Thrust reverser for by-pass gas turbine engine

Power plants – Reaction motor – Interrelated reaction motors

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Details

60230, 60266, 23926527, F02K 120, F02K 306

Patent

active

040696634

ABSTRACT:
A by-pass gas turbine engine capable of producing an unmixed exhaust stream which comprises a core of hot turbine exhaust gases surrounded by an annular layer of by-pass air, is combined with a target thrust reverser. The ratio of the total pressure of the by-pass air to the total pressure of the turbine exhaust gases is arranged to be greater than unity to a significant extent, and the buckets are made from lightweight materials such as titanium, light alloys or even fiber re-inforced composite materials.

REFERENCES:
patent: 3550855 (1970-12-01), Feld et al.
patent: 3616648 (1971-11-01), Weise
patent: 3856239 (1974-12-01), Leibach
"Gas Turbine Engine," Pratt & Whitney Oper. Instr. 200, May, 1974, p. 219.

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