Auxiliary, rotatable, independent jet engines on plane fuselage

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/20 (2006.01) B64C 15/14 (2006.01) B64D 27/26 (2006.01) B64D 33/00 (2006.01)

Patent

CA 2507280

1. A transport plane with 2 (or 4) primary jet engines-under-the-wing is supplemented by a smaller proficient "Auxiliary" jet engine installed on each side of the rear fuselage that has the mechanical and technological capability to rotate 180 degrees for Horizontal Short Take Off and Landing (H/STOL) capability. The exhaust thrust of the "Auxiliary" jet engines rotated to the front on landing serves as a direct and efficient braking mechanism for the jet plane to stop on a short runway and also to effectively "backup" the plane to its setting and there, expeditiously load or unload its cargo of either peace keeping military troops and equipment or humanitarian aid. The two "Auxiliary" jet engines are independent and have separate controls for rotatability, have their own fuel supply and electrical system with the pilot able to shift essential flight controls and thrust of the plane to the "Auxiliary" jet engines on "standard mode" either during high altitude flying to conserve fuel or in the event of an emergency, have sufficient power for the pilot to land the plane and its cargo safely. The invention is applicable to private and commercial jet planes.

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