About 28 results
https://drivepatents.com/patents/1004847 · 29 Feb 2012
Systems and methods provide for reducing motion which causes wear in a combustor. The method includes attaching a first end of a combustor liner (404) to a retainer (402) which encircles the first end of the combustor liner (404); attaching the retainer (4...
https://drivepatents.com/patents/1016163 · 26 Jan 2011
An electrical cable shroud forming an annular structure having an outer surface and an inner surface, the cable shroud comprising a substantially J-shaped cross-section having a longest side, a shorter leg, and a rounded portion therebetween. The longest s...
https://drivepatents.com/patents/1079096 · 23 Mar 2005
A low emission turbine includes a reverse flow can-type combustor (102) that generally includes a primary and secondary fuel delivery system that can be independently controlled to produce low CO, UHC, and NOx emissions at design set point and at condition...
https://drivepatents.com/patents/1081217 · 29 Dec 2004
The device has a clamp standardized according to a harness (3) and maintaining the harness in direction perpendicular to axis (4) of a jet engine (1). Another standardized clamp is maintains the harness in direction parallel to axis of the jet engine. The ...
https://drivepatents.com/patents/1095903 · 21 May 2003
A high temperature bushing 10 includes an inner core 12 made of a monolithic ceramic material having a through-hole 14 formed therein of predetermined diameter; and an outer housing 24 substantially encasing the inner core 12, the outer housing 24 made of ...
https://drivepatents.com/patents/1102980 · 24 Jul 2002
The invention relates to a device for centering a tube (3) or a component inside a hollow shaft (2) of a turbine in a turbomachine, this tube (3) or component being rotationally secured to said shaft (2) at its ends, this device comprising a sleeve (9) sec...
https://drivepatents.com/patents/1111841 · 4 Jul 2001
A ducting system for use on a gas turbine engine having two fans (102, 104) connected to a common shaft, and includes a primary inlet duct (12) that is integral with a plurality of primary discharge ducts (14, 16, 18, 20), a plurality of secondary inlet du...
https://drivepatents.com/patents/1111835 · 4 Jul 2001
A fuel manifold assembly (40) for a gas turbine engine (10) includes a spray shield (70) that directs fuel that may leak from fuel line connections away from engine components. The spray shield attaches around the fuel line connections and includes a first...