Aircraft engine mount

The invention relates to an aircraft engine mount which comprises first and second parts (54, 56) connected by connecting elements (58) and wherein one of the two connected parts comprises at least one transverse hole (56) opening onto an access face (74) of the part (56) and into which there open a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	JOURNADE FREDERIC, BOUCHET ERIC, GROSSEAU NICOLAS, MUTIN ANTOINE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention relates to an aircraft engine mount which comprises first and second parts (54, 56) connected by connecting elements (58) and wherein one of the two connected parts comprises at least one transverse hole (56) opening onto an access face (74) of the part (56) and into which there open at least two passage holes (72) each intended to house a threaded shank (66) of one of the connectingelements (58). The engine mount comprises a transverse nut which comprises at least two bodies (80.1, 80.2) joined together each having a tapped hole configured to engage with one of the threaded shanks (66). 本发明涉及种飞行器发动机组件，该飞行器发动机组件包括通过连接元件(58)连接的第和第二部分(54，56)并且其特征在于这两个连接的部分之包括通到所述部分(56)的触及面(74)上的至少个横向孔洞(76)并且至少两个通孔(72)通入该至少个横向孔洞，每个通孔旨在容纳这些连接元件(58)之的螺纹柄部(66)，并且特征在于该发动机安装节包括横向螺母，该横向螺母包括连结在起的至少两个本体(80.1，80.2)，每个本体具有被构型成用于与螺纹柄部(66)之相接合的攻丝孔洞。