BE899300A - Installation pour mesurer le poids d'un helicoptere. - Google Patents

Installation pour mesurer le poids d'un helicoptere.

Info

Publication number
BE899300A
BE899300A BE0/212673A BE212673A BE899300A BE 899300 A BE899300 A BE 899300A BE 0/212673 A BE0/212673 A BE 0/212673A BE 212673 A BE212673 A BE 212673A BE 899300 A BE899300 A BE 899300A
Authority
BE
Belgium
Prior art keywords
helicopter
weight
installation
measuring
detecting
Prior art date
Application number
BE0/212673A
Other languages
English (en)
Inventor
C D Bateman
Original Assignee
Sundstrand Data Control
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 Sundstrand Data Control filed Critical Sundstrand Data Control
Publication of BE899300A publication Critical patent/BE899300A/fr

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01GWEIGHING
    • G01G19/00Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
    • G01G19/02Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles
    • G01G19/07Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles for weighing aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Testing Of Balance (AREA)
  • Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)
  • Catching Or Destruction (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)

Abstract

L'installation pour mesurer le poids d'un hélicoptère, pour détecter le poids chargé d'un hélicoptère qui travaille à des conditions de flottement partiel ou complet pendant que les roues de l'hélicoptère sont en contact avec le sol, comporte des moyens pour détecter la charge sur le train d'atterrissage de l'hélicoptère et des moyens pour déterminer la force ascensionnelle produite par une aile tournante de l'hélicoptère. La force détectée sur le train d'atterrissage est additionnée à la force ascensionnelle calculée pour produire une indication de la charge totale de l'hélicoptère.
BE0/212673A 1983-04-01 1984-03-30 Installation pour mesurer le poids d'un helicoptere. BE899300A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/481,487 US4574360A (en) 1983-04-01 1983-04-01 Helicopter weight measuring system

Publications (1)

Publication Number Publication Date
BE899300A true BE899300A (fr) 1984-10-01

Family

ID=23912122

Family Applications (1)

Application Number Title Priority Date Filing Date
BE0/212673A BE899300A (fr) 1983-04-01 1984-03-30 Installation pour mesurer le poids d'un helicoptere.

Country Status (16)

Country Link
US (1) US4574360A (fr)
JP (1) JPS59184827A (fr)
AU (1) AU549275B2 (fr)
BE (1) BE899300A (fr)
CA (1) CA1206263A (fr)
CH (1) CH659130A5 (fr)
DE (1) DE3407051C2 (fr)
ES (1) ES8506524A1 (fr)
FR (2) FR2543678A1 (fr)
GB (1) GB2137153B (fr)
HK (1) HK94586A (fr)
IT (1) IT1177632B (fr)
NL (1) NL8401015A (fr)
NO (1) NO841011L (fr)
SE (1) SE452059B (fr)
ZA (1) ZA841646B (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4780838A (en) * 1985-01-03 1988-10-25 The Boeing Company Helicopter weight and torque advisory system
WO1988008391A1 (fr) * 1987-04-29 1988-11-03 Bell Helicopter Textron Inc. Transducteur de charge pour train d'atterrissage
US5045649A (en) * 1989-10-03 1991-09-03 Bell Helicopter Textron Inc. Self-adjusting slide assembly for weight on gear switch
US5229956A (en) * 1991-03-06 1993-07-20 United Technologies Corporation Helicopter weight measurement
DE4224578C1 (en) * 1992-07-22 1993-09-09 Hans-Heinrich O-3034 Magdeburg De Fahr Sensor for switching on and off of chronometer used in air sports e.g. hang gliding - using altering size of aerodynamic lift of carrying surface which works against weight of pilot for operating chronometer automatically at take off and landing.
US5352090A (en) * 1992-08-07 1994-10-04 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration System for determining aerodynamic imbalance
IL123512A0 (en) * 1998-03-02 1999-03-12 Security 7 Software Ltd Method and agent for the protection against hostile resource use access
US5987397A (en) * 1998-03-13 1999-11-16 The United States Of America As Represented By The Secretary Of The Navy Neural network system for estimation of helicopter gross weight and center of gravity location
US6353793B1 (en) * 1999-02-01 2002-03-05 Aero Modifications & Consulting, Llc System and apparatus for determining the center of gravity of an aircraft
US6419186B1 (en) * 2000-03-31 2002-07-16 Rosemount Aerospace Inc. Standoff mounting for air data sensing probes on a helicopter
CN100441479C (zh) * 2004-08-10 2008-12-10 贝尔直升机泰克斯特龙公司 起落架上重量确定方法、传感器以及传感器支架和飞机
US7984146B2 (en) * 2006-05-04 2011-07-19 Sikorsky Aircraft Corporation Aircraft health and usage monitoring system with comparative fleet statistics
US20090083050A1 (en) * 2007-09-25 2009-03-26 Eltman Joseph T Compilation and distribution of data for aircraft fleet management
US7983809B2 (en) * 2007-12-21 2011-07-19 Sikorsky Aircraft Corporation Aircraft integrated support system (ISS)
EP2450677B1 (fr) * 2010-11-09 2014-01-22 Eurocopter Deutschland GmbH Système de pesage d' hélicoptère et procédé de fonctionnement d'un tel système de pesage
WO2012138830A1 (fr) 2011-04-07 2012-10-11 Lord Corporation Commande de mouvement d'ailes rotatives d'aéronef et dispositif à fluide de commande de mouvement à instruments
US9139290B2 (en) 2013-09-10 2015-09-22 Sikorsky Aircraft Corporation Aircraft weight identification using filtered trim estimation
FR3036789B1 (fr) 2015-05-29 2017-05-26 Airbus Helicopters Procede d'estimation de la masse instantanee d'un aeronef a voilure tournante
US10099802B2 (en) 2017-02-14 2018-10-16 Honeywell International Inc. Methods and systems to detect and alert a dynamic rollover condition for an aircraft
FR3102856B1 (fr) * 2019-11-05 2021-10-01 Airbus Helicopters Procédé et dispositif d’estimation d’une vitesse air d’un giravion par analyse de son rotor.
FR3104137B1 (fr) * 2019-12-04 2022-04-08 Airbus Helicopters Procédé et système d’assistance au décollage d’un giravion
DE102020210349A1 (de) 2020-08-14 2022-02-17 Volkswagen Aktiengesellschaft Verfahren zum Betreiben eines vertikal startenden und landenden Luftfahrzeugs und vertikal startendes und landendes Luftfahrzeug
CN115014489B (zh) * 2022-05-18 2024-03-19 杭州沛澜航空科技有限公司 无人直升机飞行重量测量方法及装置
CN114858259B (zh) * 2022-05-26 2024-08-23 上海沃兰特航空技术有限责任公司 飞行器重量和重心测量方法及装置、电子设备和存储介质

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2402618A (en) * 1945-04-16 1946-06-25 Flatt Joseph Gross weight indicator for airplanes
GB685292A (en) * 1948-12-11 1952-12-31 Edward Noel Brailsford Apparatus for measuring the lift-coefficient of an aircraft
FR1169089A (fr) * 1955-12-29 1958-12-22 Sperry Rand Corp Système empêchant les avions de tomber en perte de vitesse
US3310976A (en) * 1963-10-17 1967-03-28 Bussell Bertram Aircraft weight and center of gravity apparatus
US3469644A (en) * 1968-02-29 1969-09-30 Boeing Co Weight indicating mechanism
US3590636A (en) * 1968-10-25 1971-07-06 Industrial Nucleonics Corp Method for determining aircraft lift capability using air density measurement
US3701279A (en) * 1971-02-08 1972-10-31 Electro Dev Corp Aircraft weight and center of gravity indicator system
US3754440A (en) * 1972-08-16 1973-08-28 Us Navy Helicopter lift margin determining system
CA989978A (en) * 1973-04-27 1976-05-25 Edelbert G. Plett Apparatus for determining the gross thrust of a jet engine
US4115755A (en) * 1976-06-11 1978-09-19 United Technologies Corporation Aerodynamic surface load sensing
US4110605A (en) * 1977-02-25 1978-08-29 Sperry Rand Corporation Weight and balance computer apparatus for aircraft
US4312042A (en) * 1979-12-12 1982-01-19 Sundstrand Data Control, Inc. Weight, balance, and tire pressure detection systems
US4463428A (en) * 1981-10-26 1984-07-31 The United States Of America As Represented By The Secretary Of The Navy Aircraft weight and center of gravity cockpit readout system
US4490802A (en) * 1981-12-21 1984-12-25 Sperry Corporation Takeoff weight computer apparatus for aircraft

Also Published As

Publication number Publication date
ES531133A0 (es) 1985-08-01
FR2543678A1 (fr) 1984-10-05
GB2137153A (en) 1984-10-03
US4574360A (en) 1986-03-04
GB2137153B (en) 1986-06-04
CA1206263A (fr) 1986-06-17
AU2609584A (en) 1984-10-04
NL8401015A (nl) 1984-11-01
CH659130A5 (fr) 1986-12-31
AU549275B2 (en) 1986-01-23
NO841011L (no) 1984-10-02
JPS59184827A (ja) 1984-10-20
IT8447961A0 (it) 1984-03-29
FR2550626A1 (fr) 1985-02-15
HK94586A (en) 1986-12-12
SE452059B (sv) 1987-11-09
DE3407051C2 (de) 1987-02-12
GB8405021D0 (en) 1984-04-04
ES8506524A1 (es) 1985-08-01
ZA841646B (en) 1984-11-28
IT8447961A1 (it) 1985-09-29
SE8401253D0 (sv) 1984-03-07
DE3407051A1 (de) 1984-10-11
IT1177632B (it) 1987-08-26
SE8401253L (sv) 1984-10-02

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: SUNDSTRAND DATA CONTROL INC.

Effective date: 19890331