Method of protecting gas turbine combustor components against wa

Power plants – Combustion products used as motive fluid

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60 3955, 60753, F02G 300

Patent

active

060475390

ABSTRACT:
A method of preventing water erosion and hot corrosion in a combustor of a gas turbine engine, wherein water is injected into said combustor for NOx abatement, which involves the step of applying a dense vertically cracked thermal barrier coating to certain components thereof The dense vertically cracked thermal barrier coating has a porosity of less than approximately 8% and a tensile strength in the range of approximately 4-7 ksi. The dense vertically cracked thermal barrier coating is applied to such combustor components so as to produce a segmented ceramic structure having macrocracks formed therein which are oriented substantially perpendicular to an interface of the combustor component and the segmented ceramic structure.

REFERENCES:
patent: 2476185 (1949-07-01), Goddard
patent: 4382771 (1983-05-01), Carr
patent: 4397356 (1983-08-01), Retallick
patent: 4455839 (1984-06-01), Wuchter
patent: 4567730 (1986-02-01), Scott
patent: 4655044 (1987-04-01), Dierberger et al.
patent: 5009070 (1991-04-01), Iizuka et al.
patent: 5073433 (1991-12-01), Taylor
patent: 5113660 (1992-05-01), Able et al.
patent: 5220786 (1993-06-01), Campbell
patent: 5528904 (1996-06-01), Jones et al.
patent: 5553455 (1996-09-01), Craig 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

Method of protecting gas turbine combustor components against wa does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of protecting gas turbine combustor components against wa, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of protecting gas turbine combustor components against wa will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1168335

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