Engine mount, particularly for a propeller-driven aircraft, comprising a tubular frame structure
US6123293A · kind A · utility
Assignees
Inventors
Key dates
| Filing date | Apr 1, 1998 |
| Grant date | Sep 26, 2000 |
| Priority date | — |
| Expiry date | Apr 1, 2018 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/40
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An engine mount (1) is disclosed which is particularly suitable for a propeller-driven aircraft. The engine mount (1) comprises a tubular frame structure (3) for the attachment of an engine (4) to a supporting structure, particularly to a cowling box (2). The frame structure (3) comprises a multitude of point-shape connected and braced members (8), (11), (12), (13), (15), and is part surrounding the engine (4). The engine (4) is bolted to mounts at one end of the tubular frame structure (3) in the direction (5) of drive, and, at its other end in the direction (5) of drive, the tubular frame structure (3) is, in turn, bolted to mounts on the supporting structure. According to the invention at least one member of the tubular frame structure (3) is an active member (12) the length of which can be changed under control.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.