公开(公告)号：US20160311555A1

公开(公告)日：2016-10-27

申请号：US15103277

申请日：2013-12-16

Applicant: MICROTURBO

Inventor： Olivier CAZENAVE ,  Clement LALANNE ,  Xavier BARNETO

IPC: B64D41/00 ,  B64D33/08 ,  B64D33/04

CPC classification number: B64D41/00 ,  B64D33/04 ,  B64D33/08 ,  B64D2041/002 ,  Y02T50/44

Abstract: The invention relates to an assembly comprising a structure (2) and a tubular element (6), which is mounted isostatically in the structure (2), said tubular element (6) comprising a first end (7) connected to said structure by at least four connecting rods 10a-10b-10c-10d, thus setting four first degrees of freedom, and a second end (8) connected to said structure (2) by an attachment means (20) that sets two second degrees of freedom, said connecting rods comprising a means for adjusting the length thereof. In particular, it relates to an exhaust suitable for an auxiliary power unit in the compartment thereof and to the mounting method for aligning them.

Abstract translation: 本发明涉及一种包括结构（2）和管状元件（6）的组件，其均匀地安装在结构（2）中，所述管状元件（6）包括第一端（7），第一端（7）通过在 至少四个连接杆10a-10b-10c-10d，从而设定四个第一自由度;以及第二端（8），通过固定两个第二自由度的连接装置（20）连接到所述结构（2） 连杆，包括用于调节其长度的装置。 特别地，涉及适用于其隔室中的辅助动力单元的排气装置及其对准的安装方法。

公开(公告)号：US20160297539A1

公开(公告)日：2016-10-13

申请号：US15100607

申请日：2014-12-04

Applicant: Microturbo

Inventor： Olivier CAZENAVE ,  Clement LALANNE ,  Luc DIONNE

IPC: B64D41/00 ,  G09B25/02 ,  G09B19/00 ,  B64F5/00 ,  F16M13/02

CPC classification number: B64D41/00 ,  B64D2041/002 ,  B64F5/00 ,  F16M13/02 ,  G09B19/0069 ,  G09B25/02 ,  Y02T50/44

Abstract: The invention relates to a method for mounting an engine module (1) in a support comprising a first structure (3) and a second structure (2) that is offset relative to the first structure (3), method intended for positioning at least a specified part (4) of the engine module (1) relative to an element (6) of the second structure (2) by means of an isostatic suspension connecting the engine module (1) to said first structure (3) by means of first connecting rods (10a, 10b, 10c, 10d) and to said second structure (2) by means of second connecting rods (10e, 10f), the length of said first and second connecting rods being defined in advance, method wherein the length of at least two (10c, 10f) of said first and second connecting rods is adjusted relative to the previously defined length thereof, in order to position said specified part (4) of the engine module (1) relative to said element (6) of the second structure (2) in said support. The invention also relates to said support comprising adjustable connecting rods, in an installation comprising in particular an auxiliary power unit for an aircraft.

Abstract translation: 本发明涉及一种用于将发动机模块（1）安装在包括相对于第一结构（3）偏移的第一结构（3）和第二结构（2））的支撑件中的方法，其用于将至少一个 发动机模块（1）的相对于第二结构（2）的元件（6）的指定部分（4）借助于通过第一结构将发动机模块（1）连接到所述第一结构（3）的等静压悬架 连接杆（10a，10b，10c，10d）和借助于第二连接杆（10e，10f）连接到所述第二结构（2），所述第一和第二连杆的长度预先限定，其中， 至少两个（10c，10f）的所述第一和第二连杆相对于其先前限定的长度被调节，以便相对于所述元件（6）将所述发动机模块（1）的所述指定部分（4）相对于所述元件 所述支撑件中的第二结构（2）。 本发明还涉及包括可调连接杆的所述支撑件，该装置尤其包括用于飞行器的辅助动力单元。