U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Microwave-powered aircraft

Patent 5503350 Issued on April 2, 1996. Estimated Expiration Date: Icon_subject October 28, 2013. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

D139634

D145145

1893129

2604276

Airplane configured with a moveable disk structure
Patent #: 4662588
Issued on: 05/05/1987
Inventor: Henderson

Dual polarization electromagnetic power reception and conversion system
Patent #: 4943811
Issued on: 07/24/1990
Inventor: Alden, et al.

Microwave powered aircraft
Patent #: 4955562
Issued on: 09/11/1990
Inventor: Martin, et al.

Power beaming system
Patent #: 5068669
Issued on: 11/26/1991
Inventor: Koert, et al.

All wing aircraft
Patent #: 5082204
Issued on: 01/21/1992
Inventor: Croston

Power beaming system with printer circuit radiating elements having resonating cavities Patent #: 5218374
Issued on: 06/08/1993
Inventor: Koert, et al.

Inventor

Assignee

Application

No. 145204 filed on 10/28/1993

US Classes:

244/1R, MISCELLANEOUS244/13, Airplane sustained244/62, AIRCRAFT PROPULSION244/190, Of pilotless aircraft244/194Monitoring circuit or response

Examiners

Primary: Grant, William

Attorney, Agent or Firm

Foreign Patent References

  • 951902 FR 11/04/2012

International Class

B64C 039/02

Abstract

An unmanned, remotely controlled microwave-powered aircraft for use as a stationary communications platform. The aircraft is generally a flying wing with a large, flat inner wing having a rectenna on the underside. Rectennas may also be provided on the underside of the wings, the combined output from the rectenna being used to provide power to two electric motors housed within torpedo-shaped nacelles which drive two rear propellers. The rectenna converts a microwave signal at 35 GHz generated by a ground power station utilizing dual gyrotrons and a 34-meter diameter antenna dish. The aircraft has a preferred airfoil cross section throughout and is constructed of lightweight but strong materials in order to provide an enhanced flying time of several months. A power management and distribution system manages the DC power produced by the rectenna to supply power to the flight controls, propulsion system and payload.

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