FR3070375B1 - Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede - Google Patents

Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede Download PDF

Info

Publication number
FR3070375B1
FR3070375B1 FR1758036A FR1758036A FR3070375B1 FR 3070375 B1 FR3070375 B1 FR 3070375B1 FR 1758036 A FR1758036 A FR 1758036A FR 1758036 A FR1758036 A FR 1758036A FR 3070375 B1 FR3070375 B1 FR 3070375B1
Authority
FR
France
Prior art keywords
conduit
fuel
filling
aircraft
tank
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
FR1758036A
Other languages
English (en)
Other versions
FR3070375A1 (fr
Inventor
Sylvain Rossi
Pierre-Yves Loubet
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.)
Safran Aerosystems SAS
Original Assignee
Zodiac Aerotechnics 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
Priority to FR1758036A priority Critical patent/FR3070375B1/fr
Application filed by Zodiac Aerotechnics SAS filed Critical Zodiac Aerotechnics SAS
Priority to RU2020106553A priority patent/RU2739369C9/ru
Priority to EP18753221.3A priority patent/EP3658461A1/fr
Priority to CA3071487A priority patent/CA3071487A1/fr
Priority to PCT/FR2018/051834 priority patent/WO2019043306A1/fr
Priority to JP2020512601A priority patent/JP2020531364A/ja
Priority to BR112020002921-1A priority patent/BR112020002921A2/pt
Priority to US16/641,658 priority patent/US20200356116A1/en
Publication of FR3070375A1 publication Critical patent/FR3070375A1/fr
Application granted granted Critical
Publication of FR3070375B1 publication Critical patent/FR3070375B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D7/00—Control of flow
    • G05D7/01—Control of flow without auxiliary power
    • G05D7/0126—Control of flow without auxiliary power the sensing element being a piston or plunger associated with one or more springs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/28—Liquid-handling installations specially adapted for fuelling stationary aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K1/00—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
    • F16K1/16—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members
    • F16K1/18—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps
    • F16K1/22—Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps with axis of rotation crossing the valve member, e.g. butterfly valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K3/00—Gate valves or sliding valves, i.e. cut-off apparatus with closing members having a sliding movement along the seat for opening and closing
    • F16K3/02—Gate valves or sliding valves, i.e. cut-off apparatus with closing members having a sliding movement along the seat for opening and closing with flat sealing faces; Packings therefor
    • F16K3/03—Gate valves or sliding valves, i.e. cut-off apparatus with closing members having a sliding movement along the seat for opening and closing with flat sealing faces; Packings therefor with a closure member in the form of an iris-diaphragm

Abstract

Procédé de circulation de carburant dans une conduite (2) de remplissage d'un réservoir d'un aéronef. Selon l'invention il consiste à faire varier automatiquement et mécaniquement la section de passage du carburant jusqu'à ce que le carburant atteigne une vitesse seuil maximale. Vanne (1) connectée à une conduite (2) de remplissage d'un réservoir de carburant d'un aéronef pour la mise en œuvre dudit procédé. Selon l'invention elle comprend un dispositif de restriction (7) de la section de passage du carburant, apte, lorsque du carburant circule dans la conduite (2), à faire varier automatiquement la section de passage du carburant jusqu'à ce que la vitesse du carburant atteigne une valeur seuil maximale.
FR1758036A 2017-08-31 2017-08-31 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede Active FR3070375B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1758036A FR3070375B1 (fr) 2017-08-31 2017-08-31 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede
EP18753221.3A EP3658461A1 (fr) 2017-08-31 2018-07-18 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en oeuvre dudit procede
CA3071487A CA3071487A1 (fr) 2017-08-31 2018-07-18 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en .uvre dudit procede
PCT/FR2018/051834 WO2019043306A1 (fr) 2017-08-31 2018-07-18 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede
RU2020106553A RU2739369C9 (ru) 2017-08-31 2018-07-18 Способ подачи топлива в заправочную трубу бака летательного аппарата и клапан, соединенный с трубой для осуществления указанного способа
JP2020512601A JP2020531364A (ja) 2017-08-31 2018-07-18 航空機のタンクの充填管路中の燃料を循環するための方法および当該方法を実施するため管路に接続される弁
BR112020002921-1A BR112020002921A2 (pt) 2017-08-31 2018-07-18 método para fluxo de combustível em um encanamento de abastecimento, e, válvula para um tanque de combustível de aeronave
US16/641,658 US20200356116A1 (en) 2017-08-31 2018-07-18 Method for the circulation of fuel in a filling line of a tank of an aircraft, and valve connected to a line for implementing said method

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1758036A FR3070375B1 (fr) 2017-08-31 2017-08-31 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede
FR1758036 2017-08-31

Publications (2)

Publication Number Publication Date
FR3070375A1 FR3070375A1 (fr) 2019-03-01
FR3070375B1 true FR3070375B1 (fr) 2019-12-13

Family

ID=60081045

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1758036A Active FR3070375B1 (fr) 2017-08-31 2017-08-31 Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede

Country Status (8)

Country Link
US (1) US20200356116A1 (fr)
EP (1) EP3658461A1 (fr)
JP (1) JP2020531364A (fr)
BR (1) BR112020002921A2 (fr)
CA (1) CA3071487A1 (fr)
FR (1) FR3070375B1 (fr)
RU (1) RU2739369C9 (fr)
WO (1) WO2019043306A1 (fr)

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2307273A (en) * 1940-08-24 1943-01-05 Infilco Inc Balanced valve
US2864410A (en) * 1956-06-28 1958-12-16 Texas Co Tandem valve arrangement for use with an eductor defueling system
GB914746A (en) * 1959-03-03 1963-01-02 British Petroleum Co Flow control system
SU848389A1 (ru) * 1976-07-12 1981-07-23 Предприятие П/Я В-2481 Система заправки
CH661333A5 (en) * 1983-05-19 1987-07-15 Sulzer Ag Pressure-operated valve device
RU2125656C1 (ru) * 1996-01-03 1999-01-27 Уфимский государственный авиационный технический университет Устройство автоматического дозирования топлива в силовых установках летательных аппаратов
JP2001241069A (ja) * 2000-02-28 2001-09-04 Kubota Corp 断水防止装置
JP2003154886A (ja) * 2001-11-21 2003-05-27 Showa Aircraft Ind Co Ltd 燃料給油車
RU23856U1 (ru) * 2002-03-13 2002-07-20 Федеральное государственное унитарное предприятие "Государственное машиностроительное конструкторское бюро "Радуга" им. А.Я.Березняка" Топливная система летательного аппарата с ускоренной заправкой
RU2435972C1 (ru) * 2010-03-01 2011-12-10 Открытое акционерное общество "СТАР" Способ управления расходом топлива в многоколлекторную камеру сгорания газотурбинного двигателя
RU113539U1 (ru) * 2011-10-20 2012-02-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Топливная система летательного аппарата
CA2959502A1 (fr) * 2014-08-29 2016-03-03 Schlumberger Canada Limited Systeme de commande d'ecoulement autonome et methodologie

Also Published As

Publication number Publication date
FR3070375A1 (fr) 2019-03-01
EP3658461A1 (fr) 2020-06-03
RU2739369C9 (ru) 2021-04-30
RU2739369C1 (ru) 2020-12-23
BR112020002921A2 (pt) 2020-07-28
JP2020531364A (ja) 2020-11-05
US20200356116A1 (en) 2020-11-12
WO2019043306A1 (fr) 2019-03-07
CA3071487A1 (fr) 2019-03-07

Similar Documents

Publication Publication Date Title
RU2019111631A (ru) Автоматизированная промывочная система для системы винтового насоса
EA201791092A1 (ru) Система бурения с управляемым давлением с измерением расхода и управлением скважиной
FR3030396B1 (fr) Procede de gestion d'un vehicule autonome ou partiellement autonome et dispositif de signalisation pour sa mise en oeuvre
MX2021006659A (es) Aparatos de bombeo submarinos y metodos relacionados.
MX2017003597A (es) Medidor de flujo coriolis que tiene tubo de flujo con diferencial de presion ecualizada.
EP2500510A3 (fr) Détection d'afflux de fluide améliorée au cours du forage sous pression controlée
RU2015132796A (ru) Отклонение потока в циркуляционной системе для буровой текучей среды для регулировки давления буровой текучей среды
RU2018122438A (ru) Устройство для регулирования давления закачки при принудительном извлечении нефти
GB2537561A (en) Standing injection valve with hydraulically dampened valve closure
CO2020001739A2 (es) Aparatos y sistemas para la regulación de flujo desde una formación geológica y métodos relacionados
MX2017004067A (es) Aparato para controlar la presion de inyeccion en la recuperacion mejorada de petroleo costa afuera.
GB2541568A (en) Device and method for scaling reduction in a dead water zone of a fluid conduit
FR3042818B1 (fr) Recirculation de fluide a travers une pompe centrifuge de turbomachine
NO20171693A1 (en) Apparatus and method for injecting a chemical to facilitate operation of a submersible well pump
FR3028202B1 (fr) Dispositif d'alimentation d'un dispositif de moulage, ligne de moulage et procede de pilotage de la ligne de moulage
BR112018072266A2 (pt) método e sistema para monitorar a integridade de um subsistema de fluido hidráulico
FR3070375B1 (fr) Procede de circulation de carburant dans une conduite de remplissage d'un reservoir d'un aeronef, et vanne connectee a une conduite pour la mise en œuvre dudit procede
MY187413A (en) A method of priming a drainage apparatus for siphoning liquid and a drainage apparatus
AR099801A1 (es) Sistema de control de contrapresión
FR3059726B1 (fr) Systeme correcteur d'effet pogo
BR112018009533A2 (pt) aparelho e métodos para determinação da eficiência em tempo real da extração de gás a partir de fluido de perfuração em superfície
FR3050483B1 (fr) Turbine pour conduite avec limitation de vitesse
SE1751065A1 (en) A system for providing a flow to a fluid
FR3012533B1 (fr) Dispositif de pressurisation autogene d'un reservoir d'ergol
CN203925617U (zh) 套装油管路循环油量调节装置

Legal Events

Date Code Title Description
PLSC Publication of the preliminary search report

Effective date: 20190301

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

CA Change of address

Effective date: 20210318

CD Change of name or company name

Owner name: SAFRAN AEROTECHNICS SAS, FR

Effective date: 20210318

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

RM Correction of a material error

Effective date: 20220621

PLFP Fee payment

Year of fee payment: 7