Device for mounting a turboreactor on an aeroplane
US4037809A · kind A · utility
Assignee
Inventor
Key dates
| Filing date | Nov 12, 1975 |
| Grant date | Jul 26, 1977 |
| Priority date | — |
| Expiry date | Nov 12, 1995 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D29/06
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A device for mounting in a nacelle on an airframe a turbojet engine contad by a casing, the device being of the type comprising a mast member integral with the airframe, a nacelle coaxial to the turbojet engine, quick release locking members connecting the compressor casing to the rear nacelle section, and elements for releasably connecting the rear nacelle section to the mast member wherein the device further comprises sliding guides permitting the nacelle to be displaced parallel to the longitudinal axis of the engine, along the mast member between an active and advanced position in which the rear nacelle section is supported against the casing of the compressor, and an inactive or remote position, in which the rear nacelle section is separate from the casing, and links directly connecting the casing of the engine to the mast with a view to ensuring support of the turbojet engine when the rear nacelle section is in the inactive or remote position.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.