magnetic flux in a stator assembly (76) to induce a corresponding flow of currents in the rotor element (72) to produce torque and motion in the unit under test (16) in the same direction as the flux movement in the stator assembly (76). |
||||||
115 | Procédé de création, notamment dans le champ gravitationnel terrestre, de conditions de microgravité, et appareil de mise en oeuvre de ce procédé | EP88401198.2 | 1988-05-18 | EP0292379A1 | 1988-11-23 | Mesland, Dick |
La présente invention est relative à un procédé de création de conditions de microgravité. Ce procédé se caractérise par :
|
||||||
116 | APPARATUS AND METHOD OF SIMULATING A SOMATOSENSORY EXPERIENCE IN SPACE | PCT/US2008074447 | 2008-08-27 | WO2009029657A3 | 2009-05-14 | XIAO QUAN |
A method of providing a user with an extra-terrestrial somatosensory experience includes equipping the user with an underwater breathing apparatus, having the user occupy an underwater environment, such environment providing buoyancy to the user, and while the user occupies the underwater environment, using a computer-implemented virtual reality system to present to the user a virtual reality environment modeling an extra-terrestrial setting. The virtual reality system inhibits visual perception by the user of items outside of the virtual reality environment so that the user experiences the virtual reality environment under a buoyancy condition provided by the underwater environment. The buoyancy condition enhances the experience of the virtual reality environment. | ||||||
117 | VARIABLE-ALTITUDE TESTING SYSTEMS | PCT/US2007076528 | 2007-08-22 | WO2008076478A2 | 2008-06-26 | ANDERSON GRANT A; MACCALLUM TABER K |
A ground-based system for simulating dynamic suborbital-f light environments occurring during substantially complete suborbital-f lights by a flight vehicle. | ||||||
118 | METHOD AND APPARATUS FOR SIMULATING SOLAR LIGHT | PCT/US2012022785 | 2012-01-26 | WO2012112276A2 | 2012-08-23 | JUNGWIRTH DOUGLAS R; QUEZADA EMILIO |
Described herein is a method and apparatus for simulating solar light to create an ideal testing environment for solar panels and the like. The method and apparatus may also be used to test solar resistance for color fading or resistance to high levels of solar energy. The apparatus generally consists of a plurality of mirrors directed towards a multi-faceted mirror, from which the light beams converge towards a target plane. The light intensity at the target plane is, according to one embodiment, between 100 and 200 suns. | ||||||
119 | SYSTEM AND METHOD FOR ASSESSING THE PERFORMANCE OF AN ATTITUDE CONTROL SYSTEM FOR SMALL SATELLITES | PCT/US2011043128 | 2011-07-07 | WO2012009198A3 | 2012-04-26 | FITZ-COY NORMAN G; NAGABHUSHAN VIVEK |
Various embodiments of the present invention include systems and methods for assessing the performance of an actuator of a attitude control system (ACS), such as a control moment gyroscope (CMG). In one embodiment, a system includes a support bracket assembly coupled to an actuator, wherein the actuator is configured to generate an output torque. The system also includes at least one sensor assembly coupled to the support bracket assembly, wherein the at least one sensor assembly includes a sensor configured to measure the output torque about at least one axis of the support bracket assembly while the support bracket assembly remains substantially motionless. | ||||||
120 | Closed loop data center and organic life ecosystem | US14335874 | 2014-07-18 | US09812925B2 | 2017-11-07 | Christian L. Belady; Brian Janous; Sean James |
Processing units and electrical power generation are integrated with a botanical environment to form a closed loop system whereby the outputs of one component serve as the inputs of another. Additionally, humans can be added to the system while maintaining the closed loop nature. Heat generated by the electrical power generation and processing units aids in the growth of botanicals and in the conversion of waste organic materials into both fertilizer and fuel for the electrical power generation. Additionally, carbon dioxide output by the electrical power generation is consumed by the botanicals, which, in turn, output oxygen consumed by the electrical power generation. Water is obtained by passing the exhaust of the electrical power generation across condenser coils, and is utilized for adiabatic cooling, as well as a heat transfer medium. Water is also consumed by the botanicals, aiding their growth. |