About 30 results
https://drivepatents.com/patents/1016194 · 26 Jan 2011
A turbocharger with a variable nozzle includes a pin (220) mounted in the center housing (150) and extending axially therefrom and engaged in a hole in the nozzle ring (170) to orient the nozzle ring rotationally relative to the center housing. A portion o...
https://drivepatents.com/patents/1079092 · 23 Mar 2005
The jet engine has a sealing system for insulating a cavity from a vein of primary flow. The system has a joint (50) mounted at periphery of an upstream portion (12a) of an external case (12) of a diffuser grid. Blades of the joint (50) are in support on a...
https://drivepatents.com/patents/1079105 · 23 Mar 2005
The engine has a crankcase whose outer shell is fixed to an annular structure (7) by a joint with brush (50) fixed to a periphery of an upstream part of an outer case (12) of a diffuser grid (10). The joint has radially extending bristles (52) supported on...
https://drivepatents.com/patents/1079284 · 16 Mar 2005
The engine has a sealing unit including an annular segment (50) whose inner radial part (51) is housed in a radially sliding manner and seals a groove. The groove is provided at a periphery of an upstream port of an outer case of a diffuser grid (10). Peri...
https://drivepatents.com/patents/1085823 · 7 Jul 2004
A first stage rotor disk (50a) and a connecting member (30) on the compressor side are fixed by a spindle bolt (20). The spindle bolt (20) is covered with a tubular member (100), between the first stage rotor disk (50a) and the connecting member (30) on th...
https://drivepatents.com/patents/1086615 · 9 Jun 2004
The device has a shaft (18) with a rotor attached to each end, a bearing housing (4) for mounting the shaft and a turbine housing (2) with an opening opposite the bearing housing so that an end part (5) of the bearing housing can be attached to walls (33) ...
https://drivepatents.com/patents/1089456 · 25 Feb 2004
A sealing structure for sealing a gap between a combustor liner having an outer surface and a surrounding structure surrounding the combustor liner, includes: an annular sealing member held on the surrounding structure so as to be in contact with the outer...
https://drivepatents.com/patents/1090579 · 7 Jan 2004
An easy-fit heat screening device (110) for connecting a cooling pipe (112) and a through-hole (114) formed in a nozzle support ring (116) of a gas turbine, of the type comprising a tubular structure (118) which has an external diameter smaller than a diam...
https://drivepatents.com/patents/1093562 · 3 Sep 2003
A method for assembling an articulated fan front frame for a gas turbine engine facilitates improving engine performance. The method includes forming a strut (60) including a pair of sidewalls (80) connected at a leading edge (82) and a trailing edge (84),...
https://drivepatents.com/patents/1109427 · 10 Oct 2001
A gas turbine nozzle segment (10) has outer and inner bands (12, 14). Each band includes a side wall (40), a cover (20) and an impingement plate (26) between the cover and nozzle wall (18) defining two cavities on opposite sides of the impingement plate. C...