-
公开(公告)号：US09517830B2
公开(公告)日：2016-12-13
申请号：US14217673
申请日：2014-03-18
Applicant: The Boeing Company
Inventor： Sham S. Hariram , Paul B. Philipp
CPC classification number: B64C1/1407 , B60J10/24 , B60J10/38 , B64C1/066 , E06B7/16 , F16J15/104 , F16J15/121
Abstract: Provided is a captured seal assembly that can be positioned between a first surface and a second surface of a structure or vehicle, such as an aircraft. The captured seal assembly includes a geometric-shaped seal such as a bulb-shaped seal that can be secured to an outer perimeter of the first surface and a receiving land capture that can be secured to an outer perimeter of the second surface. The geometric-shaped seal is designed to engage with the receiving land capture, and join the first surface and second surface when the geometric-shaped seal is engaged with the receiving land capture. In addition, the seal assembly can maintain a differential in pressure between a first region adjacent to the first surface and a second region adjacent to the second surface.
Abstract translation: 提供了可以被定位在诸如飞行器的结构或车辆的第一表面和第二表面之间的捕获的密封组件。 捕获的密封组件包括几何形状的密封件，例如可固定到第一表面的外周边的球形密封件，以及可固定到第二表面的外周边的接收平台捕获。 几何形状的密封件被设计成与接收区域捕获接合，并且当几何形状的密封件与接收区域捕获接合时，将第一表面和第二表面接合。 此外，密封组件可以保持与第一表面相邻的第一区域与邻近第二表面的第二区域之间的压力差。
-
公开(公告)号：US20160138958A1
公开(公告)日：2016-05-19
申请号：US14547828
申请日：2014-11-19
Applicant: THE BOEING COMPANY
Inventor： Tuong K. Truong , Dennis G. Koshinz , Eric Y. Chan , Todd C. Thomas , J. Everett Groat , Sigvard J. Wahlin , John L. Vento , Sham S. Hariram , Richard J. Nesting
IPC: G01F23/292
CPC classification number: G01F23/292 , B64D37/005 , G01F22/00 , Y02T50/44
Abstract: Systems and methods that use an optical impedance sensor that eliminates electricity for measuring fuel quantity in fuel tanks. The optical impedance sensor comprises two optical fibers spaced apart inside a meniscus tube, one to transmit light along its length and the other to receive light along its length. The meniscus tube minimizes the sloshing of fuel level. The fuel level in the tank modulates the optical impedance between the two optical fibers, resulting in changes in the total light received by an optical detector. Depending on fuel tank height, the optical impedance sensor may comprise different embodiments in which the detection apparatus shapes the light to be unidirectional (emitted and collected only on one side of the fiber) or omnidirectional (all directions).
Abstract translation: 使用光阻抗传感器的系统和方法，消除用于测量燃料箱中燃料量的电力。 光阻抗传感器包括在弯液面管内分开的两根光纤，一根沿其长度透射光线的光纤，另一根光纤沿其长度接收光。 弯液面管使燃油液位的晃动最小化。 油箱中的燃油液位调制两根光纤之间的光阻抗，导致由光学检测器接收到的总光的变化。 根据燃料箱高度，光阻抗传感器可以包括不同的实施例，其中检测装置将光形成单向（仅在光纤的一侧发射和收集）或全向（所有方向）。
-
公开(公告)号：US20150297923A1
公开(公告)日：2015-10-22
申请号：US14523741
申请日：2014-10-24
Applicant: The Boeing Company
Inventor： Sham S. Hariram
CPC classification number: A62C3/08 , A62C3/002 , B32B9/04 , B32B15/04 , B32B27/06 , B32B37/10 , B32B37/12 , B32B37/18 , B32B2307/3065 , B32B2307/718 , B32B2605/08 , B32B2605/18 , B65D90/022 , B65D90/22
Abstract: A fire-retarding apparatus includes a composite. The composite includes a face layer attached to a fire-retarding layer.
Abstract translation: 阻燃装置包括复合材料。 复合材料包括附着在阻燃层上的面层。
-
公开(公告)号：US20150266561A1
公开(公告)日：2015-09-24
申请号：US14217673
申请日：2014-03-18
Applicant: The Boeing Company
Inventor： Sham S. Hariram , Paul B. Philipp
CPC classification number: B64C1/1407 , B60J10/24 , B60J10/38 , B64C1/066 , E06B7/16 , F16J15/104 , F16J15/121
Abstract: Provided is a captured seal assembly that can be positioned between a first surface and a second surface of a structure or vehicle, such as an aircraft. The captured seal assembly includes a geometric-shaped seal such as a bulb-shaped seal that can be secured to an outer perimeter of the first surface and a receiving land capture that can be secured to an outer perimeter of the second surface. The geometric-shaped seal is designed to engage with the receiving land capture, and join the first surface and second surface when the geometric-shaped seal is engaged with the receiving land capture. In addition, the seal assembly can maintain a differential in pressure between a first region adjacent to the first surface and a second region adjacent to the second surface.
Abstract translation: 提供了可以被定位在诸如飞行器的结构或车辆的第一表面和第二表面之间的捕获的密封组件。 捕获的密封组件包括几何形状的密封件，例如可固定到第一表面的外周边的球形密封件，以及可固定到第二表面的外周边的接收平台捕获。 几何形状的密封件被设计成与接收区域捕获接合，并且当几何形状的密封件与接收区域捕获接合时，将第一表面和第二表面接合。 此外，密封组件可以保持与第一表面相邻的第一区域与邻近第二表面的第二区域之间的压力差。
-
公开(公告)号：US20150069068A1
公开(公告)日：2015-03-12
申请号：US14021542
申请日：2013-09-09
Applicant: The Boeing Company
Inventor： Sham S. Hariram
Abstract: A container includes a fire-retarding material, a substantially airtight cavity, and a reinforcement material. The substantially airtight cavity is formed by the fire-retarding material and is sized to hold at least one item. The reinforcement material is connected with the fire-retarding material.
Abstract translation: 容器包括阻燃材料，基本上气密的空腔和增强材料。 基本上气密的空腔由阻燃材料形成，并且其尺寸适于容纳至少一个物品。 增强材料与阻燃材料连接。
-
Patent Agency Ranking
公开(公告)号：US10052508B2
公开(公告)日：2018-08-21
申请号：US14021542
申请日：2013-09-09
Applicant: The Boeing Company
Inventor： Sham S. Hariram
Abstract: A container includes a fire-retarding material, a substantially airtight cavity, and a reinforcement material. The substantially airtight cavity is formed by the fire-retarding material and is sized to hold at least one item. The reinforcement material is connected with the fire-retarding material.
-
公开(公告)号：US09969036B2
公开(公告)日：2018-05-15
申请号：US14542751
申请日：2014-11-17
Applicant: The Boeing Company
Inventor： Sham S. Hariram
IPC: B23P19/00 , F16L11/118 , F16L11/12 , F16L11/10
CPC classification number: B23P19/00 , F16L11/10 , F16L11/118 , F16L11/125
Abstract: Provided are fireproof flexible hoses, aircraft having fire suppression systems including such fireproof flexible hoses, and methods of forming such fireproof flexible hoses. A fireproof flexible hose includes an inner structure and an outer structure at least partially enclosing and directly interfacing the inner structure. The inner structure forms an inner surface of the fireproof flexible hose and includes a polyimide at least at the inner surface. The polyimide has good fireproofing and temperature resistant characteristics and, unlike other polymers, does not need to be thermally isolated when the hose is exposed to fire. The outer structure may be made from metal and/or non-metal and may provide mechanical support to the inner structure. The outer structure may have a convoluted shape to ensure flexibility of the overall hose assembly. In some examples, a set of gaps may be present between the outer and inner structures for additional flexibility.
-
公开(公告)号：US09645004B2
公开(公告)日：2017-05-09
申请号：US14547828
申请日：2014-11-19
Applicant: The Boeing Company
Inventor： Tuong K. Truong , Dennis G. Koshinz , Eric Y. Chan , Todd C. Thomas , J. Everett Groat , Sigvard J. Wahlin , John L. Vento , Sham S. Hariram , Richard J. Nesting
IPC: G01F23/292 , G01F22/00 , B64D37/00
CPC classification number: G01F23/292 , B64D37/005 , G01F22/00 , Y02T50/44
Abstract: Systems and methods that use an optical impedance sensor that eliminates electricity for measuring fuel quantity in fuel tanks. The optical impedance sensor comprises two optical fibers spaced apart inside a meniscus tube, one to transmit light along its length and the other to receive light along its length. The meniscus tube minimizes the sloshing of fuel level. The fuel level in the tank modulates the optical impedance between the two optical fibers, resulting in changes in the total light received by an optical detector. Depending on fuel tank height, the optical impedance sensor may comprise different embodiments in which the detection apparatus shapes the light to be unidirectional (emitted and collected only on one side of the fiber) or omnidirectional (all directions).
-
公开(公告)号：US10252091B2
公开(公告)日：2019-04-09
申请号：US14021690
申请日：2013-09-09
Applicant: The Boeing Company
Inventor： Sham S. Hariram
Abstract: A fire-retaining container is disclosed which includes a first fire-retarding layer and a second fire-retarding layer connected to the first fire-retarding layer. Another fire-retaining container is disclosed which includes a fire-retarding layer and a reinforcement material reinforcing the fire-retarding layer. A method of containing an item is disclosed. In one step, an item is covered with a fire-retaining container. The fire-retaining container comprises: (1) a first fire-retarding layer and a second fire-retarding layer connected to the first fire-retarding layer; or (2) a fire-retarding layer and a reinforcement material reinforcing the fire-retarding layer.
-
公开(公告)号：US20160138737A1
公开(公告)日：2016-05-19
申请号：US14542751
申请日：2014-11-17
Applicant: The Boeing Company
Inventor： Sham S. Hariram
CPC classification number: B23P19/00 , F16L11/10 , F16L11/118 , F16L11/125
Abstract: Provided are fireproof flexible hoses, aircraft having fire suppression systems including such fireproof flexible hoses, and methods of forming such fireproof flexible hoses. A fireproof flexible hose includes an inner structure and an outer structure at least partially enclosing and directly interfacing the inner structure. The inner structure forms an inner surface of the fireproof flexible hose and includes a polyimide at least at the inner surface. The polyimide has good fireproofing and temperature resistant characteristics and, unlike other polymers, does not need to be thermally isolated when the hose is exposed to fire. The outer structure may be made from metal and/or non-metal and may provide mechanical support to the inner structure. The outer structure may have a convoluted shape to ensure flexibility of the overall hose assembly. In some examples, a set of gaps may be present between the outer and inner structures for additional flexibility.
Abstract translation: 提供防火柔性软管，具有防火柔性软管的防火系统的飞机，以及形成这种防火柔性软管的方法。 防火柔性软管包括内部结构和外部结构，其至少部分地包围并直接接合内部结构。 内部结构形成防火柔性软管的内表面，并且至少在内表面包括聚酰亚胺。 聚酰亚胺具有良好的耐火和耐温特性，与其他聚合物不同，当软管暴露于火中时，不需要热隔离。 外部结构可以由金属和/或非金属制成并且可以为内部结构提供机械支撑。 外部结构可以具有卷曲形状以确保整个软管组件的柔性。 在一些示例中，可以在外结构和内结构之间存在一组间隙以获得额外的灵活性。
-
-
-
-
-
-
-
-
-
Search Results
11
records
(took 0.014 seconds)
