首页> 外国专利> Thruster assembly comprising an engine attachment having at least one connecting pin equipped with a translation and aircraft locking system comprising at least one such propellant assembly

Thruster assembly comprising an engine attachment having at least one connecting pin equipped with a translation and aircraft locking system comprising at least one such propellant assembly

机译:推进器组件包括发动机连接,该发动机附接具有至少一个配备有一个连接销的连接销,包括至少一个这样的推进剂组件的平移和飞机锁定系统

摘要

Thruster assembly comprising an engine attachment having at least one connecting pin equipped with a translation and aircraft locking system comprising at least one such propellant assembly The subject of the invention is a propulsion assembly for an aircraft comprising a connecting pin ( 76) of an engine attachment connecting first and second parts and comprising: a first hollow tube (88), housed in bores (86) provided in the first and second parts in operation and comprising at least one groove (90.1) near at least one of its first and second ends (88.1, 88.2), at least one locking plate (100.1, 100.2) comprising at least one locking hole (102) having a first part (104.1), delimited by a first edge (B104.1) configured to fit in the groove (90.1), and a second part (104.2), delimited by a second edge (B104.2) and configured to allow the introduction of the first hollow tube (88 ) in the blocking hole (1 02), the locking plate (100.1, 100.2) being movable between a first position in which the first edge (B104.1) of the first part (104.1) is accommodated, at least partially, in the groove (90.1) and a second position in which no edge of the locking hole (102) is positioned in the groove (90.1) of the first hollow tube (88), a locking system (106) making it possible to immobilize the locking plate (100.1) , 100.2) in the first position. Figure 7
机译:推进器组件包括具有至少一个配备有一个连接销的发动机附件,该连接销包括至少一个这样的推进剂组件,本发明的主题是用于包括发动机附件的连接销(76)的飞行器的推进组件连接第一和第二部分,包括:第一中空管(88),其容纳在设置在第一和第二部分中的孔(86)中,并且包括至少一个凹槽(90.1)靠近其第一和第二端中的至少一个凹槽(90.1) (88.1,88.2),至少一个锁定板(100.1,100.2),其包括至少一个具有第一部分(104.1)的锁定孔(102),所述第一部分(104.1)由构造成适合所述凹槽的第一边缘(B104.1)限定( 90.1)和第二部分(104.2),由第二边缘(B104.2)界定并配置成允许在阻挡孔(1 02)中引入第一中空管(88),锁定板(100.1, 100.2)在WH中的第一位置之间移动第一部分(104.1)的第一边缘(B104.1)至少部分地容纳在凹槽(90.1)和第二位置,其中锁定孔(102)的边缘定位在凹槽中( 90.1)第一中空管(88),锁定系统(106),使得可以将锁定板(100.1),100.2)固定在第一位置。图7.

著录项

  • 公开/公告号FR3101615B1

    专利类型

  • 公开/公告日2021-10-15

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS (S.A.S.);

    申请/专利号FR1910930

  • 发明设计人 MERTES ANTHONY;

    申请日2019-10-02

  • 分类号B64D27/26;F02C7/20;

  • 国家 FR

  • 入库时间 2022-08-24 21:43:53

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