Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans
Abstract
A can-annular gas turbine engine combustion arrangement (10), including: a combustor can (12) comprising a combustor inlet (38) and a combustor outlet circumferentially and axially offset from the combustor inlet; an outer casing (24) defining a plenum (22) in which the combustor can is disposed; and baffles (70) configured to divide the plenum into radial sectors (72) and configured to inhibit circumferential motion of compressed air (16) within the plenum.
- Inventors:
- Issue Date:
- Research Org.:
- Siemens Energy, Inc., Orlando, FL (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1214598
- Patent Number(s):
- 9134029
- Application Number:
- 14/024,892
- Assignee:
- Siemens Energy, Inc. (Orlando, FL)
- Patent Classifications (CPCs):
-
F - MECHANICAL ENGINEERING F02 - COMBUSTION ENGINES F02C - GAS-TURBINE PLANTS
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- DOE Contract Number:
- FC26-05NT42644
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2013 Sep 12
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 33 ADVANCED PROPULSION SYSTEMS
Citation Formats
Rodriguez, Jose L. Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans. United States: N. p., 2015.
Web.
Rodriguez, Jose L. Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans. United States.
Rodriguez, Jose L. Tue .
"Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans". United States. https://www.osti.gov/servlets/purl/1214598.
@article{osti_1214598,
title = {Radial midframe baffle for can-annular combustor arrangement having tangentially oriented combustor cans},
author = {Rodriguez, Jose L.},
abstractNote = {A can-annular gas turbine engine combustion arrangement (10), including: a combustor can (12) comprising a combustor inlet (38) and a combustor outlet circumferentially and axially offset from the combustor inlet; an outer casing (24) defining a plenum (22) in which the combustor can is disposed; and baffles (70) configured to divide the plenum into radial sectors (72) and configured to inhibit circumferential motion of compressed air (16) within the plenum.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {9}
}