ATE490912T1 - Steuersystem für einlassverzerrung und wiederherstellung - Google Patents

Steuersystem für einlassverzerrung und wiederherstellung

Info

Publication number
ATE490912T1
ATE490912T1 AT07753379T AT07753379T ATE490912T1 AT E490912 T1 ATE490912 T1 AT E490912T1 AT 07753379 T AT07753379 T AT 07753379T AT 07753379 T AT07753379 T AT 07753379T AT E490912 T1 ATE490912 T1 AT E490912T1
Authority
AT
Austria
Prior art keywords
air
aircraft
engine
inlet
force
Prior art date
Application number
AT07753379T
Other languages
English (en)
Inventor
Joseph Silkey
Christopher Wilson
Richard Dyer
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE490912T1 publication Critical patent/ATE490912T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • F01D5/145Means for influencing boundary layers or secondary circulations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/057Control or regulation
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0226Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising boundary layer control means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/17Purpose of the control system to control boundary layer
    • F05D2270/172Purpose of the control system to control boundary layer by a plasma generator, e.g. control of ignition
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Plasma Technology (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
  • Testing Of Engines (AREA)
AT07753379T 2006-04-12 2007-03-16 Steuersystem für einlassverzerrung und wiederherstellung ATE490912T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/403,252 US7637455B2 (en) 2006-04-12 2006-04-12 Inlet distortion and recovery control system
PCT/US2007/006746 WO2007123612A1 (en) 2006-04-12 2007-03-16 Inlet distortion and recovery control system

Publications (1)

Publication Number Publication Date
ATE490912T1 true ATE490912T1 (de) 2010-12-15

Family

ID=38325140

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07753379T ATE490912T1 (de) 2006-04-12 2007-03-16 Steuersystem für einlassverzerrung und wiederherstellung

Country Status (7)

Country Link
US (2) US7637455B2 (de)
EP (1) EP2010429B1 (de)
JP (1) JP5265519B2 (de)
CN (1) CN101421156B (de)
AT (1) ATE490912T1 (de)
DE (1) DE602007011047D1 (de)
WO (1) WO2007123612A1 (de)

Families Citing this family (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8006939B2 (en) * 2006-11-22 2011-08-30 Lockheed Martin Corporation Over-wing traveling-wave axial flow plasma accelerator
US7870720B2 (en) * 2006-11-29 2011-01-18 Lockheed Martin Corporation Inlet electromagnetic flow control
US8016246B2 (en) * 2007-05-25 2011-09-13 The Boeing Company Plasma actuator system and method for use with a weapons bay on a high speed mobile platform
US7866609B2 (en) * 2007-06-15 2011-01-11 The Boeing Company Passive removal of suction air for laminar flow control, and associated systems and methods
WO2009015371A2 (en) * 2007-07-25 2009-01-29 University Of Florida Research Foundation Inc. Method and apparatus for efficient micropumping
US8091836B2 (en) * 2007-12-19 2012-01-10 Pratt & Whitney Rocketdyne, Inc. Rotary wing system with ion field flow control
US7995575B2 (en) * 2008-01-02 2011-08-09 Cisco Technology, Inc. Packet error handling
US8220753B2 (en) * 2008-01-04 2012-07-17 The Boeing Company Systems and methods for controlling flows with pulsed discharges
US8172547B2 (en) * 2008-01-31 2012-05-08 The Boeing Company Dielectric barrier discharge pump apparatus and method
ITTO20080142A1 (it) * 2008-02-28 2009-08-29 Alenia Aeronautica Spa Presa d'aria, in particolare per un espulsore di chaff per velivolo
DE102008001103A1 (de) * 2008-04-10 2009-10-15 Manroland Ag Umströmtes Bauteil
US9446840B2 (en) * 2008-07-01 2016-09-20 The Boeing Company Systems and methods for alleviating aircraft loads with plasma actuators
CA2732100C (en) * 2008-07-31 2013-11-26 Bell Helicopter Textron Inc. System and method for aerodynamic flow control
US8196871B2 (en) * 2008-11-26 2012-06-12 General Electric Company Control of shockwave-boundarylayer-interaction using MEMS plasma devices
US8226047B2 (en) * 2009-01-23 2012-07-24 General Electric Company Reduction of tip vortex and wake interaction effects in energy and propulsion systems
US8453457B2 (en) * 2009-08-26 2013-06-04 Lockheed Martin Corporation Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators
WO2011024736A1 (ja) 2009-08-26 2011-03-03 ダイハツ工業株式会社 プラズマアクチュエータ
US9975625B2 (en) 2010-04-19 2018-05-22 The Boeing Company Laminated plasma actuator
FR2959342B1 (fr) * 2010-04-27 2012-06-15 Snecma Procede de traitement des ondes acoustiques emises en sortie d'un turbomoteur d'un aeronef avec un dispositif a decharge a barriere dielectrique et aeronef comprenant un tel dispositif
US8523115B2 (en) 2011-01-28 2013-09-03 Lockheed Martin Corporation System, apparatus, program product, and related methods for providing boundary layer flow control
US8944370B2 (en) * 2012-01-09 2015-02-03 The Boeing Company Plasma actuating propulsion system for aerial vehicles
US20130312385A1 (en) * 2012-05-24 2013-11-28 General Electric Company Gas turbine system having a plasma actuator flow control arrangement
US20140119879A1 (en) * 2012-10-29 2014-05-01 General Electric Company Turbomachine plasma seal system
US20140144517A1 (en) * 2012-11-27 2014-05-29 Board Of Regents, The University Of Texas System Rail plasma actuator for high-authority flow control
DE102013200470A1 (de) * 2013-01-15 2014-07-17 Siemens Aktiengesellschaft Verfahren zur Steuerung eines Gasmassenstroms, Strömungskanal sowie Turbomaschine mit Strömungskanal
US9884688B2 (en) * 2013-02-14 2018-02-06 Gulfstream Aerospace Corporation Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system
US9820369B2 (en) 2013-02-25 2017-11-14 University Of Florida Research Foundation, Incorporated Method and apparatus for providing high control authority atmospheric plasma
US20160122005A1 (en) * 2013-03-11 2016-05-05 United Technologies Corporation Embedded engines in hybrid blended wing body
US9359950B2 (en) 2013-05-20 2016-06-07 Honeywell International Inc. Gas turbine engines having plasma flow-controlled intake systems
CN104443404A (zh) * 2014-11-24 2015-03-25 江西洪都航空工业集团有限责任公司 一种飞行器的s形进气道结构
EP3090952B1 (de) * 2015-03-31 2018-10-03 Rolls-Royce Corporation Triebwerksgondel
US9758253B2 (en) 2015-06-25 2017-09-12 Northrop Grumman Systems Corporation Swept gradient boundary layer diverter
US10131442B2 (en) * 2015-10-30 2018-11-20 Sikorsky Aircraft Corporation Power leveling controller
US10794281B2 (en) * 2016-02-02 2020-10-06 General Electric Company Gas turbine engine having instrumented airflow path components
US10753278B2 (en) 2016-03-30 2020-08-25 General Electric Company Translating inlet for adjusting airflow distortion in gas turbine engine
US11073090B2 (en) 2016-03-30 2021-07-27 General Electric Company Valved airflow passage assembly for adjusting airflow distortion in gas turbine engine
US9777633B1 (en) 2016-03-30 2017-10-03 General Electric Company Secondary airflow passage for adjusting airflow distortion in gas turbine engine
US10704418B2 (en) 2016-08-11 2020-07-07 General Electric Company Inlet assembly for an aircraft aft fan
US10399670B2 (en) * 2016-09-26 2019-09-03 General Electric Company Aircraft having an aft engine and internal flow passages
US20180208297A1 (en) * 2017-01-20 2018-07-26 General Electric Company Nacelle for an aircraft aft fan
US10837362B2 (en) 2016-10-12 2020-11-17 General Electric Company Inlet cowl for a turbine engine
US11149639B2 (en) * 2016-11-29 2021-10-19 Rolls-Royce North American Technologies Inc. Systems and methods of reducing distortions of the inlet airflow to a turbomachine
US10549845B2 (en) * 2017-05-26 2020-02-04 United Technologies Corporation Dedicated fans for boundary layer ingestion
GB201716836D0 (en) * 2017-10-13 2017-11-29 Rolls Royce Plc Gas turbine engine vortex suppressor
US10495121B2 (en) * 2017-11-10 2019-12-03 X Development Llc Method and apparatus for combined anemometer and plasma actuator
KR101860686B1 (ko) 2017-11-13 2018-06-29 국방과학연구소 플라즈마 구동기 보호 장치 및 이의 조립 방법
CN109159903A (zh) * 2018-08-23 2019-01-08 广州创链科技有限公司 一种无人机发动机进行口气流调节装置
US11125770B2 (en) * 2018-12-06 2021-09-21 Rosemount Aerospace Inc. Acoustic air data sensor and system
EP3980332A4 (de) * 2019-06-07 2023-06-14 Massachusetts Institute of Technology Elektroaerodynamische vorrichtungen
US11905983B2 (en) 2020-01-23 2024-02-20 Deep Science, Llc Systems and methods for active control of surface drag using electrodes
US12065236B2 (en) 2020-01-23 2024-08-20 Enterprise Science Fund, Llc Systems and methods for active control of surface drag using intermittent or variable actuation
CN113567141B (zh) * 2020-04-28 2024-02-02 中国航发商用航空发动机有限责任公司 畸变发生装置及其模拟方法和压力畸变特性试验系统
US11333079B2 (en) * 2020-04-28 2022-05-17 General Electric Company Methods and apparatus to detect air flow separation of an engine
US11542866B2 (en) * 2020-05-13 2023-01-03 The Boeing Company Adaptable flow control for engine nacelles
EP4294720A1 (de) 2021-02-17 2023-12-27 Enterprise Science Fund, Llc Querimpulsinjektion auf gleicher ebene zur unterbrechung von grossflächigen wirbeln in einer turbulenten grenzschicht
US12071224B2 (en) 2021-11-30 2024-08-27 The Boeing Company Aircraft boundary layer ingestion using multiple fans and associated methods
CN114194402B (zh) * 2021-12-16 2024-05-31 重庆交通大学绿色航空技术研究院 等离子体激励的无附面隔层进气道系统及进气控制方法
US12065979B2 (en) 2022-12-27 2024-08-20 Rolls-Royce North American Technologies Inc. Distributed electric and hybrid fans for distortion tolerance of turbofan engines
US11835064B1 (en) 2022-12-27 2023-12-05 Rolls-Royce North American Technologies Inc. Electric fan array for distortion tolerance of turbofan engines
US12025059B1 (en) 2022-12-27 2024-07-02 Rolls-Royce North American Technologies Inc. Distributed electric tip fans for distortion tolerance of turbofan engines
US12065258B2 (en) * 2023-01-25 2024-08-20 Rolls-Royce North American Technologies Inc. Multiple intake distortion adaptive fan for gas turbine engine
US12545422B2 (en) 2023-01-26 2026-02-10 The Boeing Company Variable compression air intakes for aircraft propulsion systems and methods for varying compression of an air intake
CN117780513A (zh) * 2023-11-20 2024-03-29 南京航空航天大学 一种进气畸变条件下的航空发动机稳定性控制方法
US12503978B1 (en) 2024-06-21 2025-12-23 Rolls-Royce North American Technologies Inc. Inlets for gas turbine engine fans with distortion tolerance
CN118395906B (zh) * 2024-06-28 2024-09-27 中国航发湖南动力机械研究所 进气畸变试验中温度畸变与压力畸变的等效转换方法及系统

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2694357A (en) * 1950-07-18 1954-11-16 Chance Vought Aircraft Inc Boundary layer energization for flush inlets
US3360220A (en) * 1959-01-26 1967-12-26 Space Technology Lab Inc Magnetohydrodynamic method and apparatus
US3041827A (en) * 1959-02-25 1962-07-03 Curtiss Wright Corp Supersonic inlet
GB1119701A (en) * 1964-08-13 1968-07-10 Bristol Siddeley Engines Ltd Guards for air intakes of jet engines
US4154256A (en) * 1978-03-29 1979-05-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Self stabilizing sonic inlet
US4891600A (en) * 1982-07-26 1990-01-02 Cox James E Dipole accelerating means and method
DE3407137A1 (de) 1984-02-28 1985-08-29 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Einrichtung zur verbesserung der stroemungsverhaeltnisse am lufteinlauf fuer in flugzeugen eingebaute gasturbinentriebwerke
US4696442A (en) * 1986-07-14 1987-09-29 The Boeing Company Vortex generators for inlets
US5058837A (en) * 1989-04-07 1991-10-22 Wheeler Gary O Low drag vortex generators
US5447283A (en) * 1994-02-02 1995-09-05 Grumman Aerospace Corporation Blown boundary layer control system for a jet aircraft
US5598990A (en) * 1994-12-15 1997-02-04 University Of Kansas Center For Research Inc. Supersonic vortex generator
US5779189A (en) 1996-03-19 1998-07-14 Lockheed Martin Corporation System and method for diverting boundary layer air
US5749542A (en) 1996-05-28 1998-05-12 Lockheed Martin Corporation Transition shoulder system and method for diverting boundary layer air
WO1999035893A2 (en) 1998-01-08 1999-07-15 The University Of Tennessee Research Corporation Paraelectric gas flow accelerator
US6138950A (en) * 1998-10-06 2000-10-31 Northrop Grumman Corporation Aircraft engine air intake system
US6504308B1 (en) * 1998-10-16 2003-01-07 Kronos Air Technologies, Inc. Electrostatic fluid accelerator
US20020134891A1 (en) * 2001-02-09 2002-09-26 Guillot Stephen A. Ejector pump flow control
GB0108740D0 (en) 2001-04-06 2001-05-30 Bae Systems Plc Turbulent flow drag reduction
US6570333B1 (en) 2002-01-31 2003-05-27 Sandia Corporation Method for generating surface plasma
US20040011917A1 (en) 2002-07-18 2004-01-22 Saeks Richard E. Shock wave modification via shock induced ion doping
US6796532B2 (en) 2002-12-20 2004-09-28 Norman D. Malmuth Surface plasma discharge for controlling forebody vortex asymmetry
US6805325B1 (en) 2003-04-03 2004-10-19 Rockwell Scientific Licensing, Llc. Surface plasma discharge for controlling leading edge contamination and crossflow instabilities for laminar flow
US7380756B1 (en) * 2003-11-17 2008-06-03 The United States Of America As Represented By The Secretary Of The Air Force Single dielectric barrier aerodynamic plasma actuation
US7510149B2 (en) * 2004-08-02 2009-03-31 Lockheed Martin Corporation System and method to control flowfield vortices with micro-jet arrays
US7744039B2 (en) * 2006-01-03 2010-06-29 The Boeing Company Systems and methods for controlling flows with electrical pulses

Also Published As

Publication number Publication date
EP2010429B1 (de) 2010-12-08
JP5265519B2 (ja) 2013-08-14
US7637455B2 (en) 2009-12-29
WO2007123612A1 (en) 2007-11-01
EP2010429A1 (de) 2009-01-07
CN101421156A (zh) 2009-04-29
US7975961B2 (en) 2011-07-12
CN101421156B (zh) 2011-05-25
JP2009533276A (ja) 2009-09-17
US20070241229A1 (en) 2007-10-18
US20100140418A1 (en) 2010-06-10
DE602007011047D1 (de) 2011-01-20

Similar Documents

Publication Publication Date Title
ATE490912T1 (de) Steuersystem für einlassverzerrung und wiederherstellung
EP2837563A3 (de) Verbessertes Motorkühlsystem und Verfahren
BR112013024178A2 (pt) dispositivo de ncpap e método para dividir um fluxo de jato de gás em um sistema de ncpap
WO2014055152A3 (en) Bifurcated inlet scoop for gas turbine engine
EP2500552A3 (de) Kraftstoff-Durchflusssystem mit zwei Pumpen für einen Gasturbinenmotor und Regelungsverfahren
BR112015026459A2 (pt) motor de turboventilador de aeronave
BRPI0907478A2 (pt) flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave
WO2013180788A3 (en) Constant speed pump system for engine ecs loss elimination
EP3415832A3 (de) Energieaustauschsystem zur klimatisierung in einer geschlossenen struktur
WO2009141400A3 (de) Inertisierungssystem für ein flugzeug
MX2015012758A (es) Metodo y sistema para modulacion de la respiracion.
EP2527742A3 (de) System und Verfahren zur Strömungssteuerung in einem Gasturbinenmotor
WO2013049438A3 (en) Supercharger assembly with independent superchargers and motor/generator
WO2012010116A3 (de) Angetriebenes fluggerät, insbesondere als nurflügler und/oder mit geringer radarsignatur ausgebildetes fluggerät
WO2013064768A3 (fr) Pylone d'accrochage pour turbomachine
EP2631182A3 (de) Hilfsstromaggregat
FR2975969B1 (fr) Systeme de conditionnement d'air d'un compartiment pour passagers d'un aeronef
WO2013029016A3 (en) Retrofit attachments for water treatment systems
WO2012167052A8 (en) Systems and methods for an engine
ATE502194T1 (de) Integrierte motorabgassysteme und verfahren zur reduzierung von widerstand und wärmebelastung
DE602006006865D1 (de) Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt
DE602007001781D1 (de) Flugzeugklimatisierungssystem mit zyklonabscheidern
WO2013043343A8 (en) Systems and methods for controlling exhaust flow through an aftertreatment device
BR112013015617A2 (pt) conjunto de válvula para o controle da admissão de ar em um compressor de um veículo, bem como sistema de compressor e método para o controle de sistemas de compressor
CN102673794A (zh) 一种采用供油泵作为动力的空中放油装置

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties