Gas turbine cooling system

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

415115, 415116, F01D 2512

Patent

active

040867579

ABSTRACT:
A cooling system for a gas turbine engine having a gasifier turbine and a power turbine each interconnected by a turbine casing utilizes compressed cooling air communicated to axial cavities in the ends of the respective turbine shafts. This compressed air is directed outwardly between a flange integrally formed with the turbine shaft and the turbine wheel for communication to the turbine blades. In the gasifier turbine the cooling air passes through longitudinal passages formed in each blade, while in the power turbine the cooling air is discharged adjacent the blade root. Wheel flanges affixed on either side of the turbine wheel serve to retain the blades axially on the wheel. Compressed cooling air is also communicated to the nozzle vanes of the gasifier turbine wherein internal passages communicate the air into the main gas stream. Certain nozzle vanes are equipped with passage means to communicate air to an annular chamber surrounding the gasifier turbine.

REFERENCES:
patent: 2598176 (1952-05-01), Johnstone
patent: 2962256 (1960-11-01), Bishop
patent: 3540810 (1970-11-01), Kercher
patent: 3575528 (1971-04-01), Beam et al.
patent: 3767322 (1973-10-01), Durgin et al.
patent: 3768924 (1973-10-01), Corsmeier et al.
patent: 3814539 (1974-06-01), Klompas
patent: 4017207 (1977-04-01), Bell et al.

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

Gas turbine cooling system does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-2152777

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