Suspendible carrier for carrying multiple cargo loads by helicopter

• US 5,927,649 A
• Filed: 03/07/1997
• Issued: 07/27/1999
• Est. Priority Date: 03/07/1997
• Status: Expired due to Term

• Current Assignee: Mitcham Canada ULC
• Original Assignee: Donald Terry Nykiforuk
• Inventors: Nykiforuk, Donald Terry
• Primary Examiner(s): Jordan, Charles T.
• Assistant Examiner(s): DINH, TIEN QUANG
• Application Number:
  US08/813,197
• Time in Patent Office: 872 Days
• Field of Search: 244/137.4, 244/137.1, 244/118.1, 294/82.24, 294/82.26, 294/82.3, 294/82.19, 294/82.31, 258/1.2, 258/1.4, 258/1.6, 258/1.8
• US Class Current: 244/118.1
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface

Abstract

A suspendible carrier is provided for receiving and carrying cargo from an aircraft. A detachable ground assembly releasably engages cargo to the carrier, and has a coupling means consisting of an elongate vertically-oriented shank having a coupling, such as a widened head, at its upper end. A pylon or other support structure holds the coupling in a vertical position prior to pickup by the helicopter. A cargo suspension assembly is suspended from the cable, and has a coupling engagement apparatus to releasably engage the coupling. The coupling engagement apparatus has a receiving portion to engage the coupling and a retaining portion to retain the coupling. The receiving portion may consist of a panel hinged with a one-way hinge to the engagement apparatus. The coupling is transported from the receiving portion to the retainer portion, preferably by maintaining the coupling engagement apparatus in a rearwardly-tilted orientation to permit couplings to slide towards the retainer portion. A release mechanism selectively and individually releases couplings from the suspension assembly. Preferably, the cargo suspension assembly has an elongate shape adapted to retain multiple cargo carriages. The cargo release mechanism may comprise a release arm and a keeper, both of which are pivotally mounted to the suspension assembly and engageable with a coupling. The release arm pivots to a discharge position to discharge a single coupling while the keeper prevents rearward travel of further couplings. In the retainer position, the keeper permits rearward travel of coupling units to the release arm, and the release arm engages a single coupling and prevents its release.

Claims

1. A carrier for suspension of a cargo load from an aircraft, comprising:

a) a ground assembly comprising a support structure, a coupling member having an enlarged head supported on a shank forming a neck member, and means to releasably engage said coupling member to a cargo load;

b) an airborne assembly suspendible from an aircraft, comprising an elongate frame, coupling member pickup means at a first end of said frame, coupling member retaining means at a second end of said frame, and transport means to convey said coupling members from said first end to said second end following pickup of said ground assembly by said carrier, said pickup means comprising a pair of elongate parallel flanges mounted to said frame and spaced apart to define a slot therebetween, at least one of said flanges being hinged to said frame for pivotal movement upwardly to a first position wherein said slot is widened sufficiently to permit passage of said head through said slot, said pivotal movement permitting downward rotation of said at least one flange to a second position limited by a stop means wherein said slot is narrowed sufficiently to prevent downward release of said head whereby said coupling member is suspended by said head from said pickup means; and

c) cable means to suspend said airborne assembly from an aircraft.

2. A carrier as in claim 1, wherein said frame is disposed at an angle forming a downward slope from said first end to said second end when said airborne assembly is suspended from an aircraft, sufficient to permit said coupling means to slide by action of gravity towards said second end.

3. A carrier as in claim 1, wherein there is further provided a front skirt depending from said airborne assembly to provide a ground contact for said cargo suspension assembly and to guide said coupling means into said coupling member pickup means.

4. A carrier as in claim 1 wherein there is further provided at least one rear leg depending from the rear of said airborne assembly, said at least one rear leg providing ground contact means to elevate said rear of said airborne assembly during load pickup and discharge operations.

5. A carrier as in claim 1, wherein said ground assembly includes a support to hold the coupling means in a generally vertical position.

6. A carrier as in claim 5, wherein said support includes an aperture for receiving said coupling means whereby said support is detachable from said coupling means, and detaches therefrom when said ground assembly is engaged by said suspension assembly.

7. A carrier as in claim 6, wherein said support comprises an inverted generally cone-shaped member having a receptacle at the upper end of said frame member to releasably receive said coupling means.

8. A carrier as in claim 1, further comprising release means to sequentially release said coupling members from said second end of said airborne assembly, comprising a release arm pivotally mounted to said suspension assembly, said release arm engageable at a first end with a first of said coupling member to control the release thereof, and a keeper pivotally mounted to said airborne assembly and engageable with a second said coupling member, wherein said release arm pivots to a discharged position to discharge said first coupling member while said keeper prevents rearward travel of further of said coupling members and to a retainer position wherein said keeper permits rearward travel of said second coupling member to said release arm.

9. A carrier as in claim 8 wherein rotation of both said keeper and said release arm is controlled by a lock arm, opposing ends of which contact said release arm and said keeper respectively, said lock arm being pivotally mounted to said airborne assembly and rotatably driven by a motor.

10. A carrier as in claim 9, wherein the keeper comprises an elongate, generally, horizontal member having a downwardly-extending foot at one end thereof to obstruct passage of couplings.

11. A carrier as in claim 10, wherein said release arm has a lower end defined by a concave portion for releasably cradling said first coupling, and an upper end adapted to slideably engage said lock arm.

12. A carrier as claimed in claim 1, wherein said pickup means and said retaining means respectively comprise first and second pairs of flanges, said first and second pairs of flanges each being disposed about a common vertical plane, said first and second pairs of flanges further being aligned to permit said coupling member to be conveyed from said pickup means to said retaining means.

13. A carrier for suspension of multiple cargo loads from an aircraft, comprising:

a) at least two ground assemblies each comprising a support structure, a coupling member having an enlarged head supported on a shank comprising a neck member, and means to releasably engage said coupling member to a cargo load;

b) an airborne assembly suspendible from an aircraft comprising an elongate frame, coupling member pickup means at a first end of said frame, coupling member retaining means at a second end of said frame, and transport means to convey said coupling members from said first end to said second end following pickup of each of said ground assemblies by said carrier, said pickup means comprising a pair of elongate parallel flanges mounted to said frame and spaced apart to define a slot therebetween, at least one of said flanges being hinged to said frame for pivotal movement upwardly to a first position wherein said slot is widened sufficiently to permit passage of said head through said slot, said pivotal movement permitting downward rotation of said at least one flange to a second position limited by a stop means wherein said slot is narrowed sufficiently to prevent downward release of said head whereby said coupling member is suspended by said head from said pickup means;

c) release means associated with said airborne assembly to sequentially release each of said ground assemblies from said second end; and

d) cable means to suspend said airborne assembly from an aircraft.

14. A carrier as in claim 13, wherein said frame is disposed at an angle forming a downward slope from said first end to said second end when said airborne assembly is suspended from an aircraft, sufficient to permit said coupling means to slide by action of gravity towards said second end.

15. A carrier as in claim 13, wherein there is further provided a front skirt depending from said airborne assembly to provide a ground contact for said airborne assembly and to guide said coupling means into said coupling engagement means.

16. A carrier as in claim 13, wherein there is further provided at least one rear leg depending from the rear of said airborne assembly, said at least one rear leg providing ground contact means to elevate said rear of said airborne assembly during load pickup and discharge operations.

17. A carrier as in claim 13, wherein said ground assembly includes a support to hold the coupling means in a generally vertical position.

18. A carrier as in claim 17, wherein said support includes an aperture for receiving said coupling means whereby said support is detachable from said coupling means, and detaches therefrom when said ground assembly is engaged by said suspension assembly.

19. A carrier as in claim 18, wherein said support comprises an inverted generally cone-shaped member and said support means comprises a receptacle at the upper end of said frame member to receive said coupling means.

20. A carrier as in claim 13, further comprising release means to sequentially release said coupling members from said second end of said airborne assembly, comprising a release arm pivotally mounted to said suspension assembly, said release arm engageable at a first end with a first said coupling member to control the release thereof, and a keeper pivotally mounted to said airborne assembly and engageable with a second said coupling member, wherein said release arm pivots to a discharged position to discharge said first coupling member while said keeper prevents rearward travel of further, of said coupling members and to a retainer position wherein said keeper permits rearward travel of said second coupling member to said release arm.

21. A carrier as in claim 20, wherein rotation of both said keeper and said release arm is controlled by a lock arm, opposing ends of which contact said release arm and said keeper respectively, said lock arm being pivotally mounted to said suspension assembly and rotatably driven by a motor.

22. A carrier as in claim 21, wherein the keeper comprises an elongate, generally, horizontal member having a downwardly-extending foot at one end thereof to obstruct passage of couplings.

23. A carrier as in claim 22, wherein said release arm has a lower end defined by a concave portion for releasably cradling said first coupling, and an upper end adapted to slideably engage said lock arm.

24. A carrier as claimed in claim 13, wherein said pickup means and said retaining means respectively comprise first and second pairs of flanges, said first and second pairs of flanges each being disposed about a common vertical plane, said first and second pairs of flanges further being aligned to permit said coupling member to be conveyed from said pickup means to said retaining means.

25. A method for sequentially picking up and discharging multiple cargo loads from an aircraft, comprising the steps of:

a) providing a carrier comprising first and second ground assemblies each associated with a cargo load and comprising a coupling member having an enlarged head supported on a neck member;

an airborne assembly comprising an elongate frame, coupling member pickup means at a first end of the frame, coupling member retaining means at a second end of the frame, said pickup means comprising a pair of elongate parallel flanges mounted to the frame and spaced apart to define a slot therebetween, with at least one of the flanges being hinged to the frame for pivotal movement upwardly to a first position wherein the slot is relatively widened, and downwardly to a second position wherein the slot is relatively narrowed;

release means for selectively releasing a first of said ground assemblies from said second end; and

a cable means to suspend the airborne assembly from an aircraft;

b) supporting each coupling member on the ground within a generally vertical position wherein the head forms the upper end thereof;

c) lowering the airborne assembly on a first ground assembly, whereby the coupling member head contacts the pickup means;

d) rotating the at least one flange upwardly, by lowering the airborne assembly relative to the coupling member, to permit the head to pass through said slot;

e) rotating the at least one flange downwardly, to narrow the slot sufficiently to restrict release of the coupling member head from the pickup means;

f) elevating the airborne assembly, thereby suspending the first ground assembly and cargo load therefrom;

g) conveying the first ground assembly to the second end of the airborne assembly;

h) repeating steps c through g with a second of said ground assemblies and cargo loads;

i) releasing the first said ground assembly and cargo load from the second end by actuating the release means.