Patent ID: 7089951

Claim:
A shelter for an airplane having a fuselage, wings and a tail, said shelter comprising: a plurality of vertical support members arranged parallel to each other and adapted to extend over the fuselage of an airplane between the tail of the airplane and the wings of the airplane; a singular cantilever beam attached to the upper portion of each one of said plurality of vertical support members, forming an upright-standing shelter structure with said cantilever beam, adapted to extend forwardly over the nose of the airplane; a pair of lateral support members adapted to be positioned proximate to each wingtip of said airplane; covering material arranged over said shelter structure, including over the cantilever beam and laterally to each said pair of lateral support members such that said airplane is adapted fit entirely beneath said covering material; support cables attached to said cantilever beam and to each of said lateral support members for supporting said covering material over the wings of said airplane and; means for anchoring the shelter.