| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | ТОПЛИВНЫЙ МОДУЛЬ | RU2004107542 | 2004-03-16 | RU2004107542A | 2005-10-10 | |
| 162 | ТОПЛИВНЫЙ МОДУЛЬ | RU2004107539 | 2004-03-16 | RU2004107539A | 2005-10-10 | |
| 163 | Space rope for transporting objects from Earth's surface into the space and vice versa is provided with gas balloons fixed along its length to provide a lift | DE102004007023 | 2004-02-12 | DE102004007023A1 | 2005-09-08 | MERLAKU KASTRIOT |
| The space rope (1) for transporting objects from Earth's surface into the space and vice versa is provided with gas balloons (2) fixed along its length to provide a lift equal at least to the rope weight between respective balloon levels. | ||||||
| 164 | САНИТАРНЫЙ ТРАНСПОРТ "АКАДЕМИК ЛИТВИНОВ" | RU2002128980 | 2002-10-29 | RU2254115C2 | 2005-06-20 | |
| FIELD: equipment for extreme medicine services, in particular, transport for rendering urgent aid to those suffered in extreme situations. SUBSTANCE: transport has technical evacuation means, as well as detecting, accounting, sorting out, diagnosis and rescue devices. Said devices allow first aid and medicinal aid to be rendered. Apparatus has medicinal sections including special, sanitary and therapeutic-and-diagnostic equipment, instruments and medicinal facilities. Research section has on-board radar detection complex, portable designation and reflexotherapeutic equipment of general and individual usage. Section for evaluating state of severity of sufferers has complex for taking solution in rendering aid to sufferers with regard to time and site. Said complex has automatic systems for accounting data on sufferers and sorting out and forecasting survival of wounded people. Resuscitation and intensive therapy section has on-board complex of telemedicinal subscriber's center, as well as wireless system for controlling rescue of wounded people on the basis of local computer network. Apparatus is furnished with internal and external communication means, as well as sufferer diagnosis and rescue means. All sections are equipped with working places for medicinal personnel, auxiliary catering and rest sites. Special sections are equipped with places for seriously and slightly wounded people. EFFECT: reduced lethality of wounded people due to increased extent of solution of operative tasks. 1 dwg | ||||||
| 165 | Bearing assembly for supporting tensile forces and bearing head for the bearing assembly | DE19933379 | 1999-07-20 | DE19933379B4 | 2005-03-10 | MUTH MICHAEL; SCHULZ BERND |
| Eine Lageranordnung zum Abstützen von Zugkräften, insbesondere zur hängenden Lagerung einer Masse, um in einem Gravitationsfeld deren Schwerelosigkeit zu simulieren, weist ein erstes, zumindest einen Magneten umfassendes Lagerelement und ein zweites, metallenes Lagerelement auf, das von einem ersten Lagerelement magnetisch angezogen wird. Zumindest eines der Lagerelemente weist in seiner Lagerfläche Gasaustrittsdüsen auf, die von einem Druckgas beaufschlagt sind, so daß ein aus den Gasaustrittsdüsen austretender Gasstrom ein Gaspolster zwischen den aufgrund der Magnetkraft einander anziehenden Lagerelementen bildet, das die Lagerelemente voneinander beabstandet hält. Die magnetische Anziehungskraft zwischen den Lagerelementen ist dabei gleich der Summe aus der von der Masse und dem ersten Lagerelement ausgeübten Zugkraft und der Abstoßungskraft des Gaspolsters. Eine derartige Lageranordnung wird vorzugsweise zur schwerkraftkompensierenden Aufhängung einer faltbaren Solarpanel-Anordnung für einen Satelliten in einer Testeinrichtung für eine die Schwerelosigkeit simulierende Erprobung des Entfaltungsvorgangs in einem Gravitationsfeld verwendet. | ||||||
| 166 | СОСУД ДЛЯ ПИТЬЯ В УСЛОВИЯХ НЕВЕСОМОСТИ | RU2004106960 | 2004-03-09 | RU39465U1 | 2004-08-10 | |
| Данное техническое устройство относится к средствам обеспечения жизнедеятельности человека в условиях невесомости, в частности, к сосудам для питья. В дополнительной емкости размещается доза вкусового концентрата. В жесткой емкости выполнено по меньшей мере одно сквозное отверстие, через которое внутренняя полость жесткой емкости сообщена с атмосферой. Перекрывное устройство выполнено в виде основания охватывающего трубку, двух поворотных вертикальных рычагов с выступами, на их внутренних стенках для зажима трубки, ручного привода, выполненного в виде поперечного элемента, установленного подвижно на одном из вертикальных рычагов, и с возможностью зацепления на элемент зацепки, выполненной на конце второго рычага. В данной полезной модели резьбовое соединение крышки со стаканом перенесено с внутренней стороны на внешнюю, а съемная пробка выполнена в форме конуса. При накручивании крышки на стакан, она будет давить на пробку, которая вдавливаясь во внутрь стакана своей боковой поверхностью будет прижимать верхний край дополнительной емкости к верхней части жесткой емкости. В результате применения данной полезной модели осуществляется многоразовое использование сосуда за счет его конструктивного упрощения и повышение надежности эксплуатации, при этом сохраняется возможность приготовления в сосуде газированных напитков путем смешивания концентрата с газированной водой, поступающей от внешнего источника. | ||||||
| 167 | МОДУЛЬ КАПСУЛЬНОЙ ДОСТАВКИ | RU2002122073 | 2002-08-12 | RU2232112C2 | 2004-07-10 | |
| FIELD: space engineering; updating of orbital space stations. SUBSTANCE: proposed module includes movable ring with descent capsules, pneumatic system and control system, as well as body. Adapters with bottoms are mounted on body flanges. Bottoms have ports with seats for coupling units. Body is provided with basket rigidly mounted at area where cargo is gripped. To increase number of descent capsules, additional body with additional capsules is mounted at joint. EFFECT: extended functional capabilities. 2 cl, 5 dwg, 1 dwg of prototype | ||||||
| 168 | PROPELLANT COMPARTMENT OF SPACECRAFT | RU2002123450 | 2002-09-02 | RU2231485C2 | 2004-06-27 | |
| FIELD: space engineering; designing spacecraft. ^ SUBSTANCE: proposed propellant compartment has case with fuel and oxidizer tanks inside it. Case is provided with hermetic hatches where fuel and oxidizer filling panels are mounted with valves fitted in them; they are communicated with respective propellant tanks through respective pipe lines and are provided with seals. Each hatch is provided with outer detachable protective apron and unit for coupling the filling systems of propellant tanks. Fuel and oxidizer hatches are located in case and are shifted in height and perimeter of case. ^ EFFECT: ease in servicing; enhanced safety in filling the tanks. ^ 1 dwg | ||||||
| 169 | Sports equipment for astronauts, comprises motor-driven gyroscope in casing which is fastened to limb or body | DE10251275 | 2002-11-04 | DE10251275A1 | 2004-05-19 | MERLAKU KASTRIOT |
| The motor-driven gyroscope (1) in a casing (5), has a handle or fastening strap (3). This is for attachment to the legs, hands or back of the astronaut. | ||||||
| 170 | Центробежный космический двигатель | RU2000127591 | 2000-11-02 | RU2000127591A | 2004-02-20 | |
| 171 | BIFURCATED TURBOFAN EXHAUST NOZZLE | CA2486175 | 2003-05-19 | CA2486175A1 | 2003-12-04 | LAIR JEAN-PIERRE |
| A turbofan exhaust nozzle (28) includes a fan duct (40) defined between a fa n nacelle (32) and a core engine cowling (30). The fan duct (40) includes a longitudinal endwall (48) and a partition (50) spaced therefrom to define a secondary flow duct (52). The fan duct (40) also includes a primary outlet (42), and the secondary duct (52) includes a secondary outlet (54). The partition (50) between the two ducts includes an aperture (56) covered by a selectively movable flap (58). | ||||||
| 172 | SPACECRAFT | RU2002117199 | 2002-06-27 | RU2216488C1 | 2003-11-20 | BUDANOV S V |
| FIELD: space engineering; spacecraft. SUBSTANCE: proposed spacecraft has fuselage with crew cabin, tail unit in form of two keel struts and upper and lower stabilizers, payload compartment, wing at multiple sweep, power plant, orbital maneuvering system with actuating members and landing gear made in form of multi-axle truck, nose wheel and tail steerable wheel. Spacecraft is provided with two passenger sections located on sides of fuselage on wing planes, aft hatch with flange for communication with payload compartment, hemispherical cover coupled hermetically and detachably to said flange of aft hatch. Passenger sections and payload compartment are provided with windows. Flange of aft hatch is provided with smoothly distributed with holes. Fitted in flange of aft cover are studs with threaded ends; hemispherical cover is made integral with handle located in its cavity. EFFECT: extended functional capabilities of spacecraft. 7 dwg | ||||||
| 173 | СПОСІБ І ПРИСТРІЙ ДЛЯ ОДЕРЖАННЯ НАДГЛИБОКОГО ВАКУУМУ В НАСЕЛЕНОМУ ВІДСІКУ КОСМІЧНОГО ОБ'ЄКТА | UA2001117438 | 2001-11-01 | UA61169C2 | 2003-11-17 | PATON BORYS YEVHENOVYCH; BERZHATYI VLADIMIR IVANOVICH; BYLATSEV OLEKSANDR RATMYROVYCH; ZAHREBELNYI OLEKSANDR AIZYKOVY; ZVORYKIN LEV LVOVYCH; KRIUKOV VALERII ANATOLIOVYCH; MARKOV ALEKSANDR VIKTOROVICH; PEREPECHENKO BORYS IVANOVYCH; SVECHKIN VALERII PETROVYCH; CHURILO IGOR VLADIMIROVICH |
| Спосібі пристрійдляодержаннянадглибокоговакуумув населеномувідсікукосмічногооб'єктадозволяютьреалізовувативисоковакуумнітехнологіїбезвиходукосмонавтау відкритийкосмос. Прицьому «транспортування» надглибокоговакууму, одержуваногозаекраном, увакуумнукамеру, щознаходитьсяв населеномувідсікукосмічногооб'єкта, виконуєтьсяповакуумопроводу, щотрансформується, якийвисуваєекранзамежівласноїатмосферикосмічногооб'єкта. Екранвиконанийтрансформованимі міститьшарнірно-підйомніланки, наякихзакріпленегазонепроникнеполотнищеекрана, герметичноз'єднанез вакуумопроводом. Шарнірно-підйомніланкиприводятьсяв рухспільнимприводом, причомукутповоротупершоговажелякожноїз ланокудвічіменший, ніжкутповоротудругоговажеля. Послідовневикористаннядвохчибільшевакуумнихкамердозволитьпідвищитипродуктивністьробіт. | ||||||
| 174 | Foldable structure | DE69817301 | 1998-12-01 | DE69817301D1 | 2003-09-25 | NAKAJIMA KAZUTAKA |
| 175 | BR9908124 | 1999-04-29 | BR9908124A | 2000-10-24 | SAFRONOV SERGEI MIKHAILOVICH; ZAITSEV EVGENY ALEKSANDROVICH; MELNIKOV ALEKSEI YUREVICH; KONSTANTINOV YURY FEDOROVICH; REZNIKOV ALEKSANDR EVGENEVICH; STAROSTIN STANISLAV VASILEVICH | |
| 176 | METHOD OF ACHIEVING HIGH SPACECREAFT SPEED | PL32748298 | 1998-10-14 | PL327482A1 | 2000-04-25 | PRZEPIERA MARIAN |
| 177 | SPACE VEHICLE | RU97119014 | 1997-10-30 | RU2137681C1 | 1999-09-20 | KRIVOROTOV A S |
| FIELD: aerospace engineering; study of Earth and other planets of solar systems. SUBSTANCE: space vehicle has thermally protected pressurized case in form of monowing with three communicating fuselages inside it. Solar batteries with internal evacuated cavities and external protection against overheating are mounted on the outside of space vehicle. Propellant tanks and several groups of jet engines (cruise engines, ascent and descent engines, braking engines and gas-turbine engines) are installed in case. Turbines of gas-turbine engines are connected with magneto-electric generators of on-board power supply system of space vehicle. Space vehicle includes also microspace vehicles for reconnaissance of plants and furnishing information for the crew. Space vehicle may reach various planets and return to Earth. Such space vehicle may be also used for observation of near-planet space and carry out rescue jobs. EFFECT: enhanced efficiency and reliability. 8 cl, 10 dwg | ||||||
| 178 | EEP9800051 | 1998-04-30 | EE9800051A | 1998-06-15 | RUSLAN EELENIN | |
| 179 | COMPLEX TECHNOLOGY OF PLANETARY AND INTERPLANETARY NAVIGATION | RU95101619 | 1995-02-02 | RU2106287C1 | 1998-03-10 | BELOSHAPKIN KIM PETROVICH |
| FIELD: flying vehicles of saucer configuration employing effect of rotary thermal field, namely, aerospace vehicle for atmosphere and vacuum navigation. SUBSTANCE: complex technology of planetary and interplanetary navigation includes flying device formed by at least two similar saucer-type flying vehicles of different diameters. Diameter of first flying vehicle exceeds diameters of other vehicles. Each flying vehicle is provided with propeller for motion in atmosphere employing the effect of rotary thermal field and shooting-type jet engine for motion in vacuum. EFFECT: enhanced efficiency. 2 cl, 6 dwgo | ||||||
| 180 | REFLECTOR AND FRAME | RU93012847 | 1993-03-11 | RU2104906C1 | 1998-02-20 | TARAN VALENTIN MIKHAJLOVICH |
| FIELD: space engineering; development and operation of large-sized transformable orbital reflectors. SUBSTANCE: reflector includes transformable framework in form of circular solenoids with circular flywheels mounted in them and made fro material possessing thermomechanical memory of form and folding rod-type polygonal frames connected with circular solenoids by means of coupling units. Mirror film base of reflector is made in form of strips secured to frames through form-setting members and film tension regulators; these members may be made in form of circular solenoids with circular flywheels carrying strips of film and imparting complex form to reflector, for example, parabolic form. Some strips of film may be connected with frames as controllable gills when surface of reflector is used as solar sail. In orbit, reflector opens due to effect of memory of form of circular flywheel by means of spring drives and retainers of frame rods; final form of film surface and control of orientation of reflector are made due to spinning-up of flywheels inside circular solenoids and redistribution of total angular momentum of system among different circular flywheels. EFFECT: enhanced efficiency. 4 cl, 18 dwgr | ||||||
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