About 20 results
https://drivepatents.com/patents/1010336 · 10 Aug 2011
The housing has an outer ring (3), inner ring (1) and an intermediate ring (2), which are supported against each other via an inner strut (4. 1) and outer strut (5.1). An auxiliary device gear box (7) is connected with a radial shaft (6). Other outer strut...
https://drivepatents.com/patents/1011654 · 22 Jun 2011
The turbocharger has a bearing housing (28) connected with a compressor housing (3) at an end by using a fastening device (19). A turbine housing is connected with the bearing housing by using another fastening device, where the compressor, bearing and tur...
https://drivepatents.com/patents/1015265 · 2 Mar 2011
An exemplary center housing rotating assembly includes a turbine wheel; a compressor wheel; a center housing (510) that includes a through bore (515), extending from a compressor end to a turbine end along a bore axis; a bearing assembly (530) positioned i...
https://drivepatents.com/patents/1066459 · 14 Jun 2006
A method of reducing gas turbine engine distortion includes coupling a core gas turbine engine (10) to a power turbine, coupling the power turbine to a thrust bearing support assembly through a frusto-conically shaped structural support (100) such that the...
https://drivepatents.com/patents/1067594 · 10 May 2006
A method for assembling a gas turbine engine (10) that includes providing a low-pressure turbine inner rotor (120) that includes a first plurality of turbine blade rows (124) configured to rotate in a first direction, providing a low-pressure turbine outer...
https://drivepatents.com/patents/1068774 · 29 Mar 2006
The turbofan has a monoblock arm (28) comprising support connectors (29) disposed parallel to a radial arm. Each connector connects a support situated outside an outer casing (2) with another support situated within a shell (4). The arm (28) has a distribu...
https://drivepatents.com/patents/1069584 · 1 Mar 2006
Disclosed is a structural frame (38) for a gas turbine (10) engine comprising an integral fluid reservoir (60) and air/fluid heat exchanger (68;168;268). A central hub (56) includes a reservoir (60) for storing a fluid and an outer rim (62) circumscribes t...
https://drivepatents.com/patents/1074980 · 17 Aug 2005
The turbofan has two counter-rotating fans (3, 5), and a low pressure compressor (7). The compressor has a downstream crown (18) of rotating blades (19) connecting the fan (5) to a drive shaft (6) of the fan (5). An upstream crown (40) of rotating blades (...
https://drivepatents.com/patents/1084765 · 18 Aug 2004
A bearing support for a rotor (12) of an aircraft turbine engine (10) includes a front bearing and a front bearing support (118) and bearing strut (120) for securely attaching the front bearing to the aircraft turbine engine support structure (122). The fr...
https://drivepatents.com/patents/1089896 · 4 Feb 2004
An aircraft gas turbine engine includes a low pressure turbine (26) having a low pressure turbine flowpath and counter rotatable low pressure inner and outer shaft rotors (200, 202) having inner and outer shafts (130, 140), respectively. The low pressure i...