Mount assembly for porous transition panel at annular combustor

Details Mount assembly for porous transition panel at annular combustor Mount assembly for porous transition panel at annular combustor

1977-12-21

1980-03-04

Croyle, Carlton R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60754, 431352, F02C 712, F02C 720

Patent

active

041910117

ABSTRACT:
A gas turbine engine combustor assembly of annular configuration has outer and inner walls made up of a plurality of axially extending multi-layered porous metal panels joined together at butt joints therebetween and each outer and inner wall including a transition panel of porous metal defining a combustor assembly outlet supported by a combustor mount assembly including a stiffener ring having a side undercut thereon fit over a transition panel end face; and wherein an annular weld joins the ring to the end face to transmit exhaust heat from the end face to the stiffener ring for dissipation from the combustor; a combustor pilot member is located in axially spaced, surrounding relationship to the end face and connector means support the stiffener ring in free floating relationship with the pilot member to compensate for both radial and axial thermal expansion of the transition panel; and said connector means includes a radial gap for maintaining a controlled flow of coolant from outside of the transition panel into cooling relationship with the stiffener ring and said weld to further cool the end face against excessive heat build-up therein during flow of hot gas exhaust through said outlet.

REFERENCES:
patent: 2702454 (1955-02-01), Brown
patent: 2709338 (1955-05-01), Morley et al.
patent: 2846847 (1958-08-01), Simmons
patent: 2915280 (1959-12-01), Sonder
patent: 3349558 (1967-10-01), Smith
patent: 3670497 (1972-06-01), Sheldon
patent: 3965066 (1976-06-01), Sterman et al.
patent: 4016718 (1977-04-01), Lauck

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