Aircraft vertical landing guidance method and system

• US 6,193,190 B1
• Filed: 01/08/1999
• Issued: 02/27/2001
• Est. Priority Date: 01/08/1999
• Status: Expired due to Fees

• Current Assignee: Nance C. Kirk
• Original Assignee: Nance C. Kirk
• Inventors: Nance, C. Kirk
• Primary Examiner(s): Swiatek, Robert P.
• Application Number:
  US09/226,951
• Time in Patent Office: 781 Days
• Field of Search: 244/17.17, 244/114.R, 244/183, 340/946, 340/953, 340/954, 340/955
• US Class Current: 244/114.00R
• CPC Class Codes: B64F 1/007 Helicopter portable landing pads
• CPC Class Codes: B64F 1/20 Arrangement of optical beacons
• CPC Class Codes: G05D 1/0676 specially adapted for landing
• CPC Class Codes: G05D 1/0858 specially adapted for vertical take-off of aircraft

Abstract

A vertical lift aircraft, such as a helicopter, can land in an area with impaired visibility such as fog. Around the landing area is a plurality of laser beam emitters. The emitters project a pattern of laser beams skyward. The helicopter finds the general area by spot-lights pointing up through the fog, or by navigation. As the helicopter approaches, it sends a radio signal, which is detected on the ground. The spot-lights are switched off and the laser emitters are switched on. The helicopter is positioned within the pattern so that the laser beams reflect off of a portion of the aircraft, such as the rotor blades. This forms a visual cue, which the pilot uses to maintain the position of the helicopter relative to the landing area and descends thereto.

Claims

1. A method of guiding a rotary wing aircraft to a landing zone, comprising the steps of:

a) projecting a pattern of focused nonintersecting discrete light beams from the landing zone skyward;

b) skyward of the landing zone, positioning the aircraft within the pattern;

c) illuminating simultaneously with at least a plurality of the light beams the rotary wing of the aircraft with the pattern so as to form a visual cue of the position of the aircraft relative to the landing zone.

2. The method of claim 1 wherein the focused light beams comprise beams of coherent light.

3. The method of claim 1 wherein the focused light beams comprise beams of incoherent light.

4. The method of claim 1 wherein the focused light beams comprise beams of visible light.

5. The method of claim 1 wherein the focused light beams comprise beams of invisible light, which light becomes visible when reflected off objects.

6. The method of claim 1 wherein the pattern of focused light beams projects vertically from the landing zone.

7. The method of claim 1 wherein the pattern of focused light beams projects skyward from the landing zone at an angle to vertical.

8. The method of claim 1 further comprising descending the aircraft to the landing zone using the visual cue.

9. The method of claim 1, further comprising the steps of:

a) detecting the approach of the aircraft to a position above the landing zone;

b) upon the detection of the approach of the aircraft, initiating the step of projecting a pattern of focused light beams from the landing zone skyward.

10. The method of claim 9 wherein the step of detecting the approach of the aircraft to a position above the landing zone further comprises the step of receiving a radio transmission from the aircraft.

11. The method of claim 1 further comprising the step of providing spot-lights at the landing zone before the step of projecting a pattern of focused light beams from the landing zone skyward so as to direct the aircraft to the general area of the landing zone.

12. The method of claim 1 wherein the light beams comprise a first color, further comprising the steps of:

a) projecting a second color of light into a crossing pattern of focused light beams at a first altitude;

b) projecting a third color of light into a crossing pattern of focused light beams at a second altitude.

13. The method of claim 1 wherein:

a) the focused light beams comprise beams of coherent light;

b) the landing zone has a predetermined shape and the pattern of focused light beams has a shape that corresponds to the landing zone shape.

14. The method of claim 1 wherein the focused light beams comprise beams of light in the infrared spectrum.

15. A method of guiding a rotary wing aircraft to a landing zone, comprising the steps of:

a) projecting a pattern of focused light beams from a landing zone skyward, the pattern having a curved shape so as to form a visual boundary;

b) skyward of the landing zone, positioning the aircraft within the shape;

c) illuminating the rotary wing of the aircraft with the pattern so as to form a visual cue of the position of the aircraft relative to the landing zone;

d) descending the aircraft while maintaining the aircraft within the shape, so as to continue to illuminate the rotary wing of the aircraft with the pattern.

16. The method of claim 15 wherein the pattern of focused light beams forms a cylinder as it is projected skyward.

17. A method of guiding a vertical lift aircraft to a landing zone, comprising the steps of:

a) providing diverging laser beams at the landing zone so as to direct the aircraft to the general area of the landing zone;

b) projecting a pattern of focused light beams from the landing zone skyward;

c) skyward of the landing zone, positioning the aircraft within the pattern;

d) illuminating part of the aircraft with the pattern so as to form a visual cue of the position of the aircraft relative to the landing zone.

18. A system of guiding a rotary wing aircraft to a landing zone, comprising:

a) an unobstructed area;

b) a plurality of laser beam emitters deployed in the unobstructed area, the emitters being arranged so as to project a pattern of light beams skyward and onto a descending aircraft;

c) a controller connected to the emitters, the controller comprising a detector that detects the approach of the aircraft to the landing zone, the controller also comprising a switch for operating the emitters upon the detection of the approach of the aircraft;

d) spot-lights connected to the controller, the controller operating the spot-lights so as to illuminate the space around the unobstructed area until the detector detects the approach of the aircraft to the landings zone, wherein the controller turns the spot-lights off.

19. The system of claim 18 wherein the emitters are first emitters and the light beams comprise a first color, further comprising second and third emitters, the second emitter projecting a second color of light into a crossing pattern of light beams at a first altitude above the landing zone, and the third emitter projecting a third color of light into a crossing pattern of light beams at a second altitude above the landing zone.