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Class Information
Number: 248/556
Name: Supports > Aircraft engine support > Three or more circumferentially spaced supports > Resilient
Description: Structure wherein at least one of the mountings is resilient.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7461815 |
Suspension system for a rotary wing aircraft engine |
Dec. 9, 2008 |
| 7174244 |
Suspension of a vehicle and method for controlling the same |
Feb. 6, 2007 |
| 7063290 |
Mounting system inserted between an aircraft engine and a rigid structure of an attachment strut fixed under a wing of this aircraft |
Jun. 20, 2006 |
| 6938855 |
Hooking strut of an engine under the wing unit of an aircraft |
Sep. 6, 2005 |
| 6113030 |
Readily changeable isolator and method of assembly thereof |
Sep. 5, 2000 |
| 5918833 |
Hydraulic torque restraint system |
Jul. 6, 1999 |
| 5820079 |
Mechanism for mounting and actuating a momentum wheel with high vibration isolation |
Oct. 13, 1998 |
| 5775638 |
Mounting arrangement for a gas turbine engine |
Jul. 7, 1998 |
| 5746391 |
Mounting for coupling a turbofan gas turbine engine to an aircraft structure |
May. 5, 1998 |
| 5065959 |
Vibration damping aircraft engine attachment |
Nov. 19, 1991 |
| 4441313 |
Mounting devices for multiple flow turbojet engines |
Apr. 10, 1984 |
| 4362281 |
Pylon mounting system for reducing helicopter vibration |
Dec. 7, 1982 |
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