| タイトル | NASA Lewis Research Center's combustor test facilities and capabilities |
| 本文（外部サイト） | http://hdl.handle.net/2060/19950020756 |
| 著者（英） | Bianco, Jean |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1995-05-01 |
| 言語 | eng |
| 内容記述 | NASA Lewis Research Center (LeRC) presently accommodates a total of six combustor test facilities with unique capabilities. The facilities are used to evaluate combustor and afterburner concepts for future engine applications, and also to test the survivability and performance of innovative high temperature materials, new instrumentation, and engine components in a realistic jet engine environment. The facilities provide a variety of test section interfaces and lengths to allow for flametube, sector and component testing. The facilities can accommodate a wide range of operating conditions due to differing capabilities in the following areas: inlet air pressure, temperature, and flow; fuel flow rate, pressure, and fuel storage capacity; maximum combustion zone temperature; cooling water flow rate and pressure; types of exhaust - atmospheric or altitude; air heater supply pressure; and types of air heaters - vitiated or nonvitiated. All of the facilities have provisions for standard gas (emissions) analysis, and a few of the facilities are equipped with specialized gas analysis equipment, smoke and particle size measurement devices, and a variety of laser systems. This report will present some of the unique features of each of the high temperature/high pressure combustor test facilities at NASA LeRC. |
| NASA分類 | RESEARCH AND SUPPORT FACILITIES (AIR) |
| レポートNO | 95N27176
NASA-TM-106903
E-9599
NAS 1.15:106903
AIAA PAPER 95-2681 |
| 権利 | No Copyright |
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