US2014013754A1PendingUtilityA1
Power augmentation system with dynamics damping
Assignee: SLOBODYANSKIY ILYA ALEKSANDROVICHPriority: Mar 31, 2011Filed: Mar 31, 2011Published: Jan 16, 2014
Est. expiryMar 31, 2031(~4.7 yrs left)· nominal 20-yr term from priority
Inventors:Ilya Aleksandrovich SlobodyanskiySergey Maskhutovich KhayrulinDmitry Vladlenovich TretyakovSteven Gumpangkum
F05D 2260/96F23R 3/00F23R 2900/00013Y02E20/16F02C 3/305F02C 5/11F23L 7/005F01D 9/023F23M 20/005F23R 3/40
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Claims
Abstract
A power augmentation system for a gas turbine engine which may include a transition piece of a combustor and a steam manifold positioned about the transition piece. The transition piece may include a number of transition piece passageways therethrough and the steam manifold may include a number of manifold passageways therethrough. The manifold passageways align with the transition piece passageways.
Claims
exact text as granted — not AI-modifiedWe claim:
1 . A power augmentation system with dynamics damping for a gas turbine engine, comprising:
a transition piece of a combustor; a steam manifold positioned about the transition piece; the transition piece comprising a plurality of transition piece passageways therethrough; and the steam manifold comprising a plurality of manifold passageways therethrough; the plurality of manifold passageways aligning with the plurality of transition piece passageways.
2 . The power augmentation system of claim 1 , wherein the plurality of transition piece passageways comprises a plurality of apertures therethrough.
3 . The power augmentation system of claim 2 , wherein the plurality of apertures comprises a plurality of angled apertures.
4 . The power augmentation system of claim 1 , wherein the steam manifold comprises a cavity therein.
5 . The power augmentation system of claim 1 , wherein the plurality of manifold passageways comprises a plurality of tubes.
6 . The power augmentation system of claim 5 , wherein the plurality of tubes comprises a plurality of angled tubes.
7 . The power augmentation system of claim 1 , wherein the steam manifold comprises a plurality of purge holes.
8 . The power augmentation system of claim 1 , wherein the transition piece comprises a frame and wherein the steam manifold comprises a steam passage positioned on the frame.
9 . The power augmentation system of claim 1 , wherein the plurality of manifold passageways comprises a predetermined size based upon the frequency of the combustor.
10 . A power augmentation system with dynamics damping for a gas turbine engine, comprising:
a transition piece of a combustor; a steam manifold positioned about the transition piece; the transition piece comprising a plurality of apertures extending therethrough; the steam manifold comprising a plurality of tubes extending therethrough; the plurality of tubes comprising a predetermined size based upon the frequency of the combustor; and the plurality of apertures aligning with the plurality of tubes.
11 . The power augmentation system of claim 10 , wherein the plurality of apertures comprises a plurality of angled apertures.
12 . The power augmentation system of claim 10 , wherein the steam manifold comprises a cavity therein.
13 . The power augmentation system of claim 10 , wherein the plurality of tubes comprises a plurality of angled tubes.
14 . The power augmentation system of claim 10 , wherein the steam manifold comprises a plurality of purge holes.
15 . The power augmentation system of claim 10 , wherein the transition piece comprises a frame and wherein the steam manifold comprises a steam passage positioned on the frame.
16 . A power augmentation system with dynamics damping for a gas turbine engine, comprising:
a combustor; a steam manifold positioned about the combustor; the combustor comprising a plurality of apertures extending therethrough; the steam manifold comprising a plurality of tubes extending therethrough; and the plurality of tubes comprising a predetermined size based upon the frequency of the combustor.
17 . The power augmentation system of claim 16 , wherein the combustor comprises a transition piece and wherein the steam manifold is positioned about the transition piece.
18 . The power augmentation system of claim 16 , wherein the plurality of apertures align with the plurality of tubes.
19 . The power augmentation system of claim 16 , wherein the plurality of apertures comprises a plurality of angled apertures.
20 . The power augmentation system of claim 16 , wherein the plurality of tubes comprises a plurality of angled tubes.Join the waitlist — get patent alerts
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