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1. 发明公开

EP2879956A2 VALVE FOR AN AIRCRAFT 失效转让
标题翻译：阀用于飞机投掷的的燃料罐
公开(公告)号：EP2879956A2
公开(公告)日：2015-06-10
申请号：EP13736579.7
申请日：2013-07-12
申请人： Eaton Limited
发明人： POWELL, Melvyn
IPC分类号： B64D37/12 , B64D37/00
CPC分类号： B64D37/12 , B64D37/005 , F16J15/187 , F16J15/3224 , F16K1/465 , F16K27/02 , F16L1/00 , F16L27/06 , F16L29/02
摘要： A valve for connecting an external tank to an aircraft has a valve body; and a seal assembly arranged, in use, to resiliently engage a seal surface on an aircraft. The seal assembly has a telescopic seal member extending from a proximal end within the valve body to a distal end. The telescopic seal member is constrained within the valve body so as to maintain axial alignment of the telescopic seal member and the valve body. The seal assembly may also have a seal carrier at the distal end of the telescopic seal member. The seal carrier may be pivotable relative to the telescopic seal member for alignment, in use, with the aircraft seal surface.

2. 发明公开

EP2293982A1 FUEL JETTISON SYSTEM 失效
标题翻译：燃油排放系统
公开(公告)号：EP2293982A1
公开(公告)日：2011-03-16
申请号：EP08768873.5
申请日：2008-01-28
申请人： Sikorsky Aircraft Corporation
发明人： MORGIA, James J. , CUTTING, Anthony P.
IPC分类号： B64D37/26
CPC分类号： B64D37/12 , B64D37/26 , Y02T50/44
摘要： A fuel jettison system which provides pilot-initiated automatic operation to jettison fuel down to a 60 minute useable fuel remaining level while the manual operation, requiring the pilot to hold down the jettison panel switch, jettisons fuel down to a 20-minute useable fuel remaining level. The pilot can interrupt jettisoning at any time. This termination sequence operates in either automatic or manual mode. The port and starboard main fuel tanks jettison fuel independently through independent shutoff valves and associated circuit logic to thereby maintain aircraft balance.

3. 发明授权

EP2293982B1 FUEL JETTISON SYSTEM 失效
公开(公告)号：EP2293982B1
公开(公告)日：2018-12-12
申请号：EP08768873.5
申请日：2008-01-28
申请人： Sikorsky Aircraft Corporation
发明人： MORGIA, James J. , CUTTING, Anthony P.
IPC分类号： B64D37/26 , B64D37/12
CPC分类号： B64D37/12 , B64D37/26 , Y02T50/44
摘要： A fuel jettison system which provides pilot-initiated automatic operation to jettison fuel down to a 60 minute useable fuel remaining level while the manual operation, requiring the pilot to hold down the jettison panel switch, jettisons fuel down to a 20-minute useable fuel remaining level. The pilot can interrupt jettisoning at any time. This termination sequence operates in either automatic or manual mode. The port and starboard main fuel tanks jettison fuel independently through independent shutoff valves and associated circuit logic to thereby maintain aircraft balance.

4. 发明授权

EP2879956B1 VALVE FOR A JETTISONABLE AIRCRAFT FUEL TANK 失效转让
标题翻译：阀用于飞机投掷的的燃料罐
公开(公告)号：EP2879956B1
公开(公告)日：2016-04-27
申请号：EP13736579.7
申请日：2013-07-12
申请人： Eaton Limited
发明人： POWELL, Melvyn
IPC分类号： F16K27/00
CPC分类号： B64D37/12 , B64D37/005 , F16J15/187 , F16J15/3224 , F16K1/465 , F16K27/02 , F16L1/00 , F16L27/06 , F16L29/02
摘要： A valve for connecting an external tank to an aircraft has a valve body; and a seal assembly arranged, in use, to resiliently engage a seal surface on an aircraft. The seal assembly has a telescopic seal member extending from a proximal end within the valve body to a distal end. The telescopic seal member is constrained within the valve body so as to maintain axial alignment of the telescopic seal member and the valve body. The seal assembly may also have a seal carrier at the distal end of the telescopic seal member. The seal carrier may be pivotable relative to the telescopic seal member for alignment, in use, with the aircraft seal surface.

5. 发明公开

EP1616787A1 Ablenkvorrichtung für einen Strömungskörper 有权
标题翻译： Betankungs-Pod eines Flugzeuges mit geschlepptem Betankungsschlauch
公开(公告)号：EP1616787A1
公开(公告)日：2006-01-18
申请号：EP05015539.9
申请日：2005-07-18
申请人： Airbus Deutschland GmbH
发明人： Lejeau, Damien , Schwetzler, Detlev , Aumann, Petra
IPC分类号： B64D39/00 , B64C23/06
CPC分类号： B64C23/06 , B64C2003/145 , B64D37/12 , B64D39/00 , Y02T50/162
摘要： Die vorliegende Erfindung betrifft eine Ablenkvorrichtung (2) z.B. für einen stumpfen Strömungskörper (8). Die Ablenkvorrichtung (2) weist eine Kante auf, die z.B. an dem Strömungskörper (8) anbringbar ist. Die Ablenkvorrichtung (2) ermöglicht vorteilhaft eine Beeinflussung der Nachlaufströmung derart, dass Turbulenzen, die mit der Nachlaufströmung in Verbindung stehen und sich hinter stumpfen Strömungskörpern ausbilden, einen möglichst geringen Einfluss auf das geschleppte Objekt haben, um zu verhindern, dass Aufschaukelbewegungen des geschleppten Objektes entstehen, die zu Instabilitäten führen.
摘要翻译：偏转器具有表面（4）的边缘。表面（4）是局部流动方向（13）的下注。偏转器可在主体（8）的一端附接（2）。导弹成形为导弹（8）。导弹具有钝的形式，其中可以附接拖动探针（20）。在身体后方的流动方向，发展出湍流。牵引探针的第一部分具有布置的具有第一长度（28）的偏转器。提供了拖曳探头（20）的第二部分的第二长度（24），其处于湍流范围内，并且比第一长度长。

6. 发明公开

EP3140576A4 FUEL SYSTEM BREAKAWAY VALVE REACTION BRIDGE AND REACTION COLLAR 有权
公开(公告)号：EP3140576A4
公开(公告)日：2018-01-03
申请号：EP15789860
申请日：2015-05-06
申请人： SIKORSKY AIRCRAFT CORP
发明人： CHASEN SCOTT A , ROGSTAD ROBERT R , BIEHL CHRIS JOHN
IPC分类号： F16K17/40 , B64D37/14
CPC分类号： B64D37/12 , B64D37/005 , B64D37/14 , F16K17/40
摘要： A flexible fuel bladder assembly for an aircraft includes a flexible fuel bladder positioned at an airframe and having an opening to allow a flow of fuel into and/or out of the fuel bladder. A breakaway valve is operably connected to the fuel bladder at the opening to control a flow of fuel therethrough. A non-contacting or loose fitting reaction feature is affixed to the airframe and is interactive with the breakaway valve such that movement of the breakaway valve relative to the reaction feature results in breakage of a valve body of the breakaway valve and closure of the breakaway valve to prevent flow of fuel therethrough while also allowing for a second reaction mode to cause breakage of a valve body should the connecting hose be pulled relative to the breakaway valve.

7. 发明公开

EP2293982A4 FUEL JETTISON SYSTEM 失效
标题翻译：燃油排放系统
公开(公告)号：EP2293982A4
公开(公告)日：2013-09-11
申请号：EP08768873
申请日：2008-01-28
申请人： SIKORSKY AIRCRAFT CORP
发明人： MORGIA JAMES J , CUTTING ANTHONY P
IPC分类号： B64D37/26 , B64D37/12
CPC分类号： B64D37/12 , B64D37/26 , Y02T50/44
摘要： A fuel jettison system which provides pilot-initiated automatic operation to jettison fuel down to a 60 minute useable fuel remaining level while the manual operation, requiring the pilot to hold down the jettison panel switch, jettisons fuel down to a 20-minute useable fuel remaining level. The pilot can interrupt jettisoning at any time. This termination sequence operates in either automatic or manual mode. The port and starboard main fuel tanks jettison fuel independently through independent shutoff valves and associated circuit logic to thereby maintain aircraft balance.

8. 发明公开

EP1509449A2 SYSTEM AND METHOD FOR ENHANCING THE FUEL STORAGE VOLUME AND THE FUEL CARRIAGE CAPACITY OF EXTERNAL FUEL STORES CARRIED BY AN AERIAL VEHICLE 审中-公开
标题翻译：系统和方法改进燃料存储卷和飞机的载油量能力起至外部燃料储存
公开(公告)号：EP1509449A2
公开(公告)日：2005-03-02
申请号：EP02793286.2
申请日：2002-12-04
申请人： Padan, Nir
发明人： Padan, Nir
IPC分类号： B64D37/00
CPC分类号： B64D37/12
摘要： A system and method for enhancing the fuel stores volume of an aerial vehicle (10) is disclosed. An extended external fuel stores configuration utilizes an alternative fuel transfer path. An external fuel tank (3, 7)is suspended on a external fuel tank carrier pylon (102) uploaded on a outboard wing 'pseudo-wet' stores station. The pylon is linked to a dual functionality external fuel tank carrier pylon (104) uploaded on an inboard wing 'wet' station. The pylon (104) is capable of transmitting, and controlling the fuel store in the auxiliary fuel container (3, 7) attached to the pylon (102) uploaded on a outboard wing 'pseudo-wet' station. An externally mounted stores transfer kit links the inboard pylon (104) and the outboard pylon (102).

9. 发明公开

EP3140576A1 FUEL SYSTEM BREAKAWAY VALVE REACTION BRIDGE AND REACTION COLLAR 有权
标题翻译：燃油系统断流阀反应桥和反应线圈
公开(公告)号：EP3140576A1
公开(公告)日：2017-03-15
申请号：EP15789860.2
申请日：2015-05-06
申请人： Sikorsky Aircraft Corporation
发明人： CHASEN, Scott A. , ROGSTAD, Robert R. , BIEHL, Chris John
IPC分类号： F16K17/40
CPC分类号： B64D37/12 , B64D37/005 , B64D37/14 , F16K17/40
摘要： A flexible fuel bladder assembly for an aircraft includes a flexible fuel bladder positioned at an airframe and having an opening to allow a flow of fuel into and/or out of the fuel bladder. A breakaway valve is operably connected to the fuel bladder at the opening to control a flow of fuel therethrough. A non-contacting or loose fitting reaction feature is affixed to the airframe and is interactive with the breakaway valve such that movement of the breakaway valve relative to the reaction feature results in breakage of a valve body of the breakaway valve and closure of the breakaway valve to prevent flow of fuel therethrough while also allowing for a second reaction mode to cause breakage of a valve body should the connecting hose be pulled relative to the breakaway valve.
摘要翻译：用于飞行器的柔性燃料囊组件包括定位在机身处并具有开口以允许燃料流入和/或流出燃料囊的柔性燃料囊。分离阀在开口处可操作地连接到燃料囊以控制燃料从中流过。非接触或松散配合反作用特征固定在机身上并与分离阀交互作用，使得分离阀相对于反应特征的运动导致分离阀的阀体破裂并关闭分离阀以防止燃料从中流过，同时如果连接软管相对于分离阀拉动，也允许第二反应模式导致阀体破裂。

10. 发明公开

EP3075657A1 MULTIFUNKTIONS-POD FÜR EIN FLUGZEUG 有权
标题翻译： MULTIFUNKTIONS-PODFÜREIN FLUGZEUG
公开(公告)号：EP3075657A1
公开(公告)日：2016-10-05
申请号：EP16162160.2
申请日：2016-03-24
申请人： Airbus Defence and Space GmbH
发明人： Christof, Horst
IPC分类号： B64D1/04 , B64D7/00 , B64D37/12 , F41F7/00
CPC分类号： B64D1/08 , B64D1/04 , B64D7/00 , B64D37/12 , F41F3/052 , F41F3/06 , F41F3/065 , F41F5/00
摘要： Es wird ein Multifunktions-Pod für ein Flugzeug angegeben, der mindestens zwei voneinander getrennte Bereiche (3, 4) aufweist. Mindestens ein erster Bereich (3) des Pods ist zur Aufnahme von Treibstoff vorgesehen. Ein zweiter Bereich (4) des Pods weist mindestens eine Aufnahmevorrichtung (41) zur lösbaren Anbringung mindestens einer weiteren Last (42) auf. Die weitere Last (42) ist über eine an der dem Flugzeug abgewandten Seite des Pods aufweisende Ladeöffnung (11) an der Aufnahmevorrichtung (41) lösbar anbringbar.
摘要翻译：飞机的多功能吊舱至少有两个独立的区域。提供荚的至少一个第一区域用于接收燃料。荚的第二区域包括至少一个用于可释放地附接至少一个附加负载的接收装置。额外的负载可以通过在面向远离飞机的舱的一侧上的装载开口可释放地附接到接收装置。

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