Compact gas turbine engine

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60 3936, 60739, 60760, F02C 732, F02C 305

Patent

active

050332635

ABSTRACT:
A gas turbine engine 10 having a rotor 12 with turbine blades 14 and a nozzle 16 adjacent the turbine blades 14 for directing hot gases of combustion at the turbine blades 14. The engine 10 also includes an annular combustor 18 about the rotor 12 and an annular combustor housing 30 substantially surrounding the combustor 18 in generally concentric spaced relation. A fuel injection system is operatively associated with the combustor 18 for injecting fuel into a combustion space 28 to be combusted with air from a compressor 34. The fuel injection system may include a plurality of circumferentially spaced fuel injectors 68 disposed in an outer wall 20 of the combustor 18 together with a generally oval shaped manifold 70 in fluid communication with a primary fuel source and the fuel injectors 68. A turbine shroud 36 is provided to extend radially outward from the rotor to the outer wall of the combustor on the side of the nozzle 16 opposite the combustion space 28. The turbine shroud 36 is cooled by a film of air which passes through a plurality of circumferentially spaced orifices 40 in the outer wall 20 of the combustor 18. The engine 10 also includes an abutment member 38, 60 and a spacing member 66 between the combustor 18 and the housing 30. With this arrangement, the combustor 18 and the housing 30 can be maintained in generally concentric preselected axial relation.

REFERENCES:
patent: 2916878 (1959-12-01), Wirt
patent: 3116908 (1964-01-01), Wosika
patent: 3266250 (1966-08-01), Freeman et al.
patent: 3287905 (1966-11-01), Bayard
patent: 3383855 (1968-05-01), Freeman et al.
patent: 3613360 (1971-10-01), Howes
patent: 3623318 (1971-11-01), Shank
patent: 3719042 (1973-03-01), Chamberlain
patent: 4151709 (1979-05-01), Melronian et al.
patent: 4825640 (1989-05-01), Shekleton

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Compact gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Compact gas turbine engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Compact gas turbine engine will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-424926

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.