CA3101109C - Systeme porteur de charge - Google Patents

Systeme porteur de charge Download PDF

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Publication number
CA3101109C
CA3101109C CA3101109A CA3101109A CA3101109C CA 3101109 C CA3101109 C CA 3101109C CA 3101109 A CA3101109 A CA 3101109A CA 3101109 A CA3101109 A CA 3101109A CA 3101109 C CA3101109 C CA 3101109C
Authority
CA
Canada
Prior art keywords
load
attached
carrying assembly
attachment
load carrying
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CA3101109A
Other languages
English (en)
Other versions
CA3101109A1 (fr
Inventor
Michael Behrens
Heiko Brosinger
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Helicopters Deutschland GmbH
Original Assignee
Airbus Helicopters Deutschland GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Helicopters Deutschland GmbH filed Critical Airbus Helicopters Deutschland GmbH
Priority to CA3101109A priority Critical patent/CA3101109C/fr
Publication of CA3101109A1 publication Critical patent/CA3101109A1/fr
Application granted granted Critical
Publication of CA3101109C publication Critical patent/CA3101109C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/22—Taking-up articles from earth's surface
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B66—HOISTING; LIFTING; HAULING
    • B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C13/00—Other constructional features or details
    • B66C13/04—Auxiliary devices for controlling movements of suspended loads, or preventing cable slack

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Automatic Assembly (AREA)

Abstract

Les réalisations décrites portent sur un système porteur de charge 190 permettant de transporter une charge avec un aéronef à voilure tournante 100. Le système porteur de charge 190 comprend un câble de fret 175 et un système de prise de charge 200. Le câble de fret 175 peut avoir une première extrémité 176 pouvant être reliée à un monte-charge 170 ou à un crochet délesteur de fret 180. Le système de prise de charge 200 peut comprendre une première fixation 230 attachée à la deuxième extrémité 177 du câble de fret 175, une deuxième fixation 235 qui est adaptée pour accueillir une charge, un appareil de raccord 240 qui relie la première fixation 230 à la deuxième fixation 235, et au moins deux unités de première et deuxième poussées 210a, 210b, 220a, 220b qui sont attachés à lappareil de raccord 240 et produisent une poussée dans une direction orthogonale par rapport à lextension du cargo de fret.
CA3101109A 2020-11-27 2020-11-27 Systeme porteur de charge Active CA3101109C (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA3101109A CA3101109C (fr) 2020-11-27 2020-11-27 Systeme porteur de charge

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA3101109A CA3101109C (fr) 2020-11-27 2020-11-27 Systeme porteur de charge

Publications (2)

Publication Number Publication Date
CA3101109A1 CA3101109A1 (fr) 2021-02-08
CA3101109C true CA3101109C (fr) 2023-03-21

Family

ID=74575199

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3101109A Active CA3101109C (fr) 2020-11-27 2020-11-27 Systeme porteur de charge

Country Status (1)

Country Link
CA (1) CA3101109C (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20250368325A1 (en) * 2024-06-03 2025-12-04 Rockwell Collins, Inc. Hoisting flight director mode
EP4717596A1 (fr) * 2024-09-25 2026-04-01 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Dispositif de pivotement pour relier une cargaison humaine et/ou non humaine à un giravion

Also Published As

Publication number Publication date
CA3101109A1 (fr) 2021-02-08

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