Two categories of controls advanced, one for system restricted to initiation during landing roll, other for initiation during flight; actuation system under development in relation to these requirements; its power transmission system is composed of variable displacement hydraulic pump designed as engine component; system believed to be adaptable to number of reverser systems, missions, and aircraft types. (See also Soc Automotive Engrs -- Paper n 49C for meeting Apr 8-11 1958 12 p)
Control systems for thrust reversal
SAE -- J
Society of Automotive Engineers -- Journal ; 66 , n 7
1958
2 pages
Article (Journal)
English
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