About 34 results
https://drivepatents.com/patents/978982 · 5 Feb 2014
This turbine exhaust structure and gas turbine are configured with a turbine cylinder (26) being provided that configures a combustion gas pathway (›) by forming a tubular shape, and an exhaust diffuser (31) that configures an exhaust gas pathway (B) by ...
https://drivepatents.com/patents/980313 · 1 Jan 2014
A gas turbine provided with an air bleeder tube (1) that, during startup, bleeds a portion of the compressed air of a compressor from the compressor and discharged the bled air into a cylindrical exhaust duct (20), wherein the air bleeder tube (1) is dispo...
https://drivepatents.com/patents/980171 · 1 Jan 2014
The invention relates to a diffuser (11) for the exhaust section of a gas turbine (10), comprising at least one cone (13, 14) extending along a machine axis and bordering a channel for an exhaust flow, whereby said at least one cone (13, 14) has a wall wit...
https://drivepatents.com/patents/983897 · 2 Oct 2013
A gas turbine engine recuperator system (30) includes a heat recuperator (32) positioned in a gas turbine exhaust gas duct (28) for recovering heat from turbine exhaust gases (48) to preheat a compressor flow being supplied to the combustor (26). A continu...
https://drivepatents.com/patents/984140 · 4 Sep 2013
The turbine (10) has an exhaust gas diffuser (21) connected to a turbine unit (24). An inflow-side annular diffuser channel (33) is limited by a conical channel wall (40). Inward extending hollow support ribs (35) are provided at the channel for fastening ...
https://drivepatents.com/patents/989993 · 12 Jun 2013
A pulse flow-channel-variable turbine device includes a turbine housing (1) in which a turbine impeller and an air outlet are arranged. An exhaust manifold (6) is connected to the inlet of the turbine housing (1). An internal flow channel is arranged insid...
https://drivepatents.com/patents/990466 · 22 May 2013
A retractable exhaust liner segment (18) between a gas turbine engine (20) and an exhaust liner (16).
https://drivepatents.com/patents/985556 · 20 Mar 2013
A turbine exhaust case (70) for a gas turbine engine (20) includes a multiple of ceramic matrix composite (CMC) turbine exhaust case struts (72) between a CMC core nacelle aft portion (76) and a CMC tail cone (74). A corresponding gas turbine engine (20) i...
https://drivepatents.com/patents/993752 · 23 Jan 2013
A gas turbine equipment utilizing high humidity, for preventing generation of white smoke throughout a year, and for restraining radiation of extra heat so as to restrain lowering of heat efficiency, the equipment comprising a humidifying device (6) for hu...
https://drivepatents.com/patents/999715 · 8 Aug 2012
A turbine engine comprises a case (42)and a centerbody (40) within the case (42) and separated from the case (42) by a core flowpath. A circumferential array of augmentor vanes (50) extends between the centerbody (40) and case (42). A circumferential array...