About 18 results
https://drivepatents.com/patents/966958 · 26 Nov 2014
The invention relates to a regenerative gas turbine combustor being provided to enable to reduce an amount of leakage of compressed air before preheating to compressed air after the preheating. The regenerative gas turbine combustor is such that a compress...
https://drivepatents.com/patents/968200 · 29 Oct 2014
A gas turbine engine having high reliability is provided by suppressing occurrence of thermal stress between a scroll and a support member thereof. A gas turbine engine equipped with a combustor of a single-can type includes a scroll to guide a combustion ...
https://drivepatents.com/patents/969484 · 1 Oct 2014
A combustor equipped with a combustion cylinder and an acoustic liner that is provided on the outside of the combustion cylinder, with a space formed between the outer circumferential surface of the combustion cylinder and the liner. A group of through-hol...
https://drivepatents.com/patents/974008 · 4 Jun 2014
A gas turbine engine system (10) includes a compressor (14), a combustor (16), and a turbine (22). The combustor is coupled to the compressor and disposed downstream of the compressor. The combustor includes a secondary combustor section (20) coupled to a ...
https://drivepatents.com/patents/974935 · 14 May 2014
A hot gas path assembly (30) includes an outer support ring (36), an inner support ring (40), and a transition duct (32) coupled to the outer support ring (36) and the inner support ring (40). The transition duct (32) includes a conduit (50) defining a pas...
https://drivepatents.com/patents/988867 · 10 Jul 2013
A late lean injection system transition piece (12) includes a flowsleeve interface (38) extending circumferentially around a transition interior (18). Also included is an impingement sleeve mounting surface (52) extending circumferentially around the trans...
https://drivepatents.com/patents/988864 · 10 Jul 2013
A combustor in a gas turbine engine has a wall 18 which forms a gap 20 with an outer nozzle guide vane platform 14. A closure mechanism 30, 32 is operable to open or close the gap 20. Opening of the gap 20, for example during cruise conditions, reduces the...
https://drivepatents.com/patents/985999 · 20 Feb 2013
A seal end attachment (11) is provided and includes a vessel (20) through which a working fluid flows, the vessel (20) being formed to define a recess (21) with a mating surface (22) therein, a seal (40) contacting the mating surface (22) and a pressing me...
https://drivepatents.com/patents/994051 · 9 Jan 2013
A support assembly (100) for a turbine system (10) is disclosed. The support assembly (100) includes a transition duct (50) extending between a fuel nozzle and a turbine section. The transition duct has an inlet (52), an outlet (54), and a passage (56) ext...
https://drivepatents.com/patents/994045 · 9 Jan 2013
A support assembly (100) for a turbine system (10) is disclosed. The support assembly (100) includes a transition duct (50) extending between a fuel nozzle and a turbine section. The transition duct (50) has an inlet (52), an outlet (54), and a passage (56...