Inventor
UDALL KENNETH F
GB37 patents
⚠️ This page may combine multiple inventors who share the name “UDALL KENNETH F”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
ROLLS ROYCE PLC
26 patentsUS7806363B2Oct 5, 2010
Engine mounting assembly
ROLLS ROYCE PLC56 citations98
US6935591B2Aug 30, 2005
Mounting arrangement for a gas turbine engine
ROLLS ROYCE PLC77 citations98
US6575694B1Jun 10, 2003
Gas turbine engine blade containment assembly
ROLLS ROYCE PLC111 citations97
US6109022AAug 29, 2000
Turbofan with frangible rotor support
ROLLS ROYCE PLC110 citations97
US6073439AJun 13, 2000
Ducted fan gas turbine engine
ROLLS ROYCE PLC90 citations97
US6708925B2Mar 23, 2004
Mounting arrangement for a gas turbine engine
ROLLS ROYCE PLC70 citations96
US5746391AMay 5, 1998
Mounting for coupling a turbofan gas turbine engine to an aircraft structure
ROLLS ROYCE PLC256 citations96
US6009701AJan 4, 2000
Ducted fan gas turbine engine having a frangible connection
ROLLS ROYCE PLC73 citations95
US5409184AApr 25, 1995
Mounting for coupling a turbofan gas turbine engine to an aircraft structure
ROLLS ROYCE PLC94 citations93
US7845158B2Dec 7, 2010
Turbine engine mounting arrangement
ROLLS ROYCE PLC22 citations92
US7654075B2Feb 2, 2010
Fan static structure
ROLLS ROYCE PLC29 citations92
US7086219B2Aug 8, 2006
Cowl structure for a gas turbine engine
ROLLS ROYCE PLC24 citations92
US6892526B2May 17, 2005
Cowl structure for a gas turbine engine
ROLLS ROYCE PLC26 citations92
US6098399AAug 8, 2000
Ducted fan gas turbine engine
ROLLS ROYCE PLC42 citations92
US6494032B2Dec 17, 2002
Ducted fan gas turbine engine with frangible connection
ROLLS ROYCE PLC41 citations90
US6827548B2Dec 7, 2004
Rotor assemblies for gas turbine engines
ROLLS ROYCE PLC22 citations88
US8371802B2Feb 12, 2013
Shaft stabiliser
ROLLS ROYCE PLC8 citations84
US7891167B2Feb 22, 2011
Gas turbine engine flow reverser
ROLLS ROYCE PLC7 citations84
US7143975B2Dec 5, 2006
Landing arrangement for an aircraft
ROLLS ROYCE PLC19 citations84
US7527476B2May 5, 2009
Rotor assembly and annulus filler for gas turbine engine compressor
ROLLS ROYCE PLC11 citations83
US7229252B2Jun 12, 2007
Rotor assembly retaining apparatus
ROLLS ROYCE PLC12 citations77
US5370501ADec 6, 1994
Fan for a ducted fan gas turbine engine
ROLLS ROYCE PLC13 citations74
US7806364B1Oct 5, 2010
Containment system for a gas turbine engine
ROLLS ROYCE PLC6 citations63
US6971855B2Dec 6, 2005
Blade arrangement for gas turbine engine
ROLLS ROYCE PLC5 citations62
US7523604B2Apr 28, 2009
Thrust reverser mounting structure
ROLLS ROYCE PLC1 citations52
US9845682B2Dec 19, 2017
Fan disc
ROLLS ROYCE PLC0 citations41
UDALL KENNETH F
6 patentsUS8123489B2Feb 28, 2012
Hollow aerofoil and a method of manufacturing a hollow aerofoil
UDALL KENNETH F28 citations89
US8100638B2Jan 24, 2012
Centering device
UDALL KENNETH F11 citations83
US9109733B2Aug 18, 2015
Hydraulic fluid transfer coupling
UDALL KENNETH F3 citations62
US8303187B2Nov 6, 2012
Bearing arrangement
UDALL KENNETH F4 citations62
US8444084B2May 21, 2013
Aeroengine mounting
UDALL KENNETH F4 citations61
US8985946B2Mar 24, 2015
Mounting system
UDALL KENNETH F2 citations56