Aircraft gas turbine engine sideways mount
US5443229A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Dec 13, 1993 |
| Grant date | Aug 22, 1995 |
| Priority date | — |
| Expiry date | Dec 13, 2013 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft engine sideways mount assembly includes a thrust mount and an engine suspension for suspending the engine structure sideways from the aircraft such that the thrust mount is operable to react substantially all the thrust load forces from the engine to the aircraft. The thrust mount has a thrust bar extending between the engine structure and a structure fixed to the aircraft such that the thrust bar has a line of action which intersects the engine centerline in a support mount plane through which the engine suspension suspends the engine and which is generally perpendicular the engine centerline. The thrust bar has two thrust links pivotably joined to the aircraft at their aft ends and pivotably joined to the engine structure between the pivotal support mounts at their forward ends and include lines of force which intersect the engine centerline at the forward mount plane through which the forward pivotal support mount acts to support the engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.