CA2731018C - Capteur de desaccouplage pour bec d'aeronef - Google Patents

Capteur de desaccouplage pour bec d'aeronef Download PDF

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Publication number
CA2731018C
CA2731018C CA2731018A CA2731018A CA2731018C CA 2731018 C CA2731018 C CA 2731018C CA 2731018 A CA2731018 A CA 2731018A CA 2731018 A CA2731018 A CA 2731018A CA 2731018 C CA2731018 C CA 2731018C
Authority
CA
Canada
Prior art keywords
fuse
arms
disconnect
condition
slat
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
CA2731018A
Other languages
English (en)
Other versions
CA2731018A1 (fr
Inventor
Timothy Michael Mayer
Paul F. Hastings
Dale W. Massolle, Jr.
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.)
Hamilton Sundstrand Corp
Original Assignee
Hamilton Sundstrand 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 Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Publication of CA2731018A1 publication Critical patent/CA2731018A1/fr
Application granted granted Critical
Publication of CA2731018C publication Critical patent/CA2731018C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Fuses (AREA)
  • Details Of Connecting Devices For Male And Female Coupling (AREA)

Abstract

Un capteur de désaccouplage de bec de bord d'attaque comporte un premier et un deuxième bras supportés par une base. Au moins un des bras peut pivoter relativement à la base à un pivot entre les états connecté et déconnecté. Un lien mécanique comprend une première et une deuxième parties respectivement fixées au premier et au deuxième bras. Le lien relie les bras et comprend une zone affaiblie offrant une connexion frangible dans l'état connecté, et est configuré pour se rompre à la connexion frangible à l'état déconnecté. Un fusible comprend une première et une deuxième parties installées de manière fonctionnelle au premier et au deuxième bras. Le fusible est intercalé entre les bras et offre une continuité dans l'état connecté, et la continuité est rompue entre la première et la deuxième parties dans l'état déconnecté. Le lien mécanique et le fusible peuvent être le même et une connexion électrique est fournie de chaque côté du fusible. L'arrangement de lien mécanique et de fusible réalise un capteur fiable et efficace de désaccouplage de bec de sécurité.
CA2731018A 2010-03-24 2011-02-04 Capteur de desaccouplage pour bec d'aeronef Active CA2731018C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US31700810P 2010-03-24 2010-03-24
US71/317,008 2010-03-24
US61/317,008 2010-03-24

Publications (2)

Publication Number Publication Date
CA2731018A1 CA2731018A1 (fr) 2011-09-24
CA2731018C true CA2731018C (fr) 2015-01-27

Family

ID=44659911

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2731018A Active CA2731018C (fr) 2010-03-24 2011-02-04 Capteur de desaccouplage pour bec d'aeronef

Country Status (4)

Country Link
JP (1) JP2011201530A (fr)
CN (1) CN102198863B (fr)
BR (1) BRPI1101321B8 (fr)
CA (1) CA2731018C (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8820174B2 (en) * 2012-11-21 2014-09-02 Hamilton Sundstrand Corporation Dual threshold sensor for detecting relative movement
RU2745354C1 (ru) * 2020-09-11 2021-03-24 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Разделяемый аэродинамический руль высокоскоростного летательного аппарата

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4608548A (en) * 1985-01-04 1986-08-26 Littelfuse, Inc. Miniature fuse
JP3068262B2 (ja) * 1991-07-22 2000-07-24 高砂工業株式会社 土練済み生製品切断用の切断機における切断線の断線検知装置
JP2001101468A (ja) * 1999-09-27 2001-04-13 Akira Tsukahara 災害発生時の救難信号発生装置
US6483436B1 (en) * 2001-05-21 2002-11-19 Hamilton Sundstrand Corporation Method and apparatus for sensing skews and disconnects of adjacent movable components
JP2005147712A (ja) * 2003-11-11 2005-06-09 Akihisa Inoue 水素ガスセンサ
CN100517545C (zh) * 2005-07-14 2009-07-22 科伦电器股份有限公司 表面黏着型保险丝的制法
US7921729B2 (en) * 2008-03-10 2011-04-12 Hamilton Sundstrand Corporation Disconnect sensor
CN201315301Y (zh) * 2008-10-28 2009-09-23 南京萨特科技发展有限公司 一种高可靠性片式保险丝

Also Published As

Publication number Publication date
CN102198863A (zh) 2011-09-28
CA2731018A1 (fr) 2011-09-24
BRPI1101321B1 (pt) 2020-08-25
CN102198863B (zh) 2015-08-12
JP2011201530A (ja) 2011-10-13
BRPI1101321A2 (pt) 2012-10-16
BRPI1101321B8 (pt) 2020-09-08

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