FR3098592B1 - Monitoring of a pneumatic anti-icing circuit for an aircraft wing - Google Patents

Monitoring of a pneumatic anti-icing circuit for an aircraft wing Download PDF

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Publication number
FR3098592B1
FR3098592B1 FR1907896A FR1907896A FR3098592B1 FR 3098592 B1 FR3098592 B1 FR 3098592B1 FR 1907896 A FR1907896 A FR 1907896A FR 1907896 A FR1907896 A FR 1907896A FR 3098592 B1 FR3098592 B1 FR 3098592B1
Authority
FR
France
Prior art keywords
monitoring
aircraft wing
icing
pneumatic anti
icing circuit
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
FR1907896A
Other languages
French (fr)
Other versions
FR3098592A1 (en
Inventor
Marc Wetterwald
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1907896A priority Critical patent/FR3098592B1/en
Publication of FR3098592A1 publication Critical patent/FR3098592A1/en
Application granted granted Critical
Publication of FR3098592B1 publication Critical patent/FR3098592B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • G01M3/00—Investigating fluid-tightness of structures
    • G01M3/02—Investigating fluid-tightness of structures by using fluid or vacuum
    • G01M3/26—Investigating fluid-tightness of structures by using fluid or vacuum by measuring rate of loss or gain of fluid, e.g. by pressure-responsive devices, by flow detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0607—Environmental Control Systems providing hot air or liquid for deicing aircraft parts, e.g. aerodynamic surfaces or windows
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
    • B64D2013/0603—Environmental Control Systems
    • B64D2013/0618—Environmental Control Systems with arrangements for reducing or managing bleed air, using another air source, e.g. ram air
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/50—On board measures aiming to increase energy efficiency

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Examining Or Testing Airtightness (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

L’invention concerne un procédé et un dispositif de surveillance d’un circuit pneumatique (1) d’antigivrage pour une voilure (9) d’aéronef, ledit circuit pneumatique (1) comportant une vanne de contrôle (5a, 5b) destinée à réguler le flux d’air chaud d’antigivrage à destination de la voilure (9), ledit dispositif de surveillance (13) comportant un contrôleur (15) configuré pour détecter une fuite d’air chaud au niveau de la voilure (9) à partir de l’angle d’ouverture de la vanne de contrôle (5a, 5b). Figure pour l'abrégé: Fig. 1The invention relates to a method and a device for monitoring a pneumatic anti-icing circuit (1) for an aircraft wing (9), said pneumatic circuit (1) comprising a control valve (5a, 5b) intended for regulating the flow of hot anti-icing air to the canopy (9), said monitoring device (13) comprising a controller (15) configured to detect a hot air leak from the canopy (9) to from the opening angle of the control valve (5a, 5b). Figure for the abstract: Fig. 1

FR1907896A 2019-07-12 2019-07-12 Monitoring of a pneumatic anti-icing circuit for an aircraft wing Active FR3098592B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1907896A FR3098592B1 (en) 2019-07-12 2019-07-12 Monitoring of a pneumatic anti-icing circuit for an aircraft wing

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1907896 2019-07-12
FR1907896A FR3098592B1 (en) 2019-07-12 2019-07-12 Monitoring of a pneumatic anti-icing circuit for an aircraft wing

Publications (2)

Publication Number Publication Date
FR3098592A1 FR3098592A1 (en) 2021-01-15
FR3098592B1 true FR3098592B1 (en) 2021-09-17

Family

ID=68806907

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1907896A Active FR3098592B1 (en) 2019-07-12 2019-07-12 Monitoring of a pneumatic anti-icing circuit for an aircraft wing

Country Status (1)

Country Link
FR (1) FR3098592B1 (en)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008029469B3 (en) * 2008-06-20 2009-10-29 Airbus Deutschland Gmbh Aircraft e.g. airplane, pipe monitoring system for e.g. aircraft air conditioning system, has control device for emitting signal indicating deviation, if normal operation flow and/or pressure deviates from reference flow and pressure
FR2998049B1 (en) * 2012-11-09 2017-05-05 Snecma METHOD AND SYSTEM FOR ESTIMATING AIR FLOW TAKEN FROM A MOTOR

Also Published As

Publication number Publication date
FR3098592A1 (en) 2021-01-15

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