Portable aircraft hangar
View Patent ↗Disclosed is a portable aircraft hangar assembly for use with aircraft having a series of rotor blades. The assembly is specifically designed to support a canopy over the series of rotor blades. This is accomplished by positioning a series of mounts between the undersurface of the canopy and the rotor assembly of the helicopter. The assembly further includes rotor sleeves which can be slid over the ends of each rotor blade. The rotor sleeves are connected to the canopy by way of a series of adjustment straps and coupling members.
1. A portable hangar assembly for use with aircraft having a rotor assembly with rotor blades and a central axis, the hangar assembly comprising:
a canopy mount consisting of a series of bifilar mounts interconnected to the rotor assembly, the canopy mount being aligned with the central axis of the rotor assembly;
a canopy positioned over the rotor assembly, the canopy having a central portion that is supported at a distance above the rotor assembly by the canopy mount, wherein the edges of the canopy are secured to the rotor blades of the aircraft.
2. A portable hangar assembly for use with aircraft having a rotor assembly with rotor blades and a central axis, the hangar assembly comprising:
a canopy mount interconnected to the rotor assembly and being aligned with the central axis of the rotor assembly;
a canopy including a number of corners, the canopy positioned over the rotor assembly, the canopy having a central portion that is supported at a distance above the rotor assembly by the canopy mount, wherein the hanger further comprises a series of rotor sleeves positioned over the ends of the rotor blades, with each rotor sleeve being interconnected to a corner of the canopy, the rotor sleeves thereby securing the canopy to the rotor blades.
3. A shelter to be used in conjunction with an aircraft having a rotor assembly with a number of rotor blades, each of the rotor blades having an upper surface, the shelter comprising:
a canopy having upper and lower surfaces, a central extent and corners, the canopy being secured over top of the rotor assembly by a series of mounts so as to create a space between the upper surface of the rotor blades and the lower surface of the central extent of the canopy, the corners of the canopy being secured to each of the rotor blades by way of a series of rotor sleeves positioned over the ends of each rotor blade, wherein each rotor sleeve is interconnected to one of the corners of the canopy.
4. A shelter to be used in conjunction with an aircraft having a rotor assembly with a number of rotor blades, each of the rotor blades having an upper surface, the shelter comprising:
a canopy having upper and lower surfaces, the canopy being secured over top of the rotor assembly so as to create a space between the upper surfaces of the rotor blades and the lower surface of the canopy, wherein the canopy is further secured by way of rotor sleeves positioned over the ends of the rotor blades.
5. The shelter as described in claim 4 wherein the canopy is square and each corner of the canopy is secured to a corresponding rotor blade.