Combustion liner

Details Combustion liner Combustion liner

1969-11-13

1983-07-12

Bentley, Stephen C.

Power plants

Combustion products used as motive fluid

Combustion products generator

F23R 300

Patent

active

043923550

ABSTRACT:
A combustion liner for a gas turbine engine operating at high temperatures has portions of the combustion liner double-walled, with a narrow clearance between the inner and outer walls through which cooling air flows to cool the liner. The surfaces of the walls which define these cooling air inlets are roughened to increase heat transfer from the air to the wall. The walls are joined and held apart by spacing strips extending axially of the liner and bonded to the overlapping wall sections. Large combustion air inlet holes extend through the overlapping wall sections at some points. Auxiliary air inlets for liner cooling are provided downstream of these combustion air inlet holes.

REFERENCES:
patent: 2617255 (1952-11-01), Niehus
patent: 3413704 (1968-12-01), Addoms, Jr. et al.

Affiliated with

Also associated with

Rating

Combustion liner does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-192569