Airplane fuselage structure

Details Airplane fuselage structure Airplane fuselage structure

1975-07-31

1977-01-04

Blix, Trygve M.

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

244108, B64C 108

Patent

active

040008711

ABSTRACT:
An airplane fuselage of a type having a concave bottom for providing more lift and control at low speeds and with two strut members extending along and on each side of the concave bottom for providing skids for the purpose of emergency landings. The two bottom strut members are connected at the forward end thereof but are spaced apart at the rear end thereof to prevent an aircraft from turning to one side or the other due to direct contact with the ground or a body of water. A top and central strut member is also provided on the fuselage. Relatively short wings are attached to the fuselage portion, all parts of which are located above the two lower strut members. The landing gear is located in the wing structure.

REFERENCES:
patent: 1727394 (1929-09-01), Carns
patent: 1754733 (1930-04-01), Yohe
patent: 3473761 (1969-10-01), Chutter

Affiliated with

Also associated with

Rating

Airplane fuselage structure does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Airplane fuselage structure, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Airplane fuselage structure will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-249511