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Class Information
Number: 248/554
Name: Supports > Aircraft engine support
Description: Structure for supporting the propelling engine of an aircraft.


Sub-classes under this class:

Class Number Class Name Patents
248/557 Resilient 38
248/555 Three or more circumferentially spaced supports 32


Patents under this class:
1 2 3

Patent Number Title Of Patent Date Issued
7469689 Fluid cooled supercharger Dec. 30, 2008
7451947 Engine mounting structure under an aircraft wing Nov. 18, 2008
7448573 Engine suspension pylon for aircraft Nov. 11, 2008
7445179 Engine assembly for aircraft Nov. 4, 2008
7438262 Redundant gas turbine engine mounting arrangement Oct. 21, 2008
RE39972 Detachable integral aircraft tailcone and power assembly Jan. 1, 2008
7121512 Drain particularly for engine support strut Oct. 17, 2006
7100869 Turboprop carrier structure and an assembly including such a carrier structure Sep. 5, 2006
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
7021585 Aircraft engine rear mount with thrust links and boomerang-shaped lever Apr. 4, 2006
6986482 Suspension part of a turbojet engine Jan. 17, 2006
6976655 Mounting arrangement Dec. 20, 2005
6938855 Hooking strut of an engine under the wing unit of an aircraft Sep. 6, 2005
6935591 Mounting arrangement for a gas turbine engine Aug. 30, 2005
6843449 Fail-safe aircraft engine mounting system Jan. 18, 2005
6779755 Adjustable mount for a model airplane engine Aug. 24, 2004
6758438 Jet engine suspension Jul. 6, 2004
6708925 Mounting arrangement for a gas turbine engine Mar. 23, 2004
6669393 Connector assembly for gas turbine engines Dec. 30, 2003
6648271 Device for recovery of forces generated by an aircraft engine Nov. 18, 2003
6622963 System and method for controlling the movement of an aircraft engine cowl door Sep. 23, 2003
6607165 Aircraft engine mount with single thrust link Aug. 19, 2003
6608262 Aircraft load cell shoring Aug. 19, 2003
6547182 Solid rocket motor bolted thrust takeout structure Apr. 15, 2003
6494403 Device for aircraft thrust recovery capable of linking a turboshaft engine and an engine strut Dec. 17, 2002
6474597 Gas turbine engine mounting arrangement Nov. 5, 2002
6398161 Device for fixing an aircraft propulsion system to a strut and a strut adapted to said device Jun. 4, 2002
6330995 Aircraft engine mount Dec. 18, 2001
6330985 Link component for aircraft engine mounting systems Dec. 18, 2001
6328293 Multi-linkage suspension system including outboard isolators Dec. 11, 2001
6296203 Snubber thrust mount Oct. 2, 2001
6244539 Detachable integral aircraft tailcone and power assembly Jun. 12, 2001
6209822 Device for attaching an engine to an aircraft strut Apr. 3, 2001
6196795 Turbine pack and method for adapting a turbine pack Mar. 6, 2001
6189830 Tuned engine mounting system for jet aircraft Feb. 20, 2001
6173919 Attachment device for an aircraft engine Jan. 16, 2001
6126110 Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon Oct. 3, 2000
6123293 Engine mount, particularly for a propeller-driven aircraft, comprising a tubular frame structure Sep. 26, 2000
6095456 Strut-wing interface having dual upper links Aug. 1, 2000
6059227 Device for attaching an engine to an aircraft May. 9, 2000
6039287 Detachable integral aircraft tailcone and power assembly Mar. 21, 2000
6019313 Installation for mounting an engine on a deck and for connecting its output shaft to at least one driven mechanism Feb. 1, 2000
5927644 Double failsafe engine mount Jul. 27, 1999
5921500 Integrated failsafe engine mount Jul. 13, 1999
5873547 Aircraft engine thrust mount Feb. 23, 1999
5871177 Redundant front suspension system for a turboshaft engine Feb. 16, 1999
5871175 Redundant front suspension system for a turboshaft engine Feb. 16, 1999
5871176 Redundant front suspension system for a turboshaft engine Feb. 16, 1999
5860623 Three link failsafe engine mount Jan. 19, 1999
5810319 Adaptively tuned vibration absorber with dual flexures Sep. 22, 1998

1 2 3


 
 
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