High altitude reconnaissance platform
First Claim
1. A high altitude, ultralight aircraft requiring no fuel comprising:
- an aircraft having wings with broad area upper and lower wing surfaces,a low speed propellor mounted on said aircraft;
electric motor means mounted on said aircraft and coupled to drive said propellor;
solar cell means for receiving solar energy and supplying electricity to power said motor means, said solar cell means being mounted on the upper surfaces of said wings;
long wavelength infrared (LWIR) responsive cell means for receiving albedo infrared energy from the earth and for supplying electricity to power said motor means, said LWIR cell means being mounted on the lower surfaces of said wings; and
means for storing excess electrical energy supplied by said solar and LWIR cell means beyond that needed for powering said motor means, and for supplying supplemental electrical power to said motor means when the power supplied from said cell means is inadequate;
whereby the aircraft may have a life at elevated altitudes of several years.
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Accused Products
Abstract
A high altitude, ultra lightweight aircraft has broad area relatively flat wings, and is provided with solar cells on its upper wing surfaces, and long wavelength, infrared responsive cells on its lower wing and fuselage surfaces, to provide enough power to maintain the aircraft aloft at high altitudes indefinitely. The aircraft is intended to fly at altitudes of about 60,000 feet to 110,000 feet, at speeds in the vicinity of 70 to 200 miles per hour. A battery or fuel cell and electrical system is provided to store excess electrical power and to supply electrical power when needed. A large, low speed, pusher propellor is driven by an electrical motor. The aircraft may be launched with an opaque balloon, which not only raises the aircraft to the desired elevation but also conceals it.
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Citations
17 Claims
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1. A high altitude, ultralight aircraft requiring no fuel comprising:
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an aircraft having wings with broad area upper and lower wing surfaces, a low speed propellor mounted on said aircraft; electric motor means mounted on said aircraft and coupled to drive said propellor; solar cell means for receiving solar energy and supplying electricity to power said motor means, said solar cell means being mounted on the upper surfaces of said wings; long wavelength infrared (LWIR) responsive cell means for receiving albedo infrared energy from the earth and for supplying electricity to power said motor means, said LWIR cell means being mounted on the lower surfaces of said wings; and means for storing excess electrical energy supplied by said solar and LWIR cell means beyond that needed for powering said motor means, and for supplying supplemental electrical power to said motor means when the power supplied from said cell means is inadequate; whereby the aircraft may have a life at elevated altitudes of several years. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A high altitude, ultralight aircraft requiring no fuel comprising:
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an aircraft having wings with broad area upper and lower wing surfaces; solar cell means for receiving solar energy and producing electricity, said solar cell means being mounted on the upper surfaces of said wings; long wavelength infrared (LWIR) responsive cell means for receiving albedo infrared energy from the earth and for producing electricity, said LWIR cell means being mounted on the lower surfaces of said wings; means for the storage of excess electrical energy supplied by said solar and said LWIR cell means; means for powering said aircraft to keep said aircraft aloft solely from the electricity from said solar cell means and said LWIR cell means, including means for supplementing the electrical power from said LWIR cells with power from said storage means at night, when no power is being generated by said solar cells; and opaque balloon means for raising said aircraft to the desired altitude with the aircraft within said balloon means; whereby the aircraft may remain aloft at elevated altitudes, day and night for extended periods of time. - View Dependent Claims (10, 11, 12, 13, 14, 15, 16)
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17. A high altitude, ultralight aircraft requiring no fuel comprising:
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an aircraft having wings with broad area upper and lower wing surfaces, and including both a rear wing and a front wing, said aircraft including a fuselage having a substantially flat lower surface; means for deflecting at least one of said wings for controlling the flight of said aircraft; low speed propellor means mounted for powering said aircraft; electric motor means mounted on said aircraft and coupled to drive said propellor means; solar cell means for receiving solar energy and supplying electricity to power said motor means, said solar cell means being mounted on the upper surfaces of said wings; long wavelength infrared (LWIR) responsive cell means for receiving albedo infrared energy from the earth and for supplying electricity to power said motor means, said LWIR cell means being mounted on the lower surfaces of said wings and on the flat lower surface of said fuselage; and means for storing excess electrical energy supplied by said cell means beyond that needed for powering said motor means, and for supplying supplemental electrical power to said motor means when the power supplied from said cell means is inadequate; whereby the aircraft may have a life at elevated altitudes of several years.
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Specification