CA1166277A - Detecteur de degonflement partiel d'un pneu d'aeronef - Google Patents

Detecteur de degonflement partiel d'un pneu d'aeronef

Info

Publication number: CA1166277A
Authority: CA; Canada
Prior art keywords: beam member; bogie beam; inclinometers; pair; aircraft
Prior art date: 1979-12-12
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

CA000418064A

Other languages

English (en)

Inventor

Charles D. Bateman

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.)

Sundstrand Data Control Inc

Original Assignee

Sundstrand Data Control Inc

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.)

1979-12-12

Filing date

1982-12-17

Publication date

1984-04-24

1979-12-12 Priority claimed from US06/102,776 external-priority patent/US4312042A/en

1982-12-17 Application filed by Sundstrand Data Control Inc filed Critical Sundstrand Data Control Inc

1982-12-17 Priority to CA000418064A priority Critical patent/CA1166277A/fr

1984-04-24 Application granted granted Critical

1984-04-24 Publication of CA1166277A publication Critical patent/CA1166277A/fr

Status Expired legal-status Critical Current

Links

238000001514 detection method Methods 0.000 title claims abstract description 8
230000005484 gravity Effects 0.000 claims description 9
239000000446 fuel Substances 0.000 description 11
238000005452 bending Methods 0.000 description 8
238000009826 distribution Methods 0.000 description 7
238000005259 measurement Methods 0.000 description 5
238000006073 displacement reaction Methods 0.000 description 4
239000002828 fuel tank Substances 0.000 description 4
230000001133 acceleration Effects 0.000 description 3
230000000694 effects Effects 0.000 description 3
239000003990 capacitor Substances 0.000 description 2
238000010586 diagram Methods 0.000 description 2
231100000817 safety factor Toxicity 0.000 description 2
230000035939 shock Effects 0.000 description 2
RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
230000000712 assembly Effects 0.000 description 1
238000000429 assembly Methods 0.000 description 1
230000000295 complement effect Effects 0.000 description 1
230000010006 flight Effects 0.000 description 1
230000007774 longterm Effects 0.000 description 1
238000004519 manufacturing process Methods 0.000 description 1
239000000463 material Substances 0.000 description 1
238000000034 method Methods 0.000 description 1
-1 passengers Substances 0.000 description 1
238000011179 visual inspection Methods 0.000 description 1
238000005303 weighing Methods 0.000 description 1

Landscapes

Testing Of Balance (AREA)

CA000418064A 1979-12-12 1982-12-17 Detecteur de degonflement partiel d'un pneu d'aeronef Expired CA1166277A (fr)

Priority Applications (1)

Application Number	Priority Date	Filing Date	Title
CA000418064A CA1166277A (fr)	1979-12-12	1982-12-17	Detecteur de degonflement partiel d'un pneu d'aeronef

Applications Claiming Priority (4)

Application Number	Priority Date	Filing Date	Title
US102,776		1979-12-12
US06/102,776 US4312042A (en)	1979-12-12	1979-12-12	Weight, balance, and tire pressure detection systems
CA000365404A CA1159852A (fr)	1979-12-12	1980-11-25	Systeme detecteur de masse et d'equilibre
CA000418064A CA1166277A (fr)	1979-12-12	1982-12-17	Detecteur de degonflement partiel d'un pneu d'aeronef

Publications (1)

Publication Number	Publication Date
CA1166277A true CA1166277A (fr)	1984-04-24

Family

ID=27166900

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
CA000418064A Expired CA1166277A (fr)	1979-12-12	1982-12-17	Detecteur de degonflement partiel d'un pneu d'aeronef

Country Status (1)

Country	Link
CA (1)	CA1166277A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CN109153443A (zh) *	2016-04-19	2019-01-04	株式会社普利司通	航空器用轮胎的管理方法以及航空器用轮胎的管理装置
CN110618670A (zh) *	2018-06-20	2019-12-27	里昂纳多有限公司	用于诊断结构的方法和系统及相关处理程序或程序组

1982
- 1982-12-17 CA CA000418064A patent/CA1166277A/fr not_active Expired

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CN109153443A (zh) *	2016-04-19	2019-01-04	株式会社普利司通	航空器用轮胎的管理方法以及航空器用轮胎的管理装置
CN110618670A (zh) *	2018-06-20	2019-12-27	里昂纳多有限公司	用于诊断结构的方法和系统及相关处理程序或程序组

Similar Documents

Publication	Publication Date	Title
CA1159852A (fr)	1984-01-03	Systeme detecteur de masse et d'equilibre
CA1321381C (fr)	1993-08-17	Transducteur de charge pour train d'atterrissage
EP2772732B1 (fr)	2020-02-19	Dispositif et procédé de mesure de poids total et de centre de gravité d'un aéronef
US8340892B2 (en)	2012-12-25	Onboard aircraft weight and balance system
CN100476374C (zh)	2009-04-08	用于测量飞机的质量和重心位置的随机携带装置
CA1206263A (fr)	1986-06-17	Systeme pour peser les helicopteres
US4507742A (en)	1985-03-26	Aircraft weight and balance system with automatic loading error correction
US20010054311A1 (en)	2001-12-27	Method and apparatus for determining air flow and pressure data of an aircraft or aerodynamic vehicle
US6415242B1 (en)	2002-07-02	System for weighing fixed wing and rotary wing aircraft by the measurement of cross-axis forces
US5590853A (en)	1997-01-07	Aircraft control system
GB2144225A (en)	1985-02-27	Transducer memory circuit
NZ204819A (en)	1987-02-20	Detecting underinflated tyre:monitoring frequency response of structural member
US4506328A (en)	1985-03-19	Static low tire pressure detection system for aircraft
US3488997A (en)	1970-01-13	Weight and center of gravity indication system
US5239137A (en)	1993-08-24	Method for calibrating sensors arranged in pairs on loaded structural parts
CA1166276A (fr)	1984-04-24	Systeme de mesure des contraintes imposees a un aeronef
US7395705B2 (en)	2008-07-08	System for measuring an airflow angle at the wingtip of an aircraft
VETSCH et al.	1988	Design of a certifiable primary on-board aircraft weight and balancesystem
Scheurell et al.	1968	Proposed SST Weight and Balance System
Cooney et al.	1951	Time histories of the aerodynamic loads on the vertical and horizontal tail surfaces of a jet-powered bomber airplane during sideslip maneuvers at approximately 20,000 feet
Krupovage	1978	Three dimensional transonic model testing on a rocket sled track
Marcy	1958	High-speed Landing Loads Measured on the Douglas X-3 Research Airplane
Hart et al.	1968	Pan American Operational Experience with STAN

Legal Events

Date	Code	Title	Description
2001-04-24	MKEX	Expiry