BR0307841A - Válvula de controle de pressão de cabine de uma aeronave - Google Patents

Válvula de controle de pressão de cabine de uma aeronave

Info

Publication number
BR0307841A
BR0307841A BR0307841-8A BR0307841A BR0307841A BR 0307841 A BR0307841 A BR 0307841A BR 0307841 A BR0307841 A BR 0307841A BR 0307841 A BR0307841 A BR 0307841A
Authority
BR
Brazil
Prior art keywords
cabin pressure
pressure control
control valve
aircraft cabin
valve
Prior art date
Application number
BR0307841-8A
Other languages
English (en)
Inventor
Darrell W Horner
Andrew D Bunn
Joaquin P Rabon
Original Assignee
Honeywell Int 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.)
Filing date
Publication date
Application filed by Honeywell Int Inc filed Critical Honeywell Int Inc
Publication of BR0307841A publication Critical patent/BR0307841A/pt

Links

Classifications

    • 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
    • B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • B64D13/04—Automatic control of pressure
    • 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
    • B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • 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
    • Y02T50/40—Weight reduction
    • 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

Abstract

"VáLVULA DE CONTROLE DE PRESSãO DE CABINE DE UMA AERONAVE". Uma válvula integrada do sistema de controle de pressão de cabine que utiliza uma unidade eletrónica de controle de duplo-canal, redundante, para controle simultâneo da válvula e para fornecer sinais de alarme, indicação e de controle ao sistema de eletrónica aeronáutica de bordo de uma aeronave. Cada canal na unidade eletrónica de controle inclui uma instrumentação e circuito de controle que utiliza múltiplos sensores e sinais desiguais para avisos, indicações, e controles. Essa configuração reduz a probabilidade quanto a uma falha no modo usual que poderia resultar em uma pressuposta descompressão gradual sem evento de indicação.
BR0307841-8A 2002-02-21 2003-02-21 Válvula de controle de pressão de cabine de uma aeronave BR0307841A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/080,107 US6737988B2 (en) 2002-02-21 2002-02-21 Instrumentation and control circuit having multiple, dissimilar sources for supplying warnings, indications, and controls and an integrated cabin pressure control system valve incorporating the same
PCT/US2003/005369 WO2003072432A2 (en) 2002-02-21 2003-02-21 Instrumentation and control circuit having multiple, dissimilar sources for supplying warnings, indications and controls, and an integrated cabin pressure control system valve incorporating the same

Publications (1)

Publication Number Publication Date
BR0307841A true BR0307841A (pt) 2005-02-09

Family

ID=27733148

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0307841-8A BR0307841A (pt) 2002-02-21 2003-02-21 Válvula de controle de pressão de cabine de uma aeronave

Country Status (14)

Country Link
US (1) US6737988B2 (pt)
EP (1) EP1476355B1 (pt)
JP (1) JP2005518307A (pt)
CN (1) CN1646366A (pt)
AT (1) ATE328788T1 (pt)
AU (1) AU2003219849A1 (pt)
BR (1) BR0307841A (pt)
CA (1) CA2477025C (pt)
CZ (1) CZ2004954A3 (pt)
DE (1) DE60305882T2 (pt)
ES (1) ES2262989T3 (pt)
IL (1) IL163664A0 (pt)
RU (1) RU2004127929A (pt)
WO (1) WO2003072432A2 (pt)

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DE102004048217B4 (de) * 2004-09-30 2007-04-19 Eurocopter Deutschland Gmbh Luftfahrzeug mit Kabinen-Differenzdruck-Warnsystem
DE102005001055A1 (de) * 2005-01-07 2006-07-20 Voith Turbo Gmbh & Co. Kg Redundante elektrohydraulische Ventilanordnung
DE102005002544A1 (de) * 2005-01-19 2006-07-27 Airbus Deutschland Gmbh Druckunterschied-Warnsystem
FR2895536B1 (fr) * 2005-12-22 2008-03-14 Renault Sas Dispositif et procede de determination de la valeur d'une information binaire, delivree de maniere redondante, et representative d'un parametre d'un systeme
US7670214B2 (en) 2006-08-31 2010-03-02 Honeywell International Inc. Systems and methods for intelligent alerting for cabin altitude depressurization
US9108602B2 (en) * 2006-12-05 2015-08-18 The Boeing Company Parking brake control for an aircraft having an electric brake system
US9809313B2 (en) * 2007-01-22 2017-11-07 Honeywell International Inc. Cabin altitude alerting systems and methods
US8808072B2 (en) * 2007-03-22 2014-08-19 Honeywell International Inc. Cabin pressure control system dual valve control and monitoring architecture
US7686680B2 (en) * 2007-06-26 2010-03-30 Honeywell International Inc. Closed-loop cabin pressure control system test method with actual pressure feedback
WO2009111776A1 (en) * 2008-03-07 2009-09-11 Adams Rite Aerospace Rapid decompression detection system and method
US8016232B2 (en) * 2008-05-29 2011-09-13 Honeywell International Inc. Aircraft cabin pressure descent detection and control system and method
FR2941551B1 (fr) 2009-01-28 2011-06-03 Airbus France Circuit electronique de determination d'une donnee representative d'un parametre de l'air et systeme comprenant un tel circuit
US8328606B2 (en) * 2009-03-10 2012-12-11 Honeywell International Inc. Aneroid replacement
US9017156B2 (en) * 2009-10-30 2015-04-28 Mestek, Inc. Air control module
CN102306207B (zh) * 2011-06-16 2013-08-14 西北工业大学 立柱阵列式机身壁板装配定位方法及其装置
US8694181B2 (en) 2012-03-12 2014-04-08 Honeywell International Inc. Cabin pressure control system with multiple outflow valves and method of calibrating the outflow valve position feedback during flight
US9037920B2 (en) * 2012-09-28 2015-05-19 Honeywell International Inc. Method for performing condition based data acquisition in a hierarchically distributed condition based maintenance system
GB2514108B (en) * 2013-05-13 2015-06-24 Ge Aviat Systems Ltd Method for diagnosing a bleed air system fault
US9260182B2 (en) * 2013-10-30 2016-02-16 Westjet Airlines Ltd. Integrated communication and application system for aircraft
CN105571565A (zh) * 2014-10-11 2016-05-11 中国航空工业集团公司西安飞机设计研究所 一种快速的飞机座舱高度告警模块的设计方法
US10444103B2 (en) * 2014-11-11 2019-10-15 Ams International Ag Method and apparatus for calibrating pressure sensor integrated circuit devices
US20160272341A1 (en) * 2015-03-17 2016-09-22 Airbly Inc. Aircraft environmental monitoring and alerting device
CN105279304B (zh) * 2015-06-19 2019-02-12 电子科技大学 一种基于n-2-1定位的飞机蒙皮定位偏差分析方法
CN105109701B (zh) * 2015-08-19 2017-05-17 中国航空工业集团公司西安飞机设计研究所 一种货运飞机货舱高度告警方法
JP6706121B2 (ja) * 2016-03-30 2020-06-03 株式会社フジキン 圧力制御装置および圧力制御システム
CN105912823B (zh) * 2016-05-12 2018-11-20 电子科技大学 基于n-2-1定位的飞机蒙皮和长桁装配偏差分析方法
EP3323728B1 (en) 2016-11-21 2019-01-02 Airbus Operations GmbH System and method for determining the origin of an oil leakage in an air supply system
CN107738751B (zh) * 2017-09-25 2020-06-05 中国航空工业集团公司西安飞机设计研究所 一种座舱压力变化率显示方法
US10953991B2 (en) * 2017-10-05 2021-03-23 The Boeing Company Aircraft altitude warning and oxygen presentation
US10640230B2 (en) * 2018-04-04 2020-05-05 Jurgen R. Ihns Cockpit pressurization and oxygen warning system
US11591092B2 (en) 2019-03-22 2023-02-28 Honeywell International Inc. Dissimilar microcontrollers for outflow valve
US11603206B2 (en) 2019-03-22 2023-03-14 Honeywell International Inc. Cabin pressure control system with all-electric OFV, using dis-similar manual control that performs cabin altitude hold function
EP4010251A4 (en) * 2019-08-06 2023-08-30 Telles, Angel AIRCRAFT PRESSURE CABIN PRESSURE SENSOR (CPS) SYSTEM AND RELATED PROCEDURES
CN112991650B (zh) * 2019-12-16 2024-03-08 上海航空电器有限公司 灯光告警系统所属设备的集成化设计系统
CN112748751A (zh) * 2020-12-22 2021-05-04 中国航空工业集团公司沈阳飞机设计研究所 一种数字化飞机环境控制系统及方法
FR3136824A1 (fr) * 2022-06-17 2023-12-22 Liebherr-Aerospace Toulouse Sas Système de fluide d’aéronef comprenant une vanne électrique de régulation équipée d’un actionneur intégré

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Also Published As

Publication number Publication date
CA2477025A1 (en) 2003-09-04
ES2262989T3 (es) 2006-12-01
RU2004127929A (ru) 2005-04-27
CA2477025C (en) 2007-06-12
WO2003072432A3 (en) 2003-12-31
US20030157875A1 (en) 2003-08-21
ATE328788T1 (de) 2006-06-15
DE60305882T2 (de) 2006-11-30
JP2005518307A (ja) 2005-06-23
AU2003219849A1 (en) 2003-09-09
EP1476355B1 (en) 2006-06-07
US6737988B2 (en) 2004-05-18
CZ2004954A3 (cs) 2004-12-15
CN1646366A (zh) 2005-07-27
WO2003072432A2 (en) 2003-09-04
DE60305882D1 (de) 2006-07-20
AU2003219849A8 (en) 2003-09-09
EP1476355A2 (en) 2004-11-17
IL163664A0 (en) 2005-12-18

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 9A ANUIDADE(S).

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: NAO APRESENTADA A GUIA DE CUMPRIMENTO DE EXIGENCIA. REFERENTE A 9A ANUIDADE.