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

EP3106839A1 SENSOR SYSTEM FOR LAMINATED STRUCTURES 有权
标题翻译：传感器FÜRLAMINIERTE STRUKTUREN
公开(公告)号：EP3106839A1
公开(公告)日：2016-12-21
申请号：EP16173039.5
申请日：2016-06-06
申请人： The Boeing Company
发明人： PECK, James L. Jr. , MULEY, Arun
IPC分类号： G01D5/353 , G01L1/24
CPC分类号： G01L1/241 , G01B11/002 , G01B11/16 , G01D5/268 , G01D5/30 , G01D5/353 , G01D5/35316 , G01D5/3537 , G01K1/08 , G01K7/00 , G01K11/32 , G01K11/3206 , G01L1/18 , G01L1/242 , G01L1/246 , G01L1/247 , G02B6/3608
摘要： A sensor system for a laminated structure may include a sensor assembly disposed between a first layer and a second layer of the laminated structure. The sensor assembly may include a first anchor member and a second anchor member spaced at a predetermined distance from one another. A sensor chamber is formed between the first and second anchor members. The sensor assembly may also include a sensing line extending through the anchor members and the sensor chamber. The sensing line may include a configuration within the sensor chamber for sensing one of stress forces within the laminated structure, temperature or temperature changes within the laminated structure. A first transport tube may extend from the first anchor member opposite the sensor chamber and a second transport tube may extend from the second anchor member opposite the sensor chamber. The sensing line extends through the first and second transport tubes.
摘要翻译：用于层压结构的传感器系统可以包括设置在层压结构的第一层和第二层之间的传感器组件。传感器组件可以包括彼此隔开预定距离的第一锚定构件和第二锚定构件。传感器室形成在第一和第二锚构件之间。传感器组件还可以包括延伸穿过锚定构件和传感器室的感测线。感测线可以包括传感器室内的结构，用于感测层压结构内的应力之一，层压结构内的温度或温度变化。第一输送管可以从与传感器室相对的第一锚定构件延伸，并且第二输送管可以从与传感器室相对的第二锚定构件延伸。感测线延伸穿过第一和第二输送管。

2. 发明授权

EP3106839B1 SENSOR SYSTEM FOR LAMINATED STRUCTURES 有权
公开(公告)号：EP3106839B1
公开(公告)日：2018-08-15
申请号：EP16173039.5
申请日：2016-06-06
申请人： The Boeing Company
发明人： PECK, James L. Jr. , MULEY, Arun
IPC分类号： G01D5/353 , G01L1/24
CPC分类号： G01L1/241 , G01B11/002 , G01B11/16 , G01D5/268 , G01D5/30 , G01D5/353 , G01D5/35316 , G01D5/3537 , G01K1/08 , G01K7/00 , G01K11/32 , G01K11/3206 , G01L1/18 , G01L1/242 , G01L1/246 , G01L1/247 , G02B6/3608
摘要： A sensor system for a laminated structure may include a sensor assembly disposed between a first layer and a second layer of the laminated structure. The sensor assembly may include a first anchor member and a second anchor member spaced at a predetermined distance from one another. A sensor chamber is formed between the first and second anchor members. The sensor assembly may also include a sensing line extending through the anchor members and the sensor chamber. The sensing line may include a configuration within the sensor chamber for sensing one of stress forces within the laminated structure, temperature or temperature changes within the laminated structure. A first transport tube may extend from the first anchor member opposite the sensor chamber and a second transport tube may extend from the second anchor member opposite the sensor chamber. The sensing line extends through the first and second transport tubes.

3. 发明公开

EP3210885A1 STRUCTURALLY INTEGRATED THERMAL MANAGEMENT SYSTEM FOR AEROSPACE VEHICLES 有权
标题翻译：飞行器结构综合热管理系统
公开(公告)号：EP3210885A1
公开(公告)日：2017-08-30
申请号：EP17158529.2
申请日：2017-02-28
申请人： The Boeing Company
发明人： BLANDING, David E. , MULEY, Arun , COFFMAN, Jeffrey C. , VAN AFFELEN, Doug
IPC分类号： B64C9/00 , B64C13/50 , B64G1/50
CPC分类号： B64G1/50 , B64C3/185 , B64C3/187 , B64C9/00 , B64C13/50 , B64D13/08 , Y02T50/32 , Y02T50/44 , Y02T50/54
摘要： Disclosed examples include a structurally integrated thermal management system that uses the structure of an aerospace vehicle as part of the heat dissipation system. In this system, structural elements of the aerospace vehicle function as a thermal bus, and are thermally connected with heat-generating electrical components, so that heat from those components is directed away from the component by the structure of the vehicle itself, into lower temperature surfaces of the vehicle.
摘要翻译：所公开的示例包括结构上集成的热管理系统，其使用航空交通工具的结构作为散热系统的一部分。在该系统中，航空飞行器的结构元件起到热母线的作用，并且与发热的电气元件热连接，使得来自这些元件的热量通过车辆本身的结构被引导离开该元件进入较低的温度车辆的表面。

4. 发明公开

EP4001599A1 METHODS AND SYSTEMS FOR GENERATING POWER AND THERMAL MANAGEMENT HAVING COMBINED CYCLE ARCHITECTURE 有权转让
公开(公告)号：EP4001599A1
公开(公告)日：2022-05-25
申请号：EP21194085.3
申请日：2021-08-31
申请人： The Boeing Company
发明人： EK, Garrett W. , STOIA, Michael F. , MULEY, Arun , NEEDELS, Jacob T. , BOWCUTT, Kevin G.
IPC分类号： F01K23/04 , F01K23/10 , F01K7/32 , B64C1/38 , B64D13/00
摘要： Methods and apparatus for cooling a surface on a flight vehicle and generating power include advancing the vehicle at a speed of at least Mach 3 to aerodynamically heat the surface. A first working fluid circulates through a first fluid loop that heats the first working fluid through a heat intake thermally coupled to the surface and expands the first working fluid in a first thermal engine to generate a first work output. A second fluid loop has a second working fluid that receives heat from the first working fluid and a second thermal engine to generate a second work output. The first and second work outputs are operably coupled to first and second generators, respectively, to power primary or auxiliary systems on the flight vehicle.

5. 发明公开

EP3346220A1 HEAT PIPE WITH NON-UNIFORM CROSS-SECTION 有权
公开(公告)号：EP3346220A1
公开(公告)日：2018-07-11
申请号：EP17206431.3
申请日：2017-12-11
申请人： The Boeing Company
发明人： DROLEN, Bruce Lee , VAN AFFELEN, Douglas H. , MULEY, Arun , STOIA, Michael F.
IPC分类号： F28F1/40 , F28F13/08 , F28F1/00
CPC分类号： F28D15/0266 , B23P15/26 , B23P2700/09 , B33Y10/00 , F28D15/0233 , F28D15/046 , F28D2021/0021 , F28F1/006 , F28F1/40 , F28F13/08 , F28F2215/04
摘要： A heat pipe (101) comprises a tube (112) and protrusions (114). The tube (112) has an internal surface (116), an external surface (118), and a length (120) running from a first end (122) to a second end (124). The protrusions (114) are on the internal surface (116). A first cross-section (156) of the protrusions (114) at a first location of the length (120) of the tube (112) is different from a second cross-section (158) of the protrusions (114) at a second location of the length (120) of the tube (112). The tube (112) and the protrusions (114) are monolithic (125).

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