Patent · US Active

Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine

US8083176B2 · kind B2 · utility

4Cited by
12References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 22, 2006
Grant dateDec 27, 2011
Priority date
Expiry dateMar 27, 2029

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D27/402
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A method to mount an aircraft engine on a rigid structure of an engine mount, includes securing, on the structure, an attachment body for an engine attachment, the attachment body configured to lie against a contact surface of the rigid structure oriented forwardly, and secured to the structure by at least one shear pin passing through a first and a second primary orifice. The securing of the body includes: pre-positioning the engine relative to the engine mount to place the first orifice opposite the second orifice, and inserting a pin fitted with a convex centering head through the two orifices, so that the pin forms the shear pin.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.