Suspending loads from a helicopter

• US 5,417,304 A
• Filed: 05/14/1993
• Issued: 05/23/1995
• Est. Priority Date: 05/15/1992
• Status: Expired due to Term

• Current Assignee: Michael P. Kurtgis
• Original Assignee: Michael P. Kurtgis
• Inventors: Kurtgis, Michael P.
• Primary Examiner(s): CHIN SHUE, ALVIN C
• Application Number:
  US08/062,786
• Time in Patent Office: 739 Days
• Field of Search: 182/150, 182/145, 182/3, 182/7, 244/137.4, 244/118.1, 244/137.1
• US Class Current: 182/150
• CPC Class Codes: B64D 1/18 by spraying, e.g. insecticides spraying apparatus per se B05B
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface

Abstract

An arrangement and method for suspending a load from a rotary winged aircraft such as a helicopter by two releasable connections, wherein the load is adapted to be detached from the rotary winged aircraft upon both connections being released. Further safety features are also claimed.

Claims

1. An arrangement for suspending a load from a rotary winged aircraft including:

a first releasable strap means and a second releasable strap means, both Strap means extending around a secure pad of said rotary winged aircraft; and

a connection means attached to or integral with said first strap means, said first strap means being adapted to suspend a load from said rotary winged aircraft when it is airborne, and said second strap means passing through said connection means, wherein said arrangement is adapted to suspend a load until both releasable strap means are released.

2. An arrangement for suspending a load from a rotary winged aircraft as in claim 1 in which both releasable strap means are straps, each having two ends connected together by a releasable connecting arrangement.

3. An arrangement for suspending a lead from a rotary winged aircraft as in claim 2 in which there is an elongate length of suspension means between said lead and said connection means or strap means.

4. An arrangement for suspending a load from a rotary winged aircraft as in claim 3 in which there is an extension means within said suspension means or strap means, said extension means being adapted to extend the length of the said suspension means when a greater than a pro-determine value is applied to said suspension means.

5. An arrangement for suspending a load from a rotary winged aircraft

as in claim 4 in which said extension means is adapted to provide a warning signal upon extending the length of said suspension means.

6. An arrangement for suspending a load from a rotary winged aircraft as in claim 4 in which said suspension means includes at least one non-conductive length and said load is a human located within a bosun chair at the bottom of said suspension means, said bosun chair having a suspension means attachment device and a transmission system attachment device, said suspension means attachment device being adapted to be detached from said suspension means upon said transmission system attachment device being attached to said transmission system such that said lead is suspended from said transmission system.

7. An arrangement for suspending a lead from a rotary winged aircraft as in claim 4 in which an emergency release mechanism included within said suspension means includes s quick release mechanism adapted to be activated by a human lead.

8. An arrangement for suspending a load from a rotary winged aircraft including:

two releasable strap means extending around a secure part of said rotary winged aircraft; and

a connection means arranged such that both releasable strap means pass through said connection means, said connection means being adapted to suspend a load from said rotary winged aircraft when it is airborne, wherein said arrangement is adapted to suspend a load until both releasable strap means are released.

9. An arrangement for suspending a load from a rotary winged aircraft as in claim 8 in which the releasable strap means are straps, each having two ends connected together by a releasable connecting arrangement.

10. An arrangement for suspending a load from a rotary winged aircraft as in claim 9 in which the strap means are adapted to disconnect rapidly said two ends from each other.

11. An arrangement for suspending a load from a rotary winged aircraft as in claim 8 in which there is a protective sleeve covering both said strap means.

12. An arrangement for suspending a lead from a rotary winged aircraft as in claim 11 in which there is an extension means within said suspension means, said extension means being adapted to extend the length of the said suspension means when a force greater than a pro-determine value is applied to said suspension means.