IT8619008A0 - WEIGHT AND TORQUE INDICATION SYSTEM OF A HELICOPTER. - Google Patents

WEIGHT AND TORQUE INDICATION SYSTEM OF A HELICOPTER.

Info

Publication number
IT8619008A0
IT8619008A0 IT8619008A IT1900886A IT8619008A0 IT 8619008 A0 IT8619008 A0 IT 8619008A0 IT 8619008 A IT8619008 A IT 8619008A IT 1900886 A IT1900886 A IT 1900886A IT 8619008 A0 IT8619008 A0 IT 8619008A0
Authority
IT
Italy
Prior art keywords
helicopter
weight
indication system
torque indication
torque
Prior art date
Application number
IT8619008A
Other languages
Italian (it)
Other versions
IT1188221B (en
Inventor
Richard L Adelson
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Publication of IT8619008A0 publication Critical patent/IT8619008A0/en
Application granted granted Critical
Publication of IT1188221B publication Critical patent/IT1188221B/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/006Safety devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60Testing or inspecting aircraft components or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Component Parts Of Construction Machinery (AREA)
  • Toys (AREA)
  • Jib Cranes (AREA)
  • Cosmetics (AREA)
IT19008/86A 1985-01-03 1986-01-03 WEIGHT AND TORQUE INDICATION SYSTEM OF A HELICOPTER IT1188221B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US68853385A 1985-01-03 1985-01-03

Publications (2)

Publication Number Publication Date
IT8619008A0 true IT8619008A0 (en) 1986-01-03
IT1188221B IT1188221B (en) 1988-01-07

Family

ID=24764804

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19008/86A IT1188221B (en) 1985-01-03 1986-01-03 WEIGHT AND TORQUE INDICATION SYSTEM OF A HELICOPTER

Country Status (5)

Country Link
JP (1) JPS61211199A (en)
CA (1) CA1240048A (en)
FR (1) FR2575550B1 (en)
GB (1) GB2169572B (en)
IT (1) IT1188221B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH671555A5 (en) * 1986-09-10 1989-09-15 Zermatt Air Ag
JPH064439B2 (en) * 1987-09-01 1994-01-19 防衛庁技術研究本部長 Aircraft center of gravity measuring device
US5229956A (en) * 1991-03-06 1993-07-20 United Technologies Corporation Helicopter weight measurement
FR2866109B1 (en) * 2004-02-05 2006-04-07 Airbus France METHOD AND DEVICE FOR VERIFYING A TEMPERATURE VALUE AT AN ALTITUDE OF DESTINATION OF AN AIRCRAFT
EP1989107A4 (en) * 2006-02-23 2012-10-17 Sikorsky Aircraft Corp Radio frequency emitting hook system for a rotary-wing aircraft external load handling
FR2936491B1 (en) 2008-09-26 2010-10-08 Eurocopter France METHOD FOR LARGING AN EXTERNAL LOAD CARRIED BY AN AIRCRAFT AND ASSOCIATED DEVICE
FR2953493B1 (en) 2009-12-08 2012-01-27 Eurocopter France AIRCRAFT PROVIDED WITH A STEERING ASSISTING DEVICE WHEN IT FEATURES AN EXTERNAL LOAD WITH A SLING, AND A METHOD USED THEREBY
FR2977565B1 (en) 2011-07-07 2013-07-12 Eurocopter France DEVICE FOR FIXING AND CONTROLLING THE INCLINATION OF A SLING, AND AIRCRAFT
JP5832352B2 (en) * 2012-03-29 2015-12-16 三菱重工業株式会社 Vertical take-off and landing aircraft torque estimation device, vertical take-off and landing aircraft, vertical take-off and landing aircraft torque estimation program, and vertical take-off and landing aircraft torque estimation method
JP5960019B2 (en) * 2012-10-02 2016-08-02 三菱重工業株式会社 Flight management support device, flight management support system, flight management support method, and display device
WO2016007796A1 (en) * 2014-07-10 2016-01-14 Breeze-Eastern Corporation Helicopter hoist systems, devices, and methodologies
GB2533584A (en) * 2014-12-22 2016-06-29 Airbus Operations Ltd Aircraft fuel tank inerting arrangement, method of inerting one or more aircraft fuel tanks, aircraft and software product
FR3142461A1 (en) 2022-11-30 2024-05-31 Airbus Helicopters method of setting the mass of a load to be transported by an aircraft

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1416344A (en) * 1964-02-04 1965-11-05 United Aircraft Corp Remaining power indicator
NL7905278A (en) * 1979-07-06 1981-01-08 Philips Nv APPARATUS FOR RECORDING AND READING SIGNALS IN TRACKS ON A MAGNETIC TAPE.

Also Published As

Publication number Publication date
JPS61211199A (en) 1986-09-19
GB8531319D0 (en) 1986-01-29
FR2575550B1 (en) 1989-12-15
GB2169572B (en) 1988-02-10
CA1240048A (en) 1988-08-02
IT1188221B (en) 1988-01-07
GB2169572A (en) 1986-07-16
FR2575550A1 (en) 1986-07-04

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