Engine mounting assembly
US5108045A · kind A · utility
Inventors
Key dates
| Filing date | Apr 25, 1990 |
| Grant date | Apr 28, 1992 |
| Priority date | — |
| Expiry date | Apr 25, 2010 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/404
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A vibration isolating mount for connecting spaced structures and limiting noise transmission between the connected structures, such as between an aircraft and a turbine engine. The isolator comprises a pair of arms which are interconnected at one location by a torque tube pivotally connected to the aircraft structure and which are interconnected at another location by a tie brace which is also connected to the aircraft structure by a vibration isolator pad. The engine is connected to the arms by a hanger. The mount accepts various engine leads and reactions while minimizing the transmission of engine noise into the cabin of the aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.