DE2149547C3 - Verfahren und Vorrichtung zur Be Stimmung des Schwerpunktes von mehreren Korpern und Anwendung auf Personentrans portmittel - Google Patents

Verfahren und Vorrichtung zur Be Stimmung des Schwerpunktes von mehreren Korpern und Anwendung auf Personentrans portmittel

Info

Publication number
DE2149547C3
DE2149547C3 DE2149547A DE2149547A DE2149547C3 DE 2149547 C3 DE2149547 C3 DE 2149547C3 DE 2149547 A DE2149547 A DE 2149547A DE 2149547 A DE2149547 A DE 2149547A DE 2149547 C3 DE2149547 C3 DE 2149547C3
Authority
DE
Germany
Prior art keywords
pulses
timer
group
gravity
center
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.)
Expired
Application number
DE2149547A
Other languages
German (de)
English (en)
Other versions
DE2149547A1 (de
DE2149547B2 (de
Inventor
Jacques Azum
Roger Claustre
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 Group SAS
Original Assignee
Airbus Group SAS
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 Group SAS filed Critical Airbus Group SAS
Publication of DE2149547A1 publication Critical patent/DE2149547A1/de
Publication of DE2149547B2 publication Critical patent/DE2149547B2/de
Application granted granted Critical
Publication of DE2149547C3 publication Critical patent/DE2149547C3/de
Expired 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Seats For Vehicles (AREA)
  • Air Bags (AREA)
DE2149547A 1970-10-22 1971-10-04 Verfahren und Vorrichtung zur Be Stimmung des Schwerpunktes von mehreren Korpern und Anwendung auf Personentrans portmittel Expired DE2149547C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7038138A FR2110576A5 (enExample) 1970-10-22 1970-10-22

Publications (3)

Publication Number Publication Date
DE2149547A1 DE2149547A1 (de) 1972-05-04
DE2149547B2 DE2149547B2 (de) 1973-02-22
DE2149547C3 true DE2149547C3 (de) 1973-09-13

Family

ID=9063118

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2149547A Expired DE2149547C3 (de) 1970-10-22 1971-10-04 Verfahren und Vorrichtung zur Be Stimmung des Schwerpunktes von mehreren Korpern und Anwendung auf Personentrans portmittel

Country Status (4)

Country Link
US (1) US3746844A (enExample)
DE (1) DE2149547C3 (enExample)
FR (1) FR2110576A5 (enExample)
GB (1) GB1370000A (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE369117B (enExample) * 1972-07-28 1974-08-05 Lastfoerdelningsinstr Kb I Mal
US4446524A (en) * 1978-01-18 1984-05-01 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Apparatus for loading and unloading an aircraft
DE2802003C2 (de) * 1978-01-18 1982-08-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung zum Be- und Entladen eines Flugzeuges
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
US4507742A (en) * 1982-07-30 1985-03-26 Sundstrand Data Control, Inc. Aircraft weight and balance system with automatic loading error correction
US4622639A (en) * 1983-12-16 1986-11-11 The Boeing Company Aircraft center of gravity and fuel level advisory system
US5232243A (en) * 1991-04-09 1993-08-03 Trw Vehicle Safety Systems Inc. Occupant sensing apparatus
US5521827A (en) * 1994-09-16 1996-05-28 General Electrodynamics Corporation On-board aircraft weighting and center of gravity determing apparatus and method
US5864295A (en) * 1996-03-21 1999-01-26 Trw Inc. Apparatus for sensing occupant weight in an actuatable restraint system
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
AU2002228600A1 (en) * 2000-11-08 2002-05-21 Toyota Motor Sales, U.S.A., Inc. Methods and apparatus for airspace navigation
WO2002038444A2 (en) * 2000-11-08 2002-05-16 Toyota Motor Sales, U.S.A., Inc. Methods and apparatus for automated flight preparation
US6725135B2 (en) * 2001-09-26 2004-04-20 Stability Dynamics Vehicle stability operator feedback system
WO2003062754A1 (en) * 2002-01-24 2003-07-31 Toyota Motor Sales, U.S.A., Inc. Apparatus and methods for providing a flight display in an aircraft
US7079976B2 (en) 2003-10-07 2006-07-18 The Johns Hopkins University Dense object detection system and method
DE102006026926C5 (de) * 2006-06-09 2010-05-20 Continental Automotive Gmbh Verfahren zum Erkennen einer Verklemmung eines Sitzes
US7693621B1 (en) 2006-06-27 2010-04-06 Toyota Motor Sales, U.S.A., Inc. Apparatus and methods for displaying arrival, approach, and departure information on a display device in an aircraft
US10151661B2 (en) 2015-09-14 2018-12-11 The Boeing Company System for monitoring the weight and center of gravity of a vehicle
US9738396B2 (en) 2015-09-14 2017-08-22 The Boeing Company Vehicle occupant sensor system and method
ES2678748B2 (es) * 2017-02-15 2019-02-18 Univ De Las Palmas De Gran Canaria Sistema electrónico para estimación de carga y centrado de aeronaves

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2559718A (en) * 1944-05-26 1951-07-10 Curtiss Wright Corp Weight and center of gravity indicator
US2520428A (en) * 1946-09-23 1950-08-29 Nilakantan Parameswar Center of gravity calculator
US2541429A (en) * 1949-03-26 1951-02-13 Northrop Aircraft Inc Aircraft balance indicator
GB1226214A (enExample) * 1968-03-21 1971-03-24

Also Published As

Publication number Publication date
DE2149547A1 (de) 1972-05-04
DE2149547B2 (de) 1973-02-22
GB1370000A (en) 1974-10-09
US3746844A (en) 1973-07-17
FR2110576A5 (enExample) 1972-06-02

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977
8339 Ceased/non-payment of the annual fee