Thrust reverser for by-pass gas turbine engine

Details Thrust reverser for by-pass gas turbine engine Thrust reverser for by-pass gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

K

60/83

F02K 3/02 (2006.01) F02K 1/74 (2006.01)

Patent

CA 1061579

IN THE CANADIAN PATENT OFFICE Inventors: LESLIE RICHARD HARPER WILLIAM JAMES LEWIS DAVID ROBERTS MCMURTRY LANCE PETER BELL JOHN MATTHEW HALL Invention: THRUST REVERSER FOR BY-PASS GAS TURBINE ENGINE ABSTRACT OF DISCLOSURE 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 bypass air, is combined with a target thrust reverser. The ratio of the total pressure of the bypass 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 fibre re-inforced composite materials.

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