Microwave powered aircraft

• US 4,955,562 A
• Filed: 11/16/1988
• Issued: 09/11/1990
• Est. Priority Date: 11/24/1987
• Status: Expired due to Fees

• Current Assignee: Her Majesty The Queen In Right of Canada As Represented By The Minister of National Defence
• Original Assignee: Her Majesty The Queen In Right of Canada As Represented By The Minister of National Defence
• Inventors: Martin, John E., Lillemark, Arne, DeLaurier, James D., Jull, George W.
• Primary Examiner(s): Peters, Jr., Joseph F.
• Assistant Examiner(s): Sartelle, Anne
• Application Number:
  US07/272,015
• Time in Patent Office: 664 Days
• Field of Search: 244/62, 244/1 R, 244/45 R, 244/45 A, 244/87, 244/91, 343/705, 343/708
• US Class Current: 244/62
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64C 39/12 Canard-type aircraft
• CPC Class Codes: B64D 27/24 using steam or spring force jet aircraft B64D27/16
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 30/10 Wings
• CPC Class Codes: B64U 50/13 using external fans or propellers
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 50/35 by wireless transmission, e.g. by induction
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A microwave-powered aircraft has lifting surfaces for exerting lifting forces on the aircraft in response to the propulsion of the aircraft and a rectenna array for receiving and rectifying microwave energy transmitted to the aircraft from a location remote from the aircraft. An electric motor for driving a propeller is energized by microwave energy received by the rectenna array, which is provided in a body at the underside of the aircraft. The body has its major dimensions extending horizontally and is relatively shallow with a periphery which is vertically curved so as to reduce turbulence in the airstream over the body during flight. The body is separate from the lifting surfaces and shaped to at least substantially avoid the generation of lifting forces by the body.

Claims

1. A microwave-powered aircraft, comprising:

means for propelling the aircraft;

means defining lifting surfaces on the aircraft for exerting lifting forces on the aircraft in response to the propulsion of the aircraft;

means for receiving and rectifying microwave energy transmitted to the aircraft from a location remote from the aircraft;

the means for propelling the aircraft being operable in response to the microwave energy received by the microwave energy receiving and rectifying means; and

the microwave energy receiving and rectifying means comprising a rigid body of substantially circular plan form attached to the aircraft, the horizontal dimensions of the body being a substantial fraction of the aircraft wingspan and the body being relatively shallow with a periphery which is vertically curved so as to reduce turbulence in the airstream over the body during flight, and the body being separate from the lifting means and shaped to at least substantially avoid the generation of lifting forces by the body;

a plurality of downwardly-facing microwave antennas and associated rectifying elements at the underside of the body; and

microwave reflector means provided in the body above said microwave antenna for shielding a space located above said microwave reflector means and within the body from microwave radiation.

2. A microwave-powered aircraft as claimed in claim 1, wherein the body is of substantially elliptical vertical cross-sectional shape in planes parallel to the longitudinal axis of the aircraft.

3. A microwave-powered aircraft as claimed in claim 1, wherein the means defining lifting surfaces comprise wings located forwardly of the body, which serves as means for promoting longitudinal stability of the aircraft.

4. A microwave-powered aircraft as claimed in claim 1 or 2, wherein the aircraft includes a fuselage and a canard provided on the fuselage at a location disposed forwardly of the lifting surfaces for promoting longitudinal stability and control of the aircraft.

5. A microwave-powered aircraft as claimed in claim 1, wherein the aircraft includes a fuselage, the lifting surface defining means comprising a pair of wings, and a pylon of aerofoil cross-section is mounted on the fuselage and supports the wings.

6. A microwave-powered aircraft as claimed in claim 5, wherein the aerofoil cross-section of the pylon is symmetrical.

7. The microwave-powered aircraft as claimed in claim 5, wherein the pylon includes a flap at a trailing edge of the pylon for causing a side force to act on the aircraft independently of the angle of bank of the aircraft.

8. A microwave-powered aircraft as claimed in claim 7, further including end plate fairing means extending over the extent of travel of the flap for improving the efficiency of the flap.

9. A microwave-powered aircraft as claimed in claim 5, 6 or 7, wherein the means for propelling the aircraft include at least one propeller and electric motor means associated with the propeller for driving the propeller, the electric motor means being provided at the intersection of the pylon and the wings to protect the propeller.

10. A microwave-powered aircraft as claimed in claim 5, 6 or 7, wherein the wings comprise a pair of high aspect ratio wings, and side-facing sensors are provided on the pylon.

11. A microwave-powered aircraft as claimed in claim 1 or 2, wherein the lifting surface defining means comprise a pair of high aspect ratio wings.

12. The microwave-powered aircraft claimed in claim 1, further comprising:

means for laterally deflecting the course of travel of the aircraft without causing any substantial banking of the aircraft, wherein

the said laterally deflecting means comprises a vertically extending member having a horizontal cross-section of aerofoil shape and an adjustable flap extending along a vertically trailing edge of the deflecting member.

13. A microwave-powered aircraft as claimed in claim 12, further comprising a fuselage, the lifting surface defining means comprising a pair of fixed wings and the vertically extending member supporting the wings above the fuselage.

14. A microwave-powered aircraft as claimed in claim 12, wherein the laterally deflecting means are located at least approximately above the centre of gravity of the aircraft.

15. A microwave-powered aircraft as claimed in claim 13, wherein the means for propelling the aircraft comprise at least one propeller and electric motor means mounted above the vertically extending member for rotating the propeller.

16. A microwave-powered aircraft as claimed in claim 14, further comprising a canard provided forwardly of the lifting surfaces for promoting longitudinal stability and control of the aircraft.