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1. 发明申请

WO2018202455A1 JOINT COVER WITH IMPROVED MANIFOLD BLOCK FOR DUCT LEAK DETECTION SYSTEM 审中-公开
公开(公告)号：WO2018202455A1
公开(公告)日：2018-11-08
申请号：PCT/EP2018/060307
申请日：2018-04-23
申请人： SENIOR IP GMBH
发明人： POSSERT, Eric , OWDEH, Muhannad , ALI, Karim
IPC分类号： B64D13/02 , F02C6/08 , F16L59/18 , B64D13/06
摘要： A manifold assembly (300) configured for integration with a joint cover apparatus in a ducting system to detect leaking gas comprises an elastomeric manifold block (303) having a substantially circular inlet aperture and one or more gas passages (307) (308) fluidly coupled to the inlet aperture. The assembly includes a flow control valve ((309) and (305)) configured to maintain a closed state in which a component (305) of the flow control valve sealedly engages with the inlet aperture (306) to preclude gas at the inlet aperture from flowing into the one or more gas passages until said gas reaches a pressure corresponding to a pressure threshold. The assembly also includes at least one aperture control plate (304) disposed substantially proximate to a lower end of the manifold block and including a substantially circular opening. The aperture control plate (304) is adapted to maintain the substantial circularity of the inlet aperture, so as to ensure a substantially fluid-tight seal.

2. 发明申请

WO2018083243A1 SPHERICAL COMPENSATOR JUNCTION ASSEMBLY FOR HIGH PRESSURE DUCTING SYSTEM 审中-公开
标题翻译：用于高压导管系统的球形补偿器接头组件
公开(公告)号：WO2018083243A1
公开(公告)日：2018-05-11
申请号：PCT/EP2017/078192
申请日：2017-11-03
申请人： SENIOR IP GMBH
发明人： OWDEH, Muhannad , POSSERT, Eric M.
IPC分类号： F16L25/01 , F16L27/06 , F16L39/04 , F16L41/02 , F16L41/03
摘要： A compensator junction assembly (20) for carrying pressurized hot gases in an aircraft ducting system comprises a substantially spherical inner race (21) having at least three apertures and at least three corresponding retainer assemblies (30), where the apertures in the retainer assemblies align with the apertures in the inner race, and at least three outer races (40), each having apertures generally aligned with the at least three inner race apertures, respectively. The retainer assemblies may include at least one bottom channel and at least one top channel for receiving one or more bearings (55) and seals (54). Spherically rotational movement of the retainer assemblies between the inner and outer races accommodates stresses caused by the pressurized hot gases and external forces.
摘要翻译：用于在飞机管道系统中运送加压热气体的补偿器接合组件（20）包括具有至少三个孔和至少三个对应的保持器组件（30）的基本上球形的内座圈（21），其中，其中保持器组件中的孔与内座圈中的孔对齐，以及至少三个外座圈（40），每个外座圈具有分别与至少三个内座圈孔对齐的孔。保持器组件可以包括至少一个底部通道和用于接收一个或多个轴承（55）和密封件（54）的至少一个顶部通道。内圈和外圈之间的保持器组件的球形旋转运动适应由加压热气体和外力引起的应力。

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