Method of manufacturing a combustion enclosure with cooling by transpiration
作者： Andre Beaurain , Etienne Tiret
DOI:
关键词: Enclosure 、 Perpendicular 、 Transpiration 、 Cooling flow 、 Normalization property 、 Porosity 、 Flow (psychology) 、 Combustion 、 Materials science 、 Mechanics 、 Structural engineering
摘要: The invention relates to a method of manufacturing an enclosure containing hot gases cooled by transpiration. comprises porous wall and means for applying cooling fluid the outside face cause flow pass through application is formed disposing plurality liquid distribution pipes regularly around terminating tangentially on its in superposed horizontal injection levels. Feed channels are provided crossing substantially perpendicularly pipes, between each them, connected feed means. Calibration ducts determined section provided, connecting, at levels, vertical surrounding deliver predetermined headloss inside wall. adapted as function zone be optimize rates along
lens.org 参考文章(14)
Albert L Blubaugh, Robert J Kuntz, Charles B Mcgough, Richard J Labotz, Transpiration-cooled devices ,(1967)
Charles J. Obrien, Transpiration And Regenerative Cooling Of Rocket Engine ,(1989)
Jr Harry L Wheeler, Method of constructing a porous wall ,(1956)
Masaki Sasaki, Shigeki Ochi, Hiromi Gomi, Akinaga Kumakawa, Masayuki Niino, Ryuzo Watanabe, Yoshinobu Takeda, Nobuhito Kuroishi, Hiroshi Sakamoto, Akio Suzuki, Nobuyuki Yatsuyanagi, Yoshihiko Doi, Junjiro Takekawa, Yoshimichi Masuda, Method of producing rocket combustors ,(1984)
Kazuyuki Higashino, Ryo Horiuchi, Koichi Suzuki, Satoshi Saito, Combustor of high pressure burner for rocket engine and method of fabrication thereof ,(1989)
Anthony Fortini, Rocket chamber and method of making ,(1974)
Daniel A. Bales, James R. Joyce, Method of simultaneously forming rocket thrust chamber cooling tubes ,(1994)
Prosser Joe Calvin, Cooled nozzle construction ,(1961)
James E Webb, Multislot film cooled pyrolytic graphite rocket nozzle ,(1966)