CA2665963C - Systeme embarque de centrage d'aeronef - Google Patents

Systeme embarque de centrage d'aeronef Download PDF

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Publication number
CA2665963C
CA2665963C CA2665963A CA2665963A CA2665963C CA 2665963 C CA2665963 C CA 2665963C CA 2665963 A CA2665963 A CA 2665963A CA 2665963 A CA2665963 A CA 2665963A CA 2665963 C CA2665963 C CA 2665963C
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CA
Canada
Prior art keywords
aircraft
value
pressure
load
landing gear
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.)
Active
Application number
CA2665963A
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English (en)
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CA2665963A1 (fr
Inventor
Michael A. Long
Geoffrey E. Gouette
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
Priority to CA2665963A priority Critical patent/CA2665963C/fr
Publication of CA2665963A1 publication Critical patent/CA2665963A1/fr
Application granted granted Critical
Publication of CA2665963C publication Critical patent/CA2665963C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • 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)
  • Testing Of Balance (AREA)

Abstract

Un système embarqué pour déterminer instantanément les données de masse et centrage dun aéronef de manière simple, fiable et précise, et nécessitant un étalonnage minimal. Le système comprend une mémoire pour stocker les données de frottement déterminées précédemment des jambes amortisseuses des trains datterrissage de laéronef, des capteurs pour détecter les pressions dans les jambes amortisseuses, les charges verticales exercées par les trains datterrissage sur laéronef et lassiette de laéronef par rapport à lhorizontale durant son chargement ou son déchargement, et un ordinateur pour calculer la charge verticale dans chacun des trains d'atterrissage à partir des données de frottement d'étalonnage stockées et les pressions des jambes amortisseuses, les charges verticales des trains d'atterrissage et l'assiette de l'aéronef détectée durant le chargement ou le déchargement. Lordinateur calcule alors le poids brut de laéronef et lemplacement de son centre de gravité au moyen des charges verticales calculées dans les trains datterrissage.
CA2665963A 2009-05-13 2009-05-13 Systeme embarque de centrage d'aeronef Active CA2665963C (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA2665963A CA2665963C (fr) 2009-05-13 2009-05-13 Systeme embarque de centrage d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA2665963A CA2665963C (fr) 2009-05-13 2009-05-13 Systeme embarque de centrage d'aeronef

Publications (2)

Publication Number Publication Date
CA2665963A1 CA2665963A1 (fr) 2010-11-13
CA2665963C true CA2665963C (fr) 2016-04-05

Family

ID=43070427

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2665963A Active CA2665963C (fr) 2009-05-13 2009-05-13 Systeme embarque de centrage d'aeronef

Country Status (1)

Country Link
CA (1) CA2665963C (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2480124B8 (en) * 2011-03-17 2013-09-25 Messier Dowty Ltd Method and system for determining friction coefficient u for an aircraft landing event.
EP3069994B1 (fr) 2015-03-19 2017-11-08 Safran Landing Systems UK Limited Amortisseur de choc
CN107719695B (zh) * 2017-09-08 2023-10-20 中国飞行试验研究院 大型水陆两栖飞机水面纵摇试边界的试飞方法
CN111323168B (zh) * 2020-04-16 2021-10-01 一汽红塔云南汽车制造有限公司 一种汽车质心高度的测量计算方法
EP4245667A1 (fr) 2022-03-16 2023-09-20 Fundación Tekniker Procédé, système et produit programme informatique permettant d'obtenir la position du centre de gravité d'un aéronef
GB2617315A (en) 2022-03-28 2023-10-11 Airbus Operations Ltd Determining a load condition of an aircraft
CN115183983B (zh) * 2022-09-13 2022-11-15 中国航空工业集团公司沈阳空气动力研究所 一种舵面铰链力矩天平验证加载装置

Also Published As

Publication number Publication date
CA2665963A1 (fr) 2010-11-13

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