ATE300467T1 - Kammereinlass-massenwirbelungsgenerator - Google Patents

Kammereinlass-massenwirbelungsgenerator

Info

Publication number
ATE300467T1
ATE300467T1 AT02721438T AT02721438T ATE300467T1 AT E300467 T1 ATE300467 T1 AT E300467T1 AT 02721438 T AT02721438 T AT 02721438T AT 02721438 T AT02721438 T AT 02721438T AT E300467 T1 ATE300467 T1 AT E300467T1
Authority
AT
Austria
Prior art keywords
flow passageway
uniform
compressor
area
vibration generator
Prior art date
Application number
AT02721438T
Other languages
English (en)
Inventor
Yogendra Y Sheoran
Bruce D Bouldin
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
Application granted granted Critical
Publication of ATE300467T1 publication Critical patent/ATE300467T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00—Power installations for auxiliary purposes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15D—FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS
    • F15D1/00—Influencing flow of fluids
    • F15D1/02—Influencing flow of fluids in pipes or conduits
    • F15D1/04—Arrangements of guide vanes in pipe elbows or duct bends; Construction of pipe conduit elements for elbows with respect to flow, e.g. for reducing losses of flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0213—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for auxiliary power units (APU's)
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/50—Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Slot Machines And Peripheral Devices (AREA)
  • Fuel Cell (AREA)
AT02721438T 2001-03-15 2002-03-14 Kammereinlass-massenwirbelungsgenerator ATE300467T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/809,588 US6520738B2 (en) 2001-03-15 2001-03-15 Plenum entry bulk swirl generator
PCT/US2002/008031 WO2002074621A1 (en) 2001-03-15 2002-03-14 Plenum entry bulk swirl generator

Publications (1)

Publication Number Publication Date
ATE300467T1 true ATE300467T1 (de) 2005-08-15

Family

ID=25201692

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02721438T ATE300467T1 (de) 2001-03-15 2002-03-14 Kammereinlass-massenwirbelungsgenerator

Country Status (6)

Country Link
US (1) US6520738B2 (de)
EP (1) EP1368228B1 (de)
JP (1) JP2004524474A (de)
AT (1) ATE300467T1 (de)
DE (1) DE60205229T2 (de)
WO (1) WO2002074621A1 (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7093589B2 (en) * 2004-01-08 2006-08-22 Visteon Global Technologies, Inc. Apparatus for increasing induction air flow rate to a turbocharger
EP1632678A1 (de) * 2004-09-01 2006-03-08 Ford Global Technologies, LLC, A subsidary of Ford Motor Company Drallgenerator in Bögen
US7698896B2 (en) * 2005-07-27 2010-04-20 Honeywell International Inc. Compact, light weight eductor oil cooler plenum and surge flow plenum design
US7600714B2 (en) * 2006-04-20 2009-10-13 Honeywell International Inc. Diffusing air inlet door assembly
US9194293B2 (en) * 2007-09-18 2015-11-24 Hamilton Sundstrand Corporation Air inlet noise attenuation assembly
DE112008002608T5 (de) * 2007-10-19 2010-09-02 Borgwarner Inc., Auburn Hills Kanal zur Strömungsumlenkung, insbesondere für einen Turboladerverdichtereinlass
GB0821089D0 (en) * 2008-11-19 2008-12-24 Ford Global Tech Llc A method for improving the performance of a radial compressor
US9091275B2 (en) * 2009-09-03 2015-07-28 Honeywell International Inc. Integrated EGR mixer and ported shroud housing compressor
JP5864264B2 (ja) * 2009-12-29 2016-02-17 川崎重工業株式会社 過給機の吸入ダクト
CN102182521B (zh) * 2011-04-21 2014-02-26 中国船舶重工集团公司第七�三研究所 一种内部装有导流板的焊接弯头
JP5787790B2 (ja) * 2012-02-29 2015-09-30 三菱重工業株式会社 遠心流体機械の吸気管構造
JP5917243B2 (ja) * 2012-04-06 2016-05-11 三菱日立パワーシステムズ株式会社 ガスタービン改造方法及び改造を施したガスタービン
KR101692665B1 (ko) * 2013-06-20 2017-01-03 미츠비시 히타치 파워 시스템즈 가부시키가이샤 기체 안내 장치, 이것을 구비하고 있는 설비
US9719352B2 (en) 2014-12-17 2017-08-01 Honeywell International Inc. Compartment based inlet particle separator system
JP6446705B2 (ja) * 2015-01-09 2019-01-09 三菱重工業株式会社 エンジンシステム
US9926942B2 (en) * 2015-10-27 2018-03-27 Pratt & Whitney Canada Corp. Diffuser pipe with vortex generators
JP6601338B2 (ja) * 2016-07-20 2019-11-06 トヨタ自動車株式会社 ダクト構造
US10415502B2 (en) 2017-09-11 2019-09-17 Honeywell International Inc. Swirling flow eductor system and method
US11105264B2 (en) * 2019-12-18 2021-08-31 Rolls-Royce Deutschland Ltd & Co Kg Asymmetric submerged air intake
US11592041B2 (en) 2020-10-28 2023-02-28 Artisan Industries, Inc. Device for increasing flow capacity of a fluid channel
KR102786958B1 (ko) * 2022-02-25 2025-03-27 두산에너빌리티 주식회사 공기 인렛 매니폴드 및 이를 포함하는 가스터빈
US12275533B2 (en) * 2023-06-02 2025-04-15 Honeywell International Inc. Inlet system for auxiliary power unit
US12372105B2 (en) * 2023-09-28 2025-07-29 Fca Us Llc Duct having air direction feature
TWM657368U (zh) * 2023-11-20 2024-07-01 台灣飛行器股份有限公司 無人飛行裝置
US12553450B2 (en) * 2024-05-23 2026-02-17 Pratt & Whitney Canada Corp. Plenum closure panel with integrated airflow direction device

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE842561C (de) 1949-02-04 1952-06-30 Oesterr Amerikan Magnesit Einrichtung zum Umlenken eines in einem Kanal sich bewegenden Fluessigkeits- bzw. Gasstromes mit unsymmetrischem Geschwindigkeitsprofil
US2694357A (en) 1950-07-18 1954-11-16 Chance Vought Aircraft Inc Boundary layer energization for flush inlets
FR1231173A (fr) 1959-04-09 1960-09-27 Soc Lab Sarl Perfectionnements à l'écoulement des fluides suivant des trajectoires non rectilignes
US3033491A (en) 1960-08-04 1962-05-08 Gen Electric Inlet for vertical take-off aircraft
DE1528883A1 (de) * 1966-07-15 1971-06-03 Voith Gmbh J M Saugkruemmer fuer Kreiselpumpen
US3432123A (en) 1967-04-03 1969-03-11 Dehavilland Aircraft Cross ducting system for augmentor wing aircraft
US4174083A (en) 1977-04-29 1979-11-13 The Boeing Company Flow deflector for fluid inlet
US4245803A (en) 1978-08-02 1981-01-20 United Technologies Corporation Two-dimensional inlet for a high speed winged flight vehicle
US4381017A (en) 1980-04-05 1983-04-26 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Air inlet, especially a two-dimensional air inlet set at an angle on one side for gas turbine jet propulsion plants for driving airplanes
US4378097A (en) 1980-11-24 1983-03-29 The Boeing Company High performance submerged air inlet
US4418879A (en) 1980-12-29 1983-12-06 The Boeing Company Scoop and inlet for auxiliary power units and method
US4418880A (en) 1981-11-27 1983-12-06 Waal J F De Fluid flow augmentor
US4685942A (en) 1982-12-27 1987-08-11 General Electric Company Axial flow inlet particle separator
US4696442A (en) 1986-07-14 1987-09-29 The Boeing Company Vortex generators for inlets
CA1331872C (en) * 1989-05-23 1994-09-06 Richard Sixsmith Centrifugal radially aligned outlet type fan with baffle
DE4008951A1 (de) 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlauframpe fuer ueber- oder hyperschallflugzeuge
DE4008956A1 (de) 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlaufsystem fuer ueber- oder hyperschallflugzeuge
US5327940A (en) 1992-03-09 1994-07-12 United Technologies Corporation Mechanism to reduce turning losses in angled conduits
US5655359A (en) 1995-05-15 1997-08-12 The Boeing Company Passive cooling device and method for cooling an auxiliary power unit on an airplane
DE19603337C1 (de) * 1996-01-31 1997-08-14 Grundfos As Kreiselpumpe
DE19819769C2 (de) 1998-05-04 2000-03-02 Siemens Ag Gasturbinenanlage
US6264137B1 (en) 2000-02-25 2001-07-24 Honeywell International Inc. Inlet vortex bustor and ice protector for auxiliary power units

Also Published As

Publication number Publication date
EP1368228A1 (de) 2003-12-10
US20020131862A1 (en) 2002-09-19
US6520738B2 (en) 2003-02-18
WO2002074621A1 (en) 2002-09-26
DE60205229T2 (de) 2006-05-24
EP1368228B1 (de) 2005-07-27
JP2004524474A (ja) 2004-08-12
DE60205229D1 (de) 2005-09-01

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