Load hook substructure

{
  "publication_number": "US10150565B2",
  "country": "US",
  "kind": "B2",
  "title": "Load hook substructure",
  "abstract": "A load hook substructure for attachment onto or into the cabin structure of a helicopter, having a housing in which a shaft with a hook attachment is mounted, such that a load hook can be connected with the shaft and thereby with the load hook substructure; this improves the flying characteristics of the helicopter in the case of flights with a load carried underneath. This is achieved in that the shaft passes through the interior of the housing in the longitudinal direction between a housing end wall and a housing wall, such that it can move linearly, and a return spring device is arranged between a damping plate arranged on the shaft and the housing end wall, and a damping device is arranged between the damping plate and the lower housing wall. The damping device has at least one flexibly compressible damping element, which develops a damping action in the event of a linear movement of the shaft.",
  "claims": [
    "1. A load hook substructure for attachment onto or into the cabin structure of a helicopter, comprising a housing in which a shaft with hook attachment means is mounted, such that a load hook can be connected with the shaft and thereby with the load hook substructure, wherein the shaft passes through an interior of the housing in a longitudinal direction between a housing end wall and a lower housing wall, such that the shaft is moveable linearly, and a return spring device is arranged between a damping plate arranged on the shaft and the housing end wall, and a damping device is arranged between the damping plate and the lower housing wall, wherein the damping device comprises at least one flexibly compressible damping element, which develops a damping action in the event of a linear movement of the shaft, wherein the housing has a hollow cylindrical wall, which encloses the interior of the housing and the therein-mounted return spring device, the shaft and the damping device, and wherein the load hook substructure further includes an anti-rotation device comprising at least one longitudinal slot running in the hollow cylindrical wall, in which guidance means attached to the damping plate can be moved.",
    "2. The load hook substructure of claim 1, wherein the at least one flexibly compressible damping element comprises a plurality of damping elements, stacked one above another, arranged between the damping plate and the lower housing wall.",
    "3. The load hook substructure of claim 2, wherein a reinforcing wall is arranged between adjacent damping elements, or between an outer damping element and the damping plate, and/or the lower housing wall.",
    "4. The load hook substructure of claim 2, wherein the plurality of damping elements are arranged in element stacks, and each element stack is held in a stack holder, at least one sidewall of which serves as a stop.",
    "5. The load hook substructure of claim 4, wherein the stack holders are designed to be more rigid and stiffer in bending than the damping elements.",
    "6. The load hook substructure of claim 4, wherein each of the element stacks has the same number of damping elements.",
    "7. The load hook substructure of claim 1, wherein the damping elements are configured in an annular shape enclosing the shaft.",
    "8. The load hook substructure of claim 1, wherein the return spring device has a spring embodied as a compression spring, which is mounted on the housing end wall and the shaft, surrounding a shaft guidance sleeve.",
    "9. The load hook substructure of claim 8, wherein the compression spring is operationally connected with the shaft by a spring retention pin.",
    "10. The load hook substructure of claim 1, wherein the shaft is guided such that the shaft is moveable linearly in a first shaft bearing positioned proximate the return spring device, and in a second bearing positioned proximate the damping device.",
    "11. The load hook substructure of claim 1, wherein the housing end wall is designed as a housing flange, by which the load hook substructure is attachable onto or into a cabin structure of a helicopter.",
    "12. The load hook substructure of claim 1, wherein a housing eye is arranged on the housing end wall, by which the load hook substructure can be suspended directly on or in a cabin structure of a helicopter, or indirectly, by a cable, on the cabin structure.",
    "13. The load hook substructure of claim 1, wherein the guidance means is designed as a bar, which by at least one bolt is attached to the periphery of the damping plate in a guidance means seating, and which can move through the longitudinal slot in a guided manner.",
    "14. The load hook substructure of claim 13, wherein the shaft passes through a tension spring in the return spring device, and a spring as a damping element, and the interior of the housing surrounded by the hollow cylindrical wall is filled with a fluid such that a hydromechanical damping action is achieved."
  ],
  "description_excerpt": "The present invention describes a load hook substructure for purposes of attachment onto or into a cabin structure of a helicopter, comprising a housing, in which a shaft with hook attachment means is mounted, such that a load hook can be connected with the shaft and thereby with the load hook substructure.\n\nAmongst other tasks helicopters are employed for load-carrying flights, wherein an item of freight, mounted outside the helicopter cabin, is transported by the helicopter from A to B. Various materials for various construction or maintenance tasks can be transported as the load, or in the case of rescue flights, a stretcher with living persons. As a general rule a load hook that can be remotely operated, with or without a load cable, is arranged on the outside of the helicopter, directly on the underside of its cabin, wherein during the load-carrying flight tensile forces are transferred directly from the load hook onto the underside of the cabin. Such a design is a simple and cost-effective solution, wherein the load hook can easily be removed when it is not in use. The load hook, or more particularly, a load hook substructure to which the load hook is attached, can participate in small swinging movements of the load during the flight; the possibilities for movement are however limited by the design, and such a structure is rather rigid.\n\nOther forms of embodiment are of known art, in which the load hook is attached to a separate load hook substructure.",
  "cpc": [
    "B64D 1/22",
    "B64C 27/04",
    "B64D 1/02",
    "B64D 9/00",
    "F16F 15/085",
    "F16F 3/04",
    "F16F 3/10",
    "F16M 13/02"
  ],
  "ipc": [
    "B64D 1/22",
    "F16F 15/08",
    "F16M 13/02",
    "B64C 27/04",
    "B64D 1/02",
    "B64D 9/00",
    "F16F 3/04",
    "F16F 3/10"
  ],
  "assignees": [
    "Kopter Group AG"
  ],
  "inventors": [
    "Martin Stucki",
    "Cosimo Donno"
  ],
  "filing_date": "2016-08-19",
  "publication_date": "2018-12-11",
  "grant_date": "2018-12-11",
  "priority_date": "2015-08-21",
  "application_number": "US-201615241156-A",
  "family_id": "54065138",
  "cited_by_count": 7,
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}