An Overview of High Bandwidth Liquid Fuel Flow Modulators Developed for Active Combustion Control Research

Saus, Joseph R ; Thomas, Randy

关键词: ACTIVE CONTROL;    COMBUSTION CONTROL;    LIQUID FUELS;    MODULATORS;    PERFORMANCE TESTS;    THERMOACOUSTIC EFFECTS;    BANDWIDTH;    COMMERCIAL OFF-THE-SHELF PRODUCTS;    MODULATION;    NASA PROGRAMS;    PIEZOELECTRICITY;   

RP-ID  :  NASA/TM-2018-220003,E-19610,GRC-E-DAA-TN60803

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

This paper presents a description of the general construction of three high bandwidth liquid fuel modulators along with data corresponding to their respective modulation performance. These devices are a critical element of the National Aeronautics and Space Administration Glenn Research Center's (NASA GRC) Active Combustion Control (ACC) task. These devices are not commercially-off-the-shelf available, primarily due to a one kHz bandwidth requirement. Given their special nature, NASA GRC developed specifications for the modulation devices and then, through Small Business Innovative Research (SBIR) contracts, had vendors with expertise in valve design manufacture them. The modulators described in this paper are the Active Signal Modulator (ASM), the Jansen's Aircraft System Controls (JASC) modulator, and the WASK Engineering (WASK) modulator. These modulators utilize magnetostrictive, electric motor, or piezoelectric actuation, respectively. The specifications for these devices evolved over time to meet the needs of changing objectives in the ACC research task. This is primarily true with respect to flow number as their designs accommodate a range from one to eight (lbm./hr-psi0.5). These designs also exhibit relatively small volume, weight, and power consumption with an ability to modulate approximately +/- 30% from the mean on a pressure basis. The modulators have been characterized and have undergone laboratory performance tests by the vendors. Their data indicated suitability for continued use in ACC research testing.