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51. 发明申请

US20120192908A1 Sinkless thermoelectric energy generator 审中-公开
标题翻译：无水热电发电机
公开(公告)号：US20120192908A1
公开(公告)日：2012-08-02
申请号：US12931441
申请日：2011-02-01
申请人： Bruce R. Kline
发明人： Bruce R. Kline
IPC分类号： H01L35/30
CPC分类号： H01L35/30 , B64C1/38 , B64D41/00 , Y02T50/53
摘要： Disclosed is a sinkless electric generator for generating electrical power from temperature cycles encountered by the structure of an aircraft. The sinkless electric generator includes a thermoelectric generator which is in thermal contact with the structure of the aircraft (e.g., the aircraft's skin); an insulated housing containing a thermal mass; and a circuit for providing the energy generated by the thermoelectric generator during the temperature cycles encountered by the structure of the aircraft to a device. The insulated housing is positioned in thermal contact with the thermoelectric generator; wherein during the temperature cycles encountered by the structure of the aircraft, energy is created by the thermoelectric generator when heat is released from the thermal mass contained within the housing through the thermoelectric generator to the aircraft's structure and when heat is supplied from the aircraft's structure through the thermoelectric generator to the thermal mass.
摘要翻译：公开了一种用于由飞行器结构遇到的温度循环产生电力的无接收发电机。无沉没发电机包括与飞行器结构（例如飞行器的皮肤）热接触的热电发电机; 包含热质的绝缘壳体; 以及用于在由飞行器的结构遇到的温度循环期间将热电发电机产生的能量提供给设备的电路。绝缘壳体与热电发生器热接触; 其中在飞行器结构遇到的温度循环期间，当热量通过热电发电机从包含在壳体内的热质量释放到飞行器的结构上并且当从飞行器的结构提供热量时，热能发电机产生能量热电发电机到热质。

52. 发明授权

US08205836B2 Fire protection device for an aircraft or spacecraft 有权
标题翻译：飞机或航天器的防火装置
公开(公告)号：US08205836B2
公开(公告)日：2012-06-26
申请号：US12001482
申请日：2007-12-11
申请人： Falk Brinkmann , Heinz-Peter Busch , Berend Schoke
发明人： Falk Brinkmann , Heinz-Peter Busch , Berend Schoke
IPC分类号： B64D45/00 , E05F15/20 , A62C3/08
CPC分类号： A62C3/08 , A62C2/065 , B64C1/38
摘要： A fire protection device for an aircraft or spacecraft is disclosed. The fire protection device can include a fireproof bulkhead and an adjusting device, the fireproof bulkhead can be adjusted from a ventilating position I into a screening position II. This may prevent a stream of smoke and heat from penetrating into the cabin when there is a fire underneath the fuselage.
摘要翻译：公开了一种用于飞机或航天器的防火装置。防火装置可以包括防火舱壁和调节装置，防火舱壁可以从通风位置I调整到筛选位置II。当机身下方发生火灾时，这可能会阻止烟雾和热量流入舱内。

53. 发明申请

US20110005192A1 COOLING SYSTEM FOR AN AIRCRAFT, AIRCRAFT COMPRISING THE COOLING SYSTEM AND COOLING METHOD 审中-公开
标题翻译：用于飞机的冷却系统，包括冷却系统和冷却方法的飞机
公开(公告)号：US20110005192A1
公开(公告)日：2011-01-13
申请号：US12868336
申请日：2010-08-25
申请人： Hans Martensson , Anders Hellgren
发明人： Hans Martensson , Anders Hellgren
IPC分类号： B64G1/40
CPC分类号： B64C1/38
摘要： A cooling system for an aircraft includes a cooling circuit for transporting a coolant, with the cooling circuit running to a component in the aircraft that is heated up during flying in order to take up heat from the heated-up component via the coolant. The cooling circuit runs to a jet engine for propulsion of the aircraft in order to release heat to a flow of gas in the jet engine via the coolant.
摘要翻译：用于飞行器的冷却系统包括用于运输冷却剂的冷却回路，其中冷却回路运行到在飞行期间被加热的飞机中的部件，以便经由冷却剂从加热部件吸收热量。冷却回路运行到喷气发动机以推进飞行器，以便通过冷却剂将热释放到喷气发动机中的气体流。

54. 发明授权

US07232093B2 Cooled insulation surface temperature control system 有权
标题翻译：冷却绝缘表面温度控制系统
公开(公告)号：US07232093B2
公开(公告)日：2007-06-19
申请号：US11271600
申请日：2005-11-10
申请人： William W. Behrens , Andrew R. Tucker , James E. French , Gayl J. Miller
发明人： William W. Behrens , Andrew R. Tucker , James E. French , Gayl J. Miller
IPC分类号： B64C1/38
CPC分类号： F28F13/003 , B64C1/38 , B64G1/58 , F28D2021/0078
摘要： An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surface of the porous layer to prevent erosion of the porous layer and to facilitate surface film cooling.
摘要翻译：提供了表面温度控制的装置和方法。表面温度控制是通过将冷却剂流入并连接到结构气室附近的低强度多孔层而实现的。半透层可以附着在多孔层的外表面上，以防止多孔层的腐蚀并促进表面膜冷却。

55. 发明授权

US07055781B2 Cooled insulation surface temperature control system 有权
公开(公告)号：US07055781B2
公开(公告)日：2006-06-06
申请号：US10455204
申请日：2003-06-05
申请人： William W. Behrens , Andrew R. Tucker , James E. French , Gayl J. Miller
发明人： William W. Behrens , Andrew R. Tucker , James E. French , Gayl J. Miller
IPC分类号： B64G1/58
CPC分类号： F28F13/003 , B64C1/38 , B64G1/58 , F28D2021/0078
摘要： An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surface of the porous layer to prevent erosion of the porous layer and to facilitate surface film cooling.

56. 发明申请

US20050116107A1 Area ruling for vertical stabilizers 审中-公开
标题翻译：垂直稳定器的面积统计
公开(公告)号：US20050116107A1
公开(公告)日：2005-06-02
申请号：US10706670
申请日：2003-11-11
申请人： John Morgenstern , Alan Arslan , Garret Moose
发明人： John Morgenstern , Alan Arslan , Garret Moose
IPC分类号： B64C1/38 , B64C3/38
CPC分类号： B64C1/38 , B64C3/38
摘要： A vertical stabilizer is configured to minimize the rate of change of cross-sectional area of the vehicle or device to which the vertical stabilizer is mounted. One or more “waisted” areas can be included at the tip and/or the root of the vertical stabilizers, as well as over the distance from tip to root of the vertical stabilizer. In some situations, a strake is mounted on the vehicle or device, such as an aircraft, and the vertical stabilizer is mounted to the tip of the strake. The strake can also be area ruled with one or more “waisted” sections at the juncture of the vertical stabilizer. Applying area ruling to the vertical stabilizer helps to further reduce the drag of the vehicle or device.
摘要翻译：垂直稳定器构造成使安装有垂直稳定器的车辆或装置的横截面面积的变化率最小化。一个或多个“腰围”区域可以包括在垂直稳定器的尖端和/或根部以及垂直稳定器的尖端到根部的距离处。在某些情况下，在车辆或装置（例如飞行器）上安装一个行走架，并且垂直的稳定器安装在该行李架的顶端。在垂直稳定器的接合处，也可以在一个或多个“腰部”区域上划定该区域。对垂直稳定器施加面积调整有助于进一步减少车辆或设备的阻力。

57. 发明申请

US20050045306A1 Transpiration cooling system 有权
标题翻译：蒸腾冷却系统
公开(公告)号：US20050045306A1
公开(公告)日：2005-03-03
申请号：US10624908
申请日：2003-07-22
申请人： Miklos Petervary , Kevin Lohner
发明人： Miklos Petervary , Kevin Lohner
IPC分类号： B64C1/38 , B64C3/36 , B64G1/58 , F01D5/18 , F01D25/12 , F02K1/82 , F02K9/40 , F02K9/64 , F04D29/38 , F04D29/58 , F23R3/00 , F28F7/00
CPC分类号： F01D5/184 , B64C1/38 , B64G1/401 , B64G1/58 , F01D25/12 , F02K1/825 , F02K9/64 , F02K9/972 , F05D2250/323 , F23R3/002 , F23R3/007 , F23R2900/03041 , F28D2021/0078 , F28F13/003 , F42B15/34 , Y02T50/43
摘要： A system for cooling a structure or mechanism through transpiration processes. Generally a porous structural material may be used to form a hot wall surface of a high temperature or high heat flux environment component, typically used in combustion type devices. Coolant pressurized on the “cold” or cooler side of the wall is bled, “sweated”, or otherwise transpired to the “hot” wall surface in an effort to control the hot wall surface temperature by shielding the surface with a coolant layer at the surface and by removing heat via coolant flow past the surface. This may be done to manage the hot wall temperature for structural purposes, more effectively manage high heat fluxes, or to hide thermal signatures. The porous material can be selectively made such that the coolant material flows substantially in one direction only through the porous material to transfer thermal energy only away from the structure rather than towards the structure.
摘要翻译：一种通过蒸腾过程冷却结构或机制的系统。通常，多孔结构材料可用于形成通常用于燃烧型装置的高温或高热通量环境组分的热壁表面。在壁的“冷”或冷却器侧加压的冷却剂被排出，“出汗”或以其他方式蒸发到“热”壁表面，以通过在该表面上冷却表面屏蔽冷却剂层来控制热壁表面温度通过冷却液流过表面除去热量。这可以用于管理结构目的的热壁温度，更有效地管理高热通量或隐藏热特征。可以选择性地制造多孔材料，使得冷却剂材料仅通过多孔材料基本上在一个方向上流动，以将热能仅偏离结构而不是结构。

58. 发明申请

US20040258900A1 Multi-layer ceramic composite material with a thermal-protective effect 有权
标题翻译：多层陶瓷复合材料具有保温作用
公开(公告)号：US20040258900A1
公开(公告)日：2004-12-23
申请号：US10830431
申请日：2004-04-23
发明人： Reinhard A. Simon , Helmut E.A. Knabe , Wolfgang Schafer , Walter D. Vogel , Wilhelm Wulbrand , Wilhelm Hager , Kurt Lindner , Paul Hennig
IPC分类号： B32B005/02
CPC分类号： C04B35/6263 , B32B18/00 , B32B2315/02 , B64C1/38 , B64C1/40 , B64G1/58 , C04B35/185 , C04B35/803 , C04B2235/3217 , C04B2235/3218 , C04B2235/3418 , C04B2235/3463 , C04B2235/386 , C04B2235/522 , C04B2235/5224 , C04B2235/5228 , C04B2235/5445 , C04B2235/721 , C04B2235/96 , C04B2235/9607 , C04B2237/341 , C04B2237/343 , C04B2237/38 , H01Q1/424 , Y10T428/1376 , Y10T428/249928 , Y10T428/249953 , Y10T428/252 , Y10T428/3154
摘要： A two-layer ceramic composite material, wherein the first predominantly load-bearing layer is an oxidic, carbon-free fiber-reinforced ceramic layer which is made by a colloidal process. The second predominantly thermally insulating layer is an oxide-ceramic foam. The colloidal process produces carbon-free oxide ceramics which, because of their high purity, have low dielectric losses in the entire usage temperature range. In addition, the colloidal process provides a simple and cost-effective production method.
摘要翻译：一种双层陶瓷复合材料，其中第一主要是承载层是通过胶体方法制成的无氧碳纤维增强陶瓷层。第二主要是绝热层是氧化物 - 陶瓷泡沫。胶体工艺生产无碳氧化物陶瓷，由于其高纯度，在整个使用温度范围内具有低介电损耗。此外，胶体工艺提供了一种简单且经济有效的生产方法。

59. 发明申请

US20040245389A1 Cooled insulation surface temperature control system 有权
标题翻译：冷却绝缘表面温度控制系统
公开(公告)号：US20040245389A1
公开(公告)日：2004-12-09
申请号：US10455204
申请日：2003-06-05
发明人： William W. Behrens , Andrew R. Tucker , James E. French , Gayl J. Miller
IPC分类号： B64C001/00
CPC分类号： F28F13/003 , B64C1/38 , B64G1/58 , F28D2021/0078
摘要： An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surface of the porous layer to prevent erosion of the porous layer and to facilitate surface film cooling.
摘要翻译：提供了表面温度控制的装置和方法。表面温度控制是通过将冷却剂流入并连接到结构气室附近的低强度多孔层而实现的。半透层可以附着在多孔层的外表面上，以防止多孔层的腐蚀并促进表面膜冷却。

60. 发明授权

US06472601B2 Electrically-conductive, thermally-insulating structure and method 有权
标题翻译：导电，绝热结构和方法
公开(公告)号：US06472601B2
公开(公告)日：2002-10-29
申请号：US09772757
申请日：2001-01-30
申请人： David L. Hunn , Barry W. Bartos
发明人： David L. Hunn , Barry W. Bartos
IPC分类号： H01B700
CPC分类号： C23C4/02 , B64C1/38 , B64C1/40 , C23C28/00
摘要： An electrically-conductive, thermally-insulating structure includes a thermally-insulating layer having a thermal conductivity of no more than about 3.5×10−3 W/hr·cm·°K and an electrically-conductive layer, applied to the thermally-insulating layer, which has an electrical resistivity of no more than about five ohms at 700° C. The thermally-insulating layer can include a plurality of microballoons to decrease the density of the thermally-insulating layer.
摘要翻译：导电的绝热结构包括热导率不大于约3.5×10-3W / hr·cm·K的绝热层，以及施加到绝热层的导电层，其在700℃下的电阻率不超过约5欧姆。绝热层可以包括多个微球，以降低绝热层的密度。

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