High-Temperature-Turbine Technology Program: Phase II. Technology test and support studies. Design and development of the liquid-fueled high-temperature combustor for the Turbine Spool Technology Rig
The concept selected by Curtiss-Wright for this DOE sponsored High Temperature Turbine Technology (HTTT) Program utilizes transpiration air-cooling of the turbine subsystem airfoils. With moderate quantities of cooling air, this method of cooling has been demonstrated to be effective in a 2600 to 3000/sup 0/F gas stream. Test results show that transpiration air-cooling also protects turbine components from the aggressive environment produced by the combustion of coal-derived fuels. A new single-stage, high work transpiration air-cooled turbine has been designed and fabricated for evaluation in a rotating test vehicle designated the Turbine Spool Technology Rig (TSTR). The design and development of the annular combustor for the TSTR are described. Some pertinent design characteristics of the combustor are: fuel, Jet A; inlet temperature, 525/sup 0/F; inlet pressure, 7.5 Atm; temperature rise, 2475/sup 0/F; efficiency, 98.5%; exit temperature pattern, 0.25; and exit mass flow, 92.7 pps. The development program was conducted on a 60/sup 0/ sector of the full-round annular combustor. Most design goals were achieved, with the exception of the peak gas exit temperature and local metal temperatures at the rear of the inner liner, both of which were higher than the design values. Subsequent turbine vane cascade testing established the need to reduce both the peak gas temperature (for optimum vane cooling) and the inner liner metal temperature (for combustor durability). Further development of the 60/sup 0/ combustor sector achieved the required temperature reductions and the final configuration was incorporated in the TSTR full-annular burner.
- Research Organization:
- Curtiss-Wright Corp., Wood-Ridge, NJ (USA)
- Sponsoring Organization:
- USDOE Office of Fossil Energy (FE)
- DOE Contract Number:
- AC01-76ET10348
- OSTI ID:
- 5344310
- Report Number(s):
- CW-WR-76-020.73A; ON: DE82014579
- Resource Relation:
- Other Information: Portions of document are illegible
- Country of Publication:
- United States
- Language:
- English
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High-temperature-turbine technology program. Phase II. Technology test and support studies. Turbine spool technology rig, cascade tests
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42 ENGINEERING
COAL LIQUIDS
COMBUSTION
COMBINED-CYCLE POWER PLANTS
COMBUSTORS
DESIGN
OPERATION
PERFORMANCE
COOLING
EXPERIMENTAL DATA
FUEL INJECTION SYSTEMS
GAS TURBINES
HEAT TRANSFER
MECHANICAL VIBRATIONS
PERFORMANCE TESTING
STRESS ANALYSIS
TEST FACILITIES
VERY HIGH TEMPERATURE
CHEMICAL REACTIONS
DATA
ENERGY TRANSFER
FLUIDS
FUEL SYSTEMS
INFORMATION
LIQUIDS
MACHINERY
NUMERICAL DATA
OXIDATION
POWER PLANTS
TESTING
THERMAL POWER PLANTS
THERMOCHEMICAL PROCESSES
TURBINES
TURBOMACHINERY
200104* - Fossil-Fueled Power Plants- Components
421000 - Engineering- Combustion Systems