GB8531319D0 - Helicopter weight & torque advisory system - Google Patents

Helicopter weight & torque advisory system

Info

Publication number
GB8531319D0
GB8531319D0 GB858531319A GB8531319A GB8531319D0 GB 8531319 D0 GB8531319 D0 GB 8531319D0 GB 858531319 A GB858531319 A GB 858531319A GB 8531319 A GB8531319 A GB 8531319A GB 8531319 D0 GB8531319 D0 GB 8531319D0
Authority
GB
United Kingdom
Prior art keywords
advisory system
helicopter weight
torque
torque advisory
helicopter
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.)
Granted
Application number
GB858531319A
Other versions
GB2169572B (en
GB2169572A (en
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.)
Boeing Co
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 GB8531319D0 publication Critical patent/GB8531319D0/en
Publication of GB2169572A publication Critical patent/GB2169572A/en
Application granted granted Critical
Publication of GB2169572B publication Critical patent/GB2169572B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/006—Safety devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND 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
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Cosmetics (AREA)
  • Toys (AREA)
  • Jib Cranes (AREA)
  • Component Parts Of Construction Machinery (AREA)
GB08531319A 1985-01-03 1985-12-19 A helicopter weight and torque advisory system Expired GB2169572B (en)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
GB8531319D0 true GB8531319D0 (en) 1986-01-29
GB2169572A GB2169572A (en) 1986-07-16
GB2169572B GB2169572B (en) 1988-02-10

Family

ID=24764804

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08531319A Expired GB2169572B (en) 1985-01-03 1985-12-19 A helicopter weight and torque advisory system

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
CA1240048A (en) 1988-08-02
GB2169572B (en) 1988-02-10
GB2169572A (en) 1986-07-16
IT8619008A0 (en) 1986-01-03
JPS61211199A (en) 1986-09-19
IT1188221B (en) 1988-01-07
FR2575550A1 (en) 1986-07-04
FR2575550B1 (en) 1989-12-15

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19921219