FR2381998A1 - Appareillage de mesure du poids total en charge d'un aeronef - Google Patents

Appareillage de mesure du poids total en charge d'un aeronef

Info

Publication number
FR2381998A1
FR2381998A1 FR7805391A FR7805391A FR2381998A1 FR 2381998 A1 FR2381998 A1 FR 2381998A1 FR 7805391 A FR7805391 A FR 7805391A FR 7805391 A FR7805391 A FR 7805391A FR 2381998 A1 FR2381998 A1 FR 2381998A1
Authority
FR
France
Prior art keywords
aircraft
function
measurement
loaded weight
measuring equipment
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
FR7805391A
Other languages
English (en)
Other versions
FR2381998B1 (fr
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.)
Sperry Corp
Original Assignee
Sperry Rand Corp
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 Sperry Rand Corp filed Critical Sperry Rand Corp
Publication of FR2381998A1 publication Critical patent/FR2381998A1/fr
Application granted granted Critical
Publication of FR2381998B1 publication Critical patent/FR2381998B1/fr
Granted legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/12—Static balancing; Determining position of centre of gravity
    • G01M1/122—Determining position of centre of gravity
    • G01M1/125—Determining position of centre of gravity of aircraft
    • G01M1/127—Determining position of centre of gravity of aircraft during the flight
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01G—WEIGHING
    • G01G19/00—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups
    • G01G19/02—Weighing apparatus or methods adapted for special purposes not provided for in the preceding groups for weighing wheeled or rolling bodies, e.g. vehicles
    • G01G19/07—Weighing 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)
  • Testing Of Balance (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

Système de mesure du poids total en charge d'un avion. Un premier élément mesure la force propulsive des moteurs de l'avion en fonction d'une caractéristique de leur fonctionnement. Un second élément donne, en fonction de cette première mesure et des forces aérodynamiques qui s'exercent sur l'aéronef une seconde mesure fonction de l'angle d'attaque de la voilure. Un troisième élément donne en fonction de cette seconde mesure la mesure recherchée, à savoir celle du poids total de l'aéronef. Application aux systèmes de commande et aux instruments de bord des aéronefs.
FR7805391A 1977-02-25 1978-02-24 Appareillage de mesure du poids total en charge d'un aeronef Granted FR2381998A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/772,186 US4110605A (en) 1977-02-25 1977-02-25 Weight and balance computer apparatus for aircraft

Publications (2)

Publication Number Publication Date
FR2381998A1 true FR2381998A1 (fr) 1978-09-22
FR2381998B1 FR2381998B1 (fr) 1983-04-15

Family

ID=25094235

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7805391A Granted FR2381998A1 (fr) 1977-02-25 1978-02-24 Appareillage de mesure du poids total en charge d'un aeronef

Country Status (6)

Country Link
US (1) US4110605A (fr)
JP (1) JPS53107100A (fr)
DE (1) DE2808017A1 (fr)
FR (1) FR2381998A1 (fr)
GB (1) GB1595686A (fr)
IT (1) IT1155842B (fr)

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* Cited by examiner, † Cited by third party
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FR2513380A1 (fr) * 1981-09-23 1983-03-25 Sfena Dispositif giro-anemometrique avionable
FR2543678A1 (fr) * 1983-04-01 1984-10-05 Sundstrand Data Control Dispositif de mesure de poids et appareil de mesure de la poussee developpee par l'aile tournante d'un helicoptere
WO1988005162A1 (fr) * 1987-01-08 1988-07-14 Aerospatiale Societe Nationale Industrielle Procede et dispositif pour determiner le centre de gravite d'un aeronef
WO1988005163A1 (fr) * 1987-01-08 1988-07-14 Aerospatiale Societe Nationale Industrielle Procede et dispositif pour determiner le centre de gravite d'un aeronef
EP0441007A2 (fr) * 1990-01-26 1991-08-14 The Boeing Company Méthode d'estimation en temps réel du centre de gravité d'un avion

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US4641268A (en) * 1983-01-27 1987-02-03 Sperry Corporation Cruise airspeed control for aircraft
IL68737A0 (en) * 1983-05-20 1984-06-29 Israel Aircraft Ind Ltd Excessive ground-closure rate alarm system for aircraft
US4590475A (en) * 1983-10-24 1986-05-20 The United States Of America As Represented By The Secretary Of The Army Stall avoidance system for aircraft
US4622639A (en) * 1983-12-16 1986-11-11 The Boeing Company Aircraft center of gravity and fuel level advisory system
US4780838A (en) * 1985-01-03 1988-10-25 The Boeing Company Helicopter weight and torque advisory system
US4728951A (en) * 1985-10-16 1988-03-01 Honeywell Inc. Vertical windshear detection for aircraft
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US5020740A (en) * 1990-03-28 1991-06-04 Thomas Hugh O Pitch control trimming system for canard design aircraft
US5136513A (en) * 1990-06-11 1992-08-04 Ford Motor Company Vehicle inertia and center of gravity estimator
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
DE69312687T2 (de) * 1992-02-07 1998-02-26 C. Kirk Arlington Tex. Nance Anzeiger von gewicht und schwerpunkt von flugzeugen
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US5796612A (en) * 1992-11-18 1998-08-18 Aers/Midwest, Inc. Method for flight parameter monitoring and control
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US5391934A (en) * 1993-06-08 1995-02-21 Honeywell Inc. Load sensor driver apparatus
DE4423938B4 (de) * 1994-07-07 2007-08-30 Airbus Deutschland Gmbh Anordnung zur elektronischen Messung der Belastung eines Fahrwerks
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US5571953A (en) * 1995-05-15 1996-11-05 The Boeing Company Method and apparatus for the linear real time estimation of an aircraft center of gravity
FR2738808B1 (fr) * 1995-09-14 1997-10-24 Cim Manutique Sa Equilibrage et/ou positionnement de toute charge de poids variable ou non, en mouvement non uniforme
US6128951A (en) * 1997-04-15 2000-10-10 Trinity Airweighs, L.L.C. Aircraft weight and center of gravity indicator
US6032090A (en) * 1997-05-06 2000-02-29 General Electrodynamics Corporation System and method for on-board determination of aircraft weight and load-related characteristics
GB2333672B (en) * 1998-01-27 2003-06-25 Stasys Ltd Analysing tactical data link messages
US6304194B1 (en) * 1998-12-11 2001-10-16 Continuum Dynamics, Inc. Aircraft icing detection system
US6353793B1 (en) * 1999-02-01 2002-03-05 Aero Modifications & Consulting, Llc System and apparatus for determining the center of gravity of an aircraft
US6564142B2 (en) 1999-02-01 2003-05-13 Aero Modifications & Consulting, L.L.C. System and apparatus for determining the center of gravity of an aircraft
DE10056923B4 (de) * 2000-11-16 2004-02-26 Eads Deutschland Gmbh Verfahren zur Ermittlung von massen-bezogenen Daten eines geregelten Flugzeugs
US6782346B2 (en) * 2001-05-07 2004-08-24 The Boeing Company Aircraft synthesis and systems evaluation method for determining and evaluating electrical power generation and distribution system components
FR2859787B1 (fr) * 2003-09-16 2006-01-20 Thales Sa Dispositif et procede de determination de la temperature totale pour aeronef
US7954766B2 (en) * 2005-06-24 2011-06-07 Sikorsky Aircraft Corporation System and method for improved rotary-wing aircraft performance with interior/external loads
US7281418B2 (en) * 2005-07-12 2007-10-16 Technology Patents, Llc System and method of measuring weight of passengers and luggage, and weight distribution of aircraft
FR2894046B1 (fr) * 2005-11-28 2008-02-15 Airbus France Sas Procede de detection d'une erreur d'entree d'un des parametres de decollage dans un systeme de management de vol
FR2905778B1 (fr) * 2006-09-12 2008-12-26 Thales Sa Procede de verification de pertinence d'une valeur de masse d'un aeronef
EP2117926B1 (fr) * 2007-01-10 2018-12-26 Sikorsky Aircraft Corporation Dispositif de mesure du taux de givrage à aspiration virtuelle
FR2916276B1 (fr) * 2007-05-14 2009-08-28 Airbus France Sas Dispositif et procede d'estimation d'un angle d'incidence d'un aeronef
US8761970B2 (en) * 2008-10-21 2014-06-24 The Boeing Company Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method
US8060296B2 (en) * 2008-11-12 2011-11-15 Honeywell International Inc. Low cost aircraft center of gravity monitoring systems and methods
US8583354B2 (en) 2011-04-06 2013-11-12 Robert Bosch Gmbh Continuous computation of center of gravity of a vehicle
US8998132B2 (en) 2011-11-30 2015-04-07 Lockheed Martin Corporation Aerodynamic wing load distribution control
DE102011056777B4 (de) * 2011-12-21 2013-11-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Schwerpunktermittlung
US9567097B2 (en) 2012-02-03 2017-02-14 Rosemount Aerospace Inc. System and method for real-time aircraft performance monitoring
FR2988836B1 (fr) * 2012-03-28 2014-04-25 Dassault Aviat Procede de determination d'une masse estimee d'un aeronef et systeme correspondant
GB2516916B (en) * 2013-08-06 2016-09-14 Lacsop Ltd Method and apparatus for determining the mass of a body
US9284043B2 (en) * 2013-11-21 2016-03-15 Aai Corporation Evaluating aileron deflection while an unmanned aerial vehicle is in flight
US9361486B2 (en) 2013-11-25 2016-06-07 AeroData, Inc. Determining a profile for an aircraft prior to flight using a fuel vector and uncertainty bands
US9703293B2 (en) * 2015-08-31 2017-07-11 The Boeing Company Aircraft stall protection system
US10089634B2 (en) 2015-10-27 2018-10-02 C Kirk Nance Method to recover non-recognized errors in aircraft weight determinations to increase weight and center of gravity limitations for regulated aircraft
EP3336485B1 (fr) 2016-12-15 2020-09-23 Safran Landing Systems UK Limited Composant aéronautique comprenant un capteur de braquage
US10669015B2 (en) * 2017-06-07 2020-06-02 The Boeing Company Automatic adjustment of center of mass of a vehicle
US10768201B2 (en) * 2017-06-12 2020-09-08 The Boeing Company System for estimating airspeed of an aircraft based on a drag model
US10737768B2 (en) * 2017-08-10 2020-08-11 Embraer S.A. Enhanced takeoff trim indication
GB2576787B (en) * 2018-09-03 2022-05-11 Ge Aviat Systems Ltd Measuring weight and balance and optimizing center of gravity
CN109855712B (zh) * 2019-01-09 2023-09-01 山东太古飞机工程有限公司 一种用于飞机称重工艺中的定距定中辅助工装
US11001392B1 (en) 2019-11-10 2021-05-11 John Timothy Kern System of hardware and software for determining the weight and center of gravity location of an airplane or other vehicles, like a forklift, truck, and maritime vessel
US11341786B1 (en) * 2020-11-13 2022-05-24 Samsara Inc. Dynamic delivery of vehicle event data
US11643102B1 (en) 2020-11-23 2023-05-09 Samsara Inc. Dash cam with artificial intelligence safety event detection
WO2023087080A1 (fr) * 2021-11-18 2023-05-25 Тогрул Иса КАРИМЛИ Procédé de bord dynamique et système (dispositif) de mesure automatique de masse et de centrage, de tangage, de lacet, de roulis et de décalage du centrage d'un aéronef au sol et dans l'espace
CN114896680B (zh) * 2022-03-18 2024-06-07 成都飞机工业（集团）有限责任公司 一种基于爬升试飞数据的稳定盘旋过载修正方法

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US3159738A (en) * 1960-05-20 1964-12-01 Smith & Sons Ltd S Aircraft ground run predictors
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US3584503A (en) * 1969-12-04 1971-06-15 Blh Electronics Aircraft weight and center of gravity determination system which includes alarm,self-checking,and fault override circuitry
FR2097395A5 (fr) * 1970-07-03 1972-03-03 Messier Fa
US3654443A (en) * 1969-11-03 1972-04-04 Sperry Rand Corp Angle-of-attack computer
US3691356A (en) * 1970-12-10 1972-09-12 Sperry Rand Corp Speed command and throttle control system for aircraft
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US3048329A (en) * 1958-03-17 1962-08-07 Honeywell Regulator Co Aircraft instruments
US3159738A (en) * 1960-05-20 1964-12-01 Smith & Sons Ltd S Aircraft ground run predictors
US3513300A (en) * 1967-08-23 1970-05-19 Jack Asher Elfenbein Aircraft weight and center of gravity computer
US3654443A (en) * 1969-11-03 1972-04-04 Sperry Rand Corp Angle-of-attack computer
US3584503A (en) * 1969-12-04 1971-06-15 Blh Electronics Aircraft weight and center of gravity determination system which includes alarm,self-checking,and fault override circuitry
FR2097395A5 (fr) * 1970-07-03 1972-03-03 Messier Fa
US3691356A (en) * 1970-12-10 1972-09-12 Sperry Rand Corp Speed command and throttle control system for aircraft
US3701279A (en) * 1971-02-08 1972-10-31 Electro Dev Corp Aircraft weight and center of gravity indicator system

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2513380A1 (fr) * 1981-09-23 1983-03-25 Sfena Dispositif giro-anemometrique avionable
FR2543678A1 (fr) * 1983-04-01 1984-10-05 Sundstrand Data Control Dispositif de mesure de poids et appareil de mesure de la poussee developpee par l'aile tournante d'un helicoptere
WO1988005162A1 (fr) * 1987-01-08 1988-07-14 Aerospatiale Societe Nationale Industrielle Procede et dispositif pour determiner le centre de gravite d'un aeronef
WO1988005163A1 (fr) * 1987-01-08 1988-07-14 Aerospatiale Societe Nationale Industrielle Procede et dispositif pour determiner le centre de gravite d'un aeronef
FR2609545A1 (fr) * 1987-01-08 1988-07-15 Aerospatiale Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable et application a la surveillance dudit centre de gravite au voisinage du foyer de l'aeronef
FR2609546A1 (fr) * 1987-01-08 1988-07-15 Aerospatiale Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable
EP0281429A1 (fr) * 1987-01-08 1988-09-07 AEROSPATIALE Société Nationale Industrielle Procédé et dispositif pour déterminer le centre de gravité d'un aéronef
EP0281428A1 (fr) * 1987-01-08 1988-09-07 AEROSPATIALE Société Nationale Industrielle Procédé et dispositif pour déterminer le centre de gravité d'un aéronef
US4937754A (en) * 1987-01-08 1990-06-26 Aerospatiale Societe Nationale Industrielle Process and system for determining the longitudinal position of the center of gravity of an aircraft provided with an adjustable horizontal stabilizer and application to the monitoring of said center of gravity near the focus of the aircraft
US4949269A (en) * 1987-01-08 1990-08-14 Societe Nationale Industrielle Et Aerospatiale Process and system for determining the longitudinal position of the center of gravity of an aircraft provided with an adjustable horizontal stabilizer
EP0441007A2 (fr) * 1990-01-26 1991-08-14 The Boeing Company Méthode d'estimation en temps réel du centre de gravité d'un avion
EP0441007A3 (en) * 1990-01-26 1992-08-26 The Boeing Company Method and apparatus for real time estimation of aircraft center of gravity

Also Published As

Publication number Publication date
FR2381998B1 (fr) 1983-04-15
DE2808017A1 (de) 1978-08-31
DE2808017C2 (fr) 1989-09-21
GB1595686A (en) 1981-08-12
IT7848189A0 (it) 1978-02-24
JPS53107100A (en) 1978-09-18
IT1155842B (it) 1987-01-28
US4110605A (en) 1978-08-29

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