Articulated heliport pad

• US 4,834,321 A
• Filed: 03/09/1987
• Issued: 05/30/1989
• Est. Priority Date: 03/09/1987
• Status: Expired due to Fees

• Current Assignee: Denis Granger
• Original Assignee: Denis Granger
• Inventors: Granger, Denis
• Primary Examiner(s): BAREFOOT, GALEN L
• Application Number:
  US07/023,630
• Time in Patent Office: 813 Days
• Field of Search: 244/1 R, 244/63, 244/17.17, 244/114 R, 244/115, 244/116, 410/77, 410/80, 410/107, 410/111, 410/117, 410/157, 410/12, 410/100, 340/949
• US Class Current: 244/110.00E
• CPC Class Codes: B64F 1/007 Helicopter portable landing pads
• CPC Class Codes: B64F 1/125 Mooring or ground handling devices for helicopters

Abstract

An articulated heliport pad in which the pilot controls the rotation of a central disk for last minute changes in wind direction as well as the operation of a unique hold-down device.

Claims

1. A helicopter landing pad comprising a substantially horizontal planar surface having a generally circular aperture;

a disk substantially coplanar with said planar surface and substantially filling said aperture therein;

selectively operable radio controlled means disposed beneath said planar surface for selectively rotating said disk within said aperture about a vertical axis; and

selectively operable hold-down means carried by said disks for clamping the landing gear of a helicopter, said hold-down means including radio controlled clamping means selectively positionable from a first position at or below the elevation of said disk to a second position above the elevation of said disk clamping the landing gear of a helicopter.

2. The helicopter landing pad of claim 1 including first lighting means on said surface for indicating wind direction.

3. The helicopter landing pad of claim 2, wherein said first lightening means is radio controlled.

4. The helicopter landing pad of claim 3, including second lighting means carried by said disk to indicate the orientation thereof.

5. The helicopter landing pad of claim 1, including second lighting means carried by said disk to indicate the orientation thereof.

6. The helicopter landing pad of claim 5, wherein said second lighting means is radio controlled.

7. The helicopter landing pad of claim 1, wherein said disk rotating means includes a chain drive.

8. The helicopter landing pad of claim 1, wherein said disk includes a plurality of gear teeth around the periphery thereof,

wherein said disk rotating means includes a motor driven gear in operable engagement with said gear teeth, and

wherein said pad includes a plurality of rotatable supports each engaging said disk at one of a like plurality of spaced points adjacent the periphery thereof.

9. The helicopter landing pad of claim 1, wherein said disk includes a plurality of parallel slots;

wherein each said slot in said disk includes a pair of clamps simultaneously displaceable toward each other to effect clamping of the helicopter; and

wherein said clamping means are disposed within said slots below the upper surface of said disk in said first position.

10. The helicopter landing pad of claim 9 wherein the movement of said clamps is independently responsive to the pressure of engagement with the helicopter.

11. A helicopter landing pad comprising a substantially horizontal planar surface having a generally circular aperture;

a disk substantially coplanar with said planar surface and substantially filling said aperture therein;

means disposed beneath said planar surface for selectively rotating said disk within said aperture about a vertical axis; and

selectively operable radio controlled hold-down means carried by said disk, for clamping the landing gear of a helicopter said hold-down means including clamping means selectively positionable from a first position at or below the elevation of said disk to a second position above the elevation of said disk clamping the landing gear of a helicopter, said hold-down means including pressure responsive means responsive to the pressure of engagement of said clamping means on the landing gear of a helicopter, and the locking of said hold-down means being responsive to said pressure means.

12. The helicopter landing pad of claim 11, wherein deactivation of said hold-down means is radio controlled, and including means for returning said hold-down means to said first position upon the deactivation thereof.

13. A method of landing a helicopter on a heliport having selectively rotatable landing disk with a selectively operable hold-down device comprising the steps of:

(a) providing a selectively rotatable disk having a selectively operable hold-down carried by the disk;

(b) selectively rotating the disk to a predetermined position relative to the wind;

(c) landing the helicopter into the wind onto the disk;

(d) activating the hold down responsively to the helicopter to secure the helicopter to the disk; and

(e) thereafter shutting off the helicopter engine.

14. The method of claim 13 wherein the rotation of the disk is remotely controlled from the helicopter.

15. Means for selectively securing a helicopter to a generally horizontal heliport comprising:

a surface;

a plurality of elongated parallel slots in said surface;

means associated with each of said slots adapted to clamp the landing gear of a helicopter;

means associated with each of said slots for selectively positioning said clamps between a first position in one of said slots at an elevation below said surface and a second position above the elevation of said surface and displaced along the length of said slot sufficiently to contact with the landing gear of a helicopter, said means for displacing said clamps acting in opposite directions in different ones of said slots, each of said clamps including means for sensing the pressure of said clamp against the landing gear of the helicopter.

16. The helicopter securing means of claim 15 including two clamps and two selective positioning means associated with said slots;

and wherein said two clamps for each of said slots are displaced in opposite directions.

17. The helicopter receiving means of claim 15 wherein each of said clamps includes an elongated roller for engaging the landing gear of the helicopter.

18. The helicopter receiving means of claim 15 wherein the displacement of the clamp in one of each of said slots is independent of the displacement of the clamp in each of the other of said slots.