专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

KR1020130061555A 진공 탈기 방식의 발사체용 단열재 有权
标题翻译：真空灭菌方法的热绝缘子
公开(公告)号：KR1020130061555A
公开(公告)日：2013-06-11
申请号：KR1020110127929
申请日：2011-12-01
申请人： 한국항공우주연구원
发明人： 김성룡
IPC分类号： B64G1/58 , F16L59/02 , B32B5/18
CPC分类号： B64G1/58 , B32B5/18
摘要： PURPOSE: An insulation material for a vacuum deaeration type projectile is provided to prevent damage to the insulation material due to heat by charging inert gas into the insulation material. CONSTITUTION: An insulation material(1) for a vacuum deaeration type projectile is attached to the outer surface of the projectile. Pores(11) are formed inside the insulation member and are filled with inert gas. When peripheral pressure becomes a vacuum state, the inert gas draws out to the outside of the insulation member.
摘要翻译：目的：提供用于真空脱泡型抛射体的绝缘材料，以通过将惰性气体充入绝缘材料中来防止由于热量而导致的绝缘材料损坏。构成：用于真空脱泡型抛射体的绝缘材料（1）附着在抛射体的外表面上。孔（11）形成在绝缘构件的内部并且填充有惰性气体。当周围压力变为真空状态时，惰性气体向绝缘构件外部抽出。

2. 发明公开

KR1020100079804A 복사 및 전도 열전달을 동시에 차단하는 복합 단열재 失效
标题翻译：热绝缘子防止两个辐射和导热传热
公开(公告)号：KR1020100079804A
公开(公告)日：2010-07-08
申请号：KR1020080138379
申请日：2008-12-31
申请人： 한국항공우주연구원
发明人： 최상호
IPC分类号： B64G1/58 , F16L59/02 , F02K9/14
CPC分类号： B64G1/58
摘要： PURPOSE: A complex adiabatic material for blocking radiant and conductive heat transfer is provided to prevent radiant heat from being blocked by preventing the pollution of an adiabatic material. CONSTITUTION: A complex adiabatic material(1) for blocking radiant and conductive heat transfer comprises a foam adiabatic material(10), a film adiabatic material(20) and a ceramic fiber(30). The form adiabatic material blocks the conductive heat transfer. The film adiabatic material blocks the radiant heat transfer. The ceramic fiber couples the form adiabatic material to the film adiabatic material by sewing. The film adiabatic material attaches a film tape to the upper surface of the ceramic fiber exposed to outside. On the film adiabatic material, an air outlet(21) is formed. The film adiabatic material prevents external pollutant from penetrating by attaching/detaching a film protecting layer(22).
摘要翻译：目的：提供一种用于阻挡辐射和导电传热的复合绝热材料，以防止辐射热被阻止，以防止绝热材料的污染。构成：用于阻挡辐射和导电传热的复合绝热材料（1）包括泡沫绝热材料（10），绝热材料（20）和陶瓷纤维（30）。绝热材料的形式阻止导电传热。绝热材料阻挡辐射热传递。陶瓷纤维通过缝制将绝热材料形式与绝热材料相结合。薄膜绝热材料将胶带粘附到暴露于外部的陶瓷纤维的上表面。在绝热材料上形成出气口（21）。膜绝热材料通过附着/分离膜保护层（22）来防止外部污染物渗透。

3. 发明公开

KR1020110020096A 정지궤도 위성의 방열판 차폐구조 无效
标题翻译：地球卫星热屏蔽覆盖结构
公开(公告)号：KR1020110020096A
公开(公告)日：2011-03-02
申请号：KR1020090077816
申请日：2009-08-21
申请人： 한국항공우주연구원
发明人： 전형열 , 김정훈 , 한조영 , 양군호 , 유명종
IPC分类号： B64G1/50 , B64G1/58 , B64G1/44
CPC分类号： B64G1/503 , B64G1/58
摘要： PURPOSE: A cover structure of thermal shield for a geostationary satellite is provided to prevent excessive heat from being emitted from a satellite to an outer space. CONSTITUTION: A cover structure of thermal shield for a geostationary satellite comprises a cover winding roller(30), a cover supporter(50), a guiderail(40), cover guides(60), and cover fixing units. The cover winding roller is installed in one side of a satellite panel. The cover supporter connects the cover guides in the end of a cover(20). The guiderail guides the cover guides installed in both ends of the cover. The cover fixing units fixes or unfixes the cover.
摘要翻译：目的：提供用于对地静止卫星的防护罩的盖结构，以防止过多的热量从卫星发射到外部空间。构成：用于对地静止卫星的隔热罩的盖结构包括盖卷绕辊（30），盖支撑件（50），导轨（40），盖导向件（60）和盖固定单元。盖卷绕辊安装在卫星面板的一侧。盖支架连接盖（20）端部的盖导轨。导轨引导安装在盖两端的盖导板。盖固定单元固定或不固定盖。

4. 发明公开

KR1020100066023A 인공위성용 다층박막단열재 失效
标题翻译：卫星多层绝缘
公开(公告)号：KR1020100066023A
公开(公告)日：2010-06-17
申请号：KR1020080124653
申请日：2008-12-09
申请人： 한국항공우주연구원
发明人： 현범석 , 김희경 , 이장준
IPC分类号： B64G1/58
CPC分类号： B64G1/58
摘要： PURPOSE: A multi-layered thin film insulating material for an artificial satellite is provided to facilitate clipping by a nipper-shaped clip when a repair patch adheres to a multi-layer insulation main body. CONSTITUTION: A multi-layered thin film insulating material for an artificial satellite comprises a multi-layer insulation main body(11), a repair patch(12) and a nipper-shaped clip(20). The repair patch is attached to a damaged part. The nipper-shaped clip connects the boundary part of the repair patch and the multi-layer insulation main body. The damaged part of the multi-layer insulation main body is repaired. The nipper-shaped clip is bent in a triangle shape to form a clipping part.
摘要翻译：目的：提供一种用于人造卫星的多层薄膜绝缘材料，以便当修补贴片粘附到多层绝缘主体上时，通过夹钳形夹子便于夹持。构成：用于人造卫星的多层薄膜绝缘材料包括多层绝缘主体（11），修补贴片（12）和钳子形夹子（20）。修补补片附着在损坏的部位上。夹钳形夹将修补补片的边界部分和多层绝缘主体连接起来。多层绝缘主体损坏部分进行维修。夹钳形的夹子被弯曲成三角形以形成夹持部分。

5. 发明公开

KR20180058353A 인공위성 추력기의 복사열 차폐 장치 및 상기 인공위성 추력기의 복사열 차폐 장치의 제조 방법 有权
公开(公告)号：KR20180058353A
公开(公告)日：2018-06-01
申请号：KR20160157189
申请日：2016-11-24
申请人： 한국항공우주연구원
发明人： 채종원
IPC分类号： B64G1/58 , F02K9/80
CPC分类号： B64G1/58 , F02K9/80
摘要： 일실시예에따른인공위성추력기의복사열차폐장치는, 인공위성추력기의추력실및 노즐사이에장착된차폐프레임; 상기추력실을바라보는상기차폐프레임의외측면에서상기추력실에인접한위치에제1 코팅물질로코팅된제1 코팅부; 및상기추력실을바라보는상기차폐프레임의외측면에서상기제1 코팅부보다상기추력실로부터먼 위치에제2 코팅물질로코팅된제2 코팅부;를포함하고, 상기제1 코팅물질은상기제2 코팅물질보다방사율이낮을수 있다.

6. 发明公开

KR1020120074378A 냉각채널이 구비된 복합재료 无效
标题翻译：具有冷却通道的复合材料
公开(公告)号：KR1020120074378A
公开(公告)日：2012-07-06
申请号：KR1020100136190
申请日：2010-12-28
申请人： 한국항공우주연구원
发明人： 은세원 , 공철원 , 이종웅 , 장영순 , 이영무
IPC分类号： B64G1/50 , B29C70/88 , B64G1/58
CPC分类号： B64G1/50 , B64G1/58
摘要： PURPOSE: A composite materials with a cooling channel is provided to remove problems following from the damage of insulation materials in aerodynamic sections by insulating without the insulation materials even in case of severe aerodynamic conditions. CONSTITUTION: A composite materials with a cooling channel comprises a composite material stacking part(100) and a cooling part. In the composite material stacking part, a layer is formed by at least one material among a carbon or a glass and is multiply laminated to form the composite material stacking part. The cooling part constitutes at least one layer of the composite material stacking part and comprises a cooling body(210) and refrigerant circulating channels(220). The refrigerant circulating channels are formed inside the cooling body and transfer refrigerant.
摘要翻译：目的：提供具有冷却通道的复合材料，以消除在空气动力学部分的绝缘材料损坏之后的问题，即使在严重的空气动力学条件的情况下也绝缘而不使用绝缘材料。构成：具有冷却通道的复合材料包括复合材料堆叠部分（100）和冷却部分。在复合材料堆叠部分中，通过碳或玻璃中的至少一种材料形成层，并且被多层压以形成复合材料堆叠部分。冷却部分构成至少一层复合材料堆叠部分，并包括冷却体（210）和制冷剂循环通道（220）。制冷剂循环通道形成在冷却体的内部并传递制冷剂。

7. 发明公开

KR20180034121A 우주비행체 및 우주비행체의 발사 방법 有权
标题翻译：太空飞行器和发射太空飞行器的方法
公开(公告)号：KR20180034121A
公开(公告)日：2018-04-04
申请号：KR20160124249
申请日：2016-09-27
IPC分类号： B64G1/46 , B64G1/58 , B64G1/64
CPC分类号： B64G1/46 , B64G1/58 , B64G1/64
摘要： 본발명의일 실시예에따른우주비행체는, 추진력을제공하는발사체, 상기발사체상에배치된페이로드(payload) 및상기발사체와체결되고, 상기페이로드를둘러싸도록배치되며, 대기압보다낮은기압을가지는내부공간을형성하는페어링(fairing)을포함한다.
摘要翻译：根据本发明的实施例的航天器包括提供推进力的抛射体，设置在抛射体上的有效载荷以及安装在抛射体上的踏板，设置成围绕有效载荷，该分支包括形成内部空间的整流罩。

8. 发明授权

KR101516805B1 태양전지셀이 구비된 인공위성용 다층박막단열재 有权
标题翻译：用于太阳能电池的卫星多层绝缘
公开(公告)号：KR101516805B1
公开(公告)日：2015-05-04
申请号：KR1020130153051
申请日：2013-12-10
申请人： 한국항공우주연구원
发明人： 현범석 , 이장준 , 전형열
IPC分类号： B64G1/44 , H01L31/0445 , B64G1/58
CPC分类号： Y02E10/50 , B64G1/58 , B64G1/443 , C08G73/10 , H01L31/0445
摘要： 본발명은외측에폴리이미드필름이결합되며, 내측에다수개의박막필름으로적층형성된인공위성용다층박막단열재에있어서, 상기폴리이미드필름의외측에는태양전지셀을더 포함하는것을특징으로하는인공위성용다층박막단열재에관한것으로써, 특히, 다층박막단열재의최외곽층인폴리이미드필름에플렉시블한재질의태양전지셀을부착하여인공위성의운용에필요한전력을생산할수 있는태양전지셀이구비된인공위성용다층박막단열재에관한것이다.
摘要翻译：本发明涉及一种用于具有太阳能电池的卫星的多层薄膜绝缘体，其中聚酰亚胺膜耦合在外侧，并且多个薄膜形成为层叠在内侧，并且还包括太阳能电池聚酰亚胺膜的外侧。更具体地说，本发明涉及一种用于具有太阳能电池的卫星的多层薄膜绝缘体，其中柔性太阳能电池被附着到作为多层薄膜绝缘体的最外层的聚酰亚胺膜; 从而产生操作卫星所需的电力。

9. 发明授权

KR100175719B1 차량 배기 시스템의 열 조정 失效
标题翻译：车辆排气系统的热调节
公开(公告)号：KR100175719B1
公开(公告)日：1999-03-20
申请号：KR1019960704070
申请日：1995-01-27
申请人： 데이비드 케이. 벤손 , 토마스 에프. 포터
发明人： 데이비드케이.벤손 , 토마스에프.포터
IPC分类号： F01N3/10
CPC分类号： B64G1/22 , B64G1/226 , B64G1/50 , B64G1/503 , B64G1/58 , E04C2/292 , E04C2/34 , E06B3/66304 , F01N3/08 , F01N3/2006 , F01N3/2013 , F01N3/2046 , F01N3/2828 , F01N3/2875 , F01N3/2882 , F01N3/2889 , F01N5/02 , F01N5/025 , F01N13/0097 , F01N13/14 , F01N2240/02 , F01N2240/10 , F01N2260/02 , F01N2260/08 , F01N2330/06 , F01N2470/12 , F28F13/00 , F28F2013/005 , Y02A50/2322 , Y02T10/16 , Y02T10/26
摘要： A catalytic converter (10,140) is surrounded by variable conductance insulation (30,164) for maintaining the operating temperature of the catalytic converter (10,140) at an optimum level, for inhibiting heat loss when raising catalytic converter temperature to light-off temperature, for storing excess heat to maintain or accelerate reaching light-off temperature, and for conducting excess heat away from the catalytic converter (10,140) after reaching light-off temperature. The variable conductance insulation (30,164) includes vacuum gas control and metal-to-metal thermal shunt mechanisms (134). Radial and axial (138) shielding inhibits radiation and convection heat loss. Thermal storage media includes phase change material (150), and heat exchanger chambers (164) and fluids (166) carry heat to and from the catalytic converter (10,140).

10. 发明公开

KR1020170134537A 결합된 보강재/히트 파이프를 갖는 인공위성 방열기 패널 审中-实审
标题翻译：带加强筋/热管组合的卫星散热器面板
公开(公告)号：KR1020170134537A
公开(公告)日：2017-12-06
申请号：KR1020177031249
申请日：2016-03-30
申请人： 월드뷰 새틀라이트 리미티드
发明人： 스미스알렉산더디 , 필드다니엘더블유 , 아스키잔아르멘 , 글로스만제임스
IPC分类号： B64G1/50 , B64G1/10 , F28D15/02
CPC分类号： B64G1/503 , B64G1/10 , B64G1/283 , B64G1/40 , B64G1/402 , B64G1/50 , B64G1/506 , B64G1/58 , B64G1/66 , F28D15/02 , F28D15/0275 , F28F1/10
摘要： 인공위성에서사용하기위한패시브열 시스템은, 표면에복수의히트파이프가부착된고체방열기패널을포함한다. 열전달능력외에도, 히트파이프는, 히트파이프가커플링되는방열기패널을강화한다. 몇몇실시형태에서, 히트파이프는그들의면적관성모멘트를증가시키도록구조적으로변형된다.
摘要翻译：用于卫星的无源热系统包括固体散热器面板，其具有附接到其表面的多个热管。除了传热能力之外，热管还增强了热管所连接的散热器面板。在一些实施例中，热管在结构上被修改以增加它们的面积惯性矩。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式