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1. 发明申请

US20060284018A1 VALVES FOR ANNULAR CONDUITS INCLUDING AIRCRAFT FUEL CONDUITS AND ASSOCIATED SYSTEMS AND METHODS 有权
标题翻译：用于包括飞机燃料导管和相关系统和方法的电磁阀的阀门
公开(公告)号：US20060284018A1
公开(公告)日：2006-12-21
申请号：US11147138
申请日：2005-06-07
申请人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
发明人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
IPC分类号： B64D39/00
CPC分类号： B64D39/06 , F16L3/1222 , F16L39/005 , F16L2201/30
摘要： Valves for annular conduits and associated systems and methods are disclosed. A fluid transmission system in accordance with one embodiment of the invention includes a first conduit having a first wall aligned with a flow direction in the first conduit and a second conduit disposed annularly around the first conduit with a second wall aligned with the flow direction. An access channel can be positioned to have an aperture in fluid communication with the first conduit and can be isolated from fluid communication with the second conduit. A valve element can be positioned in fluid communication with the access channel and can be movable between a first position and a second position, with the valve element being positioned to allow a first amount of flow through the access channel when in the first position and being positioned to allow no flow or a second amount of flow less than the first amount of flow through the access channel when in the second position. The valve can be installed in aircraft fuel lines or other systems.
摘要翻译：公开了用于环形导管和相关系统和方法的阀。根据本发明的一个实施例的流体传动系统包括第一管道，其具有与第一管道中的流动方向对准的第一壁和围绕第一管道设置的第二管道，第二管道具有与流动方向对准的第二壁。进入通道可以被定位成具有与第一管道流体连通的孔，并且可以与第二管道的流体连通隔离。阀元件可以定位成与进入通道流体连通，并且可以在第一位置和第二位置之间移动，其中阀元件被定位成允许在处于第一位置时通过进入通道的第一量的流量定位成当处于第二位置时不允许流过或接近通道的第一流量小于第一流量。阀门可以安装在飞机燃油管路或其他系统中。

2. 发明申请

US20060278763A1 Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, and associated systems and methods 有权
公开(公告)号：US20060278763A1
公开(公告)日：2006-12-14
申请号：US11440726
申请日：2006-05-24
申请人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
发明人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
IPC分类号： B64D39/00
CPC分类号： F16L3/1226 , B64D39/06 , Y10T29/494 , Y10T29/49826
摘要： Adjustable fittings for attaching support members to fluid conduits, including aircraft fuel conduits, are disclosed herein. An aircraft system in accordance with one embodiment of the invention includes a fluid conduit carried by an aircraft and a housing fixedly attached to the fluid conduit. The housing can include a first attachment feature having one of a projection extending outwardly from the housing or an aperture extending at least partially through the housing. The system further includes a support member having an attachment portion positioned proximate to the attachment feature. The attachment portion includes a support member aperture positioned over at least a portion of the first attachment feature. An adjustable fitting couples the support member to the housing. The adjustable fitting can include a first side, a second side opposite the first side, and an engagement portion at the second side positioned within at least a portion of the support member aperture. The fitting can also include a second attachment feature mated with the first attachment feature. The second attachment feature includes the other one of the projection or the aperture. The second attachment feature has a center point eccentrically offset from a center point of the fitting.

3. 发明申请

US20060278760A1 Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems 有权
公开(公告)号：US20060278760A1
公开(公告)日：2006-12-14
申请号：US11301131
申请日：2005-12-12
申请人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
发明人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
IPC分类号： B64D39/00
CPC分类号： B64D39/06 , F16L5/06 , F16L5/08 , F16L39/005 , F16L2201/30
摘要： Fittings with redundant seals for aircraft fuel lines, fuel tanks, and other systems are disclosed. A fitting in accordance with one embodiment can be positioned adjacent to an aperture in a fuel tank wall having an inner surface and an outer surface. The fitting can include a first member having a flange and a barrel. The barrel can further include a passageway. A first flange seal can be positioned at a face of the flange and can be sealably coupled to a surface, for example, the tank wall. A second flange seal can be disposed outwardly from the first flange seal against the surface. The fitting can further include a second member (e.g., a sensor) positioned within the passageway of the barrel. The fitting can further include first and second barrel seals positioned between the barrel and the second member.

4. 发明申请

US20070051406A1 Shrouded valve apparatus and related methods 有权
标题翻译：有盖阀门装置及相关方法
公开(公告)号：US20070051406A1
公开(公告)日：2007-03-08
申请号：US11150853
申请日：2005-06-10
申请人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
发明人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
IPC分类号： F16K23/00
CPC分类号： F16K1/22 , F16K27/0218 , F16K37/0066 , F16L39/005 , Y10T137/0318 , Y10T137/5762 , Y10T137/87153
摘要： A shrouded valve apparatus including an outer conduit, an inner conduit disposed within the outer conduit, and a valve member operable to regulate flow through the inner conduit. This apparatus is useful in shrouded aircraft fuel systems.
摘要翻译：一种带盖的阀门装置，包括外部导管，设置在外部导管内部的内部导管，以及可操作以调节通过内部导管的流动的阀构件。该装置在被覆盖的飞机燃料系统中是有用的。

5. 发明申请

US20060278759A1 System and methods for distributing loads from fluid conduits, including aircraft fuel conduits 有权
标题翻译：用于从流体管道（包括飞机燃料管道）分配负载的系统和方法
公开(公告)号：US20060278759A1
公开(公告)日：2006-12-14
申请号：US11150005
申请日：2005-06-09
申请人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
发明人： James Carns , Theron Cutler , Mark Shelly , Benjamin Van Kampen
IPC分类号： B64D39/00
CPC分类号： F16L3/00 , B64D39/06 , Y10T29/49826
摘要： Systems and methods for distributing loads from fluid conduits, including aircraft fuel conduits, are disclosed. An aircraft configured in accordance with one embodiment of the invention includes a fuselage portion, a wing portion, and a fuel tank carried by least one of the fuselage portion and the wing portion. The aircraft also includes a spar carried by at least one of the fuselage portion and the wing portion. The spar includes a first spar rib and a second spar rib spaced apart from the first spar rib. The aircraft further includes a fluid conduit proximate to the spar and operably coupled to the fuel tank. A support member carrying the fluid conduit is operably coupled to the spar. The support member can be positioned to transfer at least approximately all of the axial loads from the fluid conduit to at least one of the first spar rib and the second spar rib.
摘要翻译：公开了用于从流体管道（包括飞机燃料管道）分配负载的系统和方法。根据本发明的一个实施例构造的飞机包括由机身部分和翼部分中的至少一个承载的机身部分，翼部分和燃料箱。飞机还包括由机身部分和机翼部分中的至少一个承载的翼梁。翼梁包括与第一翼梁相隔开的第一翼梁和第二翼梁。飞机还包括靠近翼梁的流体导管并且可操作地联接到燃料箱。承载流体导管的支撑构件可操作地联接到翼梁。支撑构件可以被定位成将来自流体导管的至少几乎所有轴向载荷传递到第一翼梁肋和第二翼梁中的至少一个。

6. 发明申请

US20060278017A1 Shrouded body flow meter assembly 有权
标题翻译：有罩体流量计总成
公开(公告)号：US20060278017A1
公开(公告)日：2006-12-14
申请号：US11450925
申请日：2006-06-09
申请人： James Carns , Theron Cutler , Mark Shelly
发明人： James Carns , Theron Cutler , Mark Shelly
IPC分类号： G01F1/05
CPC分类号： G01F1/10 , G01F1/115 , G01F15/14 , G01F15/185 , G01N9/24
摘要： A shrouded body flow meter assembly includes an inner fluid-conducting conduit disposed in a spaced relation from and within an outer conduit. The shrouded flow meter assembly can be connected to other shrouded fluid-conducting apparatus and/or used to replace sections of a shrouded fluid-conducting apparatus system. The shrouded flow meter assembly maintains the integrity of the inner fluid-conducting conduits and outer conduits of the shrouded fluid-conducting apparatus.
摘要翻译：被罩身体流量计组件包括以与外管道间隔开的关系设置的内部流体导管。被覆盖的流量计组件可以连接到其它被覆盖的流体传导装置和/或用于替换被覆盖的流体传导装置系统的部分。被覆盖的流量计组件保持被覆盖的流体传导装置的内部导流管道和外部导管的完整性。

7. 发明申请

US20050120534A1 Shrouded fluid-conducting apparatus 审中-公开
标题翻译：带罩的导液装置
公开(公告)号：US20050120534A1
公开(公告)日：2005-06-09
申请号：US10988309
申请日：2004-11-13
申请人： James Carns , Theron Cutler , Mark Shelly
发明人： James Carns , Theron Cutler , Mark Shelly
IPC分类号： F16L39/00 , B23P11/00
CPC分类号： F16L39/005 , B64D37/005 , B64D37/32 , F16L23/167 , F16L25/01 , F16L2201/30 , H01R4/643 , Y10T29/49826 , Y10T29/53443
摘要： A shrouded fluid-conducting apparatus is provided that includes at least one outer conduit and at least one inner conduit disposed within the outer conduit. Preferably, the shrouded fluid-conducting apparatus further includes at least one shrouded end fitting disposed at an end of the shrouded fluid-conducting apparatus and at least one support member engaged with the inner and outer conduits. The shrouded end fitting allows the shrouded fluid-conducting apparatus to be engaged with an additional shrouded fluid-conducting apparatus. The support member allows for the transfer of loads from the inner and/or outer conduits to one or more components external to the shrouded fluid-conducting apparatus. Accordingly, the shrouded fluid-conducting apparatus may be used to transport fuel through an aircraft “ignition zone” in an FAA-compliant manner.
摘要翻译：提供了一种被覆盖的流体传导装置，其包括至少一个外管道和设置在外管道内的至少一个内管道。优选地，被覆盖的流体传导装置还包括设置在被覆盖的流体传导装置的端部处的至少一个被覆盖的端部配件和与内部和外部导管接合的至少一个支撑构件。被覆盖的端部配件允许被覆盖的流体传导装置与附加的被覆盖的流体传导装置接合。支撑构件允许将负载从内部管道和/或外部管道传递到被覆盖的流体传导装置外部的一个或多个部件。因此，被覆盖的导流装置可以用于以符合FAA的方式将燃料运输通过飞行器“点燃区域”。

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