Patent · US Active

In-line removable heat shield for a turbomachine suspension yoke

US9359954B2 · kind B2 · utility

1Cited by

3References

14Claims

0Family size

Assignee

SNECMA · FR

Inventors

Lambert Olivier Marie Demoulin · Paris, FR
Julien Pavillet · Moissy-Cramayel, FR
Guilhem Seize · Corbeil-Essonnes, FR

Key dates

Filing date	Oct 15, 2013
Grant date	Jun 7, 2016
Priority date	—
Expiry date	Sep 13, 2034

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF02C7/24
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

A heat shield device for a yoke suspending an engine from an aircraft is provided. The device includes panels able to be fixed to the yoke, at least one of the panels extending radially in the direction of the axis of the engine, and a component configured to be fixed to the engine and including a groove shaped in such a way that the lower end of the panel can be inserted into it.

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