Abstract: A novel airplane shelter provides a plurality of arched vertical support members arranged axially along a line corresponding to the fuselage of an airplane to be sheltered. A cantilever beam is attached to the apex of each arched vertical support member, forming a “spine” along the top of the aligned arched support members. The cantilever beam is attached at one end to the rearwardmost arched support member, and the opposite end extends forwardly past the forwardmost arched support member to a point corresponding to the forwardmost point of an airplane to be sheltered. Separate lateral support members are placed at points corresponding to the wingtips of the airplane. The result is an open frame that defines a volume capable of enclosing an airplane. A covering material is placed over the open frame and stretched taut or otherwise secured over the entire structure.

Abstract: A novel airplane shelter provides a plurality of arched vertical support members arranged axially along a line corresponding to the fuselage of an airplane to be sheltered. A cantilever beam is attached to the apex of each arched vertical support member, forming a “spine” along the top of the aligned arched support members. The cantilever beam is attached at one end to the rearwardmost arched support member, and the opposite end extends forwardly past the forwardmost arched support member to a point corresponding to the forwardmost point of an airplane to be sheltered. Separate lateral support members are placed at points corresponding to the wingtips of the airplane. The result is an open frame that defines a volume capable of enclosing an airplane. A covering material is placed over the open frame and stretched taut or otherwise secured over the entire structure.

Abstract: A novel airplane shelter provides a plurality of arched vertical support members arranged axially along a line corresponding to the fuselage of an airplane to be sheltered. A cantilevered beam is attached to the apex of each arched vertical support member, forming a “spine” along the top of the aligned arched support members. The cantilevered beam is attached at one end to the rearwardmost arched support member, and the opposite end extends forwardly past the forwardmost arched support member to a point corresponding to the forwardmost point of an airplane to be sheltered. Separate lateral support members are placed at points corresponding to the wingtips of the airplane. The result is an open frame that defines a volume capable of enclosing an airplane. A covering material is placed over the open frame and stretched taut over the entire structure.

Abstract: A collision avoidance system for airplanes particularly suited for clear weather visual circumstances which includes television cameras suitably positioned on an airplane to view all areas where there is a potential for collision with another airplane. The system includes an on-board television display in ready view of the pilot which is connected to a machine vision system predeterminedly programmed to respond to other flying objects which could present a collision hazard. The television cameras on the airplane are, in turn, connected to the machine vision system so as to transmit images to which it is responsive thereby causing an alert condition for pilot scrutiny.