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公开(公告)号：US20170152052A1
公开(公告)日：2017-06-01
申请号：US15357106
申请日：2016-11-21
Applicant: Airbus Operations SAS
Inventor： David Ewens , Jonathan Blanc , Yves Belloc
CPC classification number: B64D27/26 , B64C3/32 , B64D27/18 , B64D2027/264 , B64D2027/266 , B64D2027/268
Abstract: An aircraft engine assembly including a set of rear engine attachments comprising a first shackle hinged on a bracket secured to the engine and on a bracket made as one piece with one of the two side panels, the shackle being oriented along a vertical direction, a second shackle hinged on a bracket secured to the engine and on a bracket made as one piece with the other one of the two side panels, the second shackle being oriented along the vertical direction, and a third shackle for transversally transmitting loads, inclined relative to the vertical direction and hinged on a bracket secured to the engine and on a bracket secured to the primary structure.
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2.发明申请AIRCRAFT PROPELLING ASSEMBLY INCLUDING A DUCT FORMING A THERMAL BARRIER INTEGRATED IN THE CAISSON OF THE RIGID STRUCTURE OF THE ENGINE MOUNTING SYSTEM 有权飞机螺旋桨组件，其中包括形成一个集成在发动机安装系统的刚性结构中的热障板公开(公告)号：US20150321765A1
公开(公告)日：2015-11-12
申请号：US14707240
申请日：2015-05-08
Applicant: Airbus Operations (SAS)
Inventor： Wolfgang Brochard , Misael Hernandez-Perez , Yves Belloc
CPC classification number: B64D27/26 , B64D2027/264 , B64D2027/266 , F28F3/02
Abstract: Housing a conduit of a thermal protection system of a rigid structure of an attachment pylon in an aircraft propulsion assembly within a box of the rigid structure, so as to take advantage of the volume within the rigid structure. The elements forming the conduits thus form an integral part of the rigid structure and can thus play a structural role.
Abstract translation: 在刚性结构的箱体内的飞机推进组件中安装附接塔的刚性结构的热保护系统的导管，以便利用刚性结构内的体积。 因此，形成导管的元件形成刚性结构的组成部分，因此可以发挥结构作用。
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公开(公告)号：US10189575B2
公开(公告)日：2019-01-29
申请号：US15357106
申请日：2016-11-21
Applicant: Airbus Operations SAS
Inventor： David Ewens , Jonathan Blanc , Yves Belloc
Abstract: An aircraft engine assembly including a set of rear engine attachments comprising a first shackle hinged on a bracket secured to the engine and on a bracket made as one piece with one of the two side panels, the shackle being oriented along a vertical direction, a second shackle hinged on a bracket secured to the engine and on a bracket made as one piece with the other one of the two side panels, the second shackle being oriented along the vertical direction, and a third shackle for transversally transmitting loads, inclined relative to the vertical direction and hinged on a bracket secured to the engine and on a bracket secured to the primary structure.
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公开(公告)号：US09975641B2
公开(公告)日：2018-05-22
申请号：US14707240
申请日：2015-05-08
Applicant: Airbus Operations (SAS)
Inventor： Wolfgang Brochard , Misael Hernandez-Perez , Yves Belloc
CPC classification number: B64D27/26 , B64D2027/264 , B64D2027/266 , F28F3/02
Abstract: Housing a conduit of a thermal protection system of a rigid structure of an attachment pylon in an aircraft propulsion assembly within a box of the rigid structure, so as to take advantage of the volume within the rigid structure. The elements forming the conduits thus form an integral part of the rigid structure and can thus play a structural role.
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