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AIRCRAFT ENGINE ASSEMBLY STAND

发明专利审中
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20权利要求 · 3 独立
§ Ⅰ

卷宗概要

发明人

Pierre-Luc LACHANCE; Roch LAMARRE; Maxime PATRY; Vishi WIJESINGHE; Nathan VOLLO; Scott CAMERON; Cory BRISCOE; Annie ROTHER; Matthew DALLAS

IPC 分类

B64F 5/50F16M 1/4F16M 11/12

CPC 分类

B64F5/50F16M1/4F16M11/125F16M2200/24

An aircraft engine stand for supporting an aircraft engine, has: a support; a mount rotatably mounted to the support, the mount extending around a central axis from a first end to a second end, the mount surrounding an engine-receiving space having an opening between the first end and the second end, the opening sized for allowing the aircraft engine to be positioned into and removed from the engine-receiving space, the mount rotatable relative to the support about the central axis and about a transverse axis intersecting the central axis; and an adaptor extending radially inwardly into the engine-receiving space relative to the central axis from a mounting interface removably secured to the mount to an engine interface removably securable to the aircraft engine.

原文(中文)

An aircraft engine stand for supporting an aircraft engine, has: a support; a mount rotatably mounted to the support, the mount extending around a central axis from a first end to a second end, the mount surrounding an engine-receiving space having an opening between the first end and the second end, the opening sized for allowing the aircraft engine to be positioned into and removed from the engine-receiving space, the mount rotatable relative to the support about the central axis and about a transverse axis intersecting the central axis; and an adaptor extending radially inwardly into the engine-receiving space relative to the central axis from a mounting interface removably secured to the mount to an engine interface removably securable to the aircraft engine.