SG131832A1 - Variable geometry inlet guide vane - Google Patents

Variable geometry inlet guide vane

Info

Publication number
SG131832A1
SG131832A1 SG200605790-5A SG2006057905A SG131832A1 SG 131832 A1 SG131832 A1 SG 131832A1 SG 2006057905 A SG2006057905 A SG 2006057905A SG 131832 A1 SG131832 A1 SG 131832A1
Authority
SG
Singapore
Prior art keywords
guide vane
inlet guide
variable geometry
geometry inlet
variable
Prior art date
Application number
SG200605790-5A
Other languages
English (en)
Inventor
Christian A Carroll
James Allen Eley
Carl Brian Klinetob
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SG131832A1 publication Critical patent/SG131832A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/148—Blades with variable camber, e.g. by ejection of fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30—Vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/18—Rotors
    • F04D29/22—Rotors specially for centrifugal pumps
    • F04D29/24—Vanes
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Air-Flow Control Members (AREA)
  • Superstructure Of Vehicle (AREA)
SG200605790-5A 2005-10-25 2006-08-23 Variable geometry inlet guide vane SG131832A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/258,608 US7549839B2 (en) 2005-10-25 2005-10-25 Variable geometry inlet guide vane

Publications (1)

Publication Number Publication Date
SG131832A1 true SG131832A1 (en) 2007-05-28

Family

ID=36972756

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200605790-5A SG131832A1 (en) 2005-10-25 2006-08-23 Variable geometry inlet guide vane

Country Status (11)

Country Link
US (1) US7549839B2 (ru)
EP (3) EP2460977B1 (ru)
JP (1) JP2007120494A (ru)
KR (1) KR20070044765A (ru)
CN (1) CN1955441A (ru)
AU (1) AU2006230736A1 (ru)
BR (1) BRPI0603516A (ru)
CA (1) CA2555074A1 (ru)
IL (1) IL177592A0 (ru)
RU (1) RU2006130698A (ru)
SG (1) SG131832A1 (ru)

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US20140064955A1 (en) * 2011-09-14 2014-03-06 General Electric Company Guide vane assembly for a gas turbine engine
US9068460B2 (en) 2012-03-30 2015-06-30 United Technologies Corporation Integrated inlet vane and strut
US10221707B2 (en) 2013-03-07 2019-03-05 Pratt & Whitney Canada Corp. Integrated strut-vane
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US9494053B2 (en) 2013-09-23 2016-11-15 Siemens Aktiengesellschaft Diffuser with strut-induced vortex mixing
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US9909434B2 (en) 2015-07-24 2018-03-06 Pratt & Whitney Canada Corp. Integrated strut-vane nozzle (ISV) with uneven vane axial chords
US9915149B2 (en) 2015-08-27 2018-03-13 Rolls-Royce North American Technologies Inc. System and method for a fluidic barrier on the low pressure side of a fan blade
US10125622B2 (en) 2015-08-27 2018-11-13 Rolls-Royce North American Technologies Inc. Splayed inlet guide vanes
US20170057649A1 (en) 2015-08-27 2017-03-02 Edward C. Rice Integrated aircraft propulsion system
US10267159B2 (en) 2015-08-27 2019-04-23 Rolls-Royce North America Technologies Inc. System and method for creating a fluidic barrier with vortices from the upstream splitter
US9976514B2 (en) 2015-08-27 2018-05-22 Rolls-Royce North American Technologies, Inc. Propulsive force vectoring
US10233869B2 (en) 2015-08-27 2019-03-19 Rolls Royce North American Technologies Inc. System and method for creating a fluidic barrier from the leading edge of a fan blade
US10267160B2 (en) 2015-08-27 2019-04-23 Rolls-Royce North American Technologies Inc. Methods of creating fluidic barriers in turbine engines
US10280872B2 (en) 2015-08-27 2019-05-07 Rolls-Royce North American Technologies Inc. System and method for a fluidic barrier from the upstream splitter
US10718221B2 (en) 2015-08-27 2020-07-21 Rolls Royce North American Technologies Inc. Morphing vane
CN106050318B (zh) * 2016-05-30 2018-01-05 西安交通大学 一种适应大变工况范围的柔性静叶装置
US10443451B2 (en) 2016-07-18 2019-10-15 Pratt & Whitney Canada Corp. Shroud housing supported by vane segments
US10233782B2 (en) * 2016-08-03 2019-03-19 Solar Turbines Incorporated Turbine assembly and method for flow control
CN107725482A (zh) * 2016-08-10 2018-02-23 上海电气燃气轮机有限公司 改善压气机变工况性能的分段调节出口导叶及其调节机构
US10253779B2 (en) * 2016-08-11 2019-04-09 General Electric Company Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan
US20190078450A1 (en) * 2017-09-08 2019-03-14 United Technologies Corporation Inlet guide vane having a varied trailing edge geometry
CN107420349B (zh) * 2017-09-14 2019-03-01 西安交通大学 一种预旋条件下低流动损失的离心压缩机进口导叶结构的设计方法
CN109159902B (zh) * 2018-08-23 2020-08-21 金湖县农副产品营销协会 一种无人机发动机进气口引流机构
US10794200B2 (en) * 2018-09-14 2020-10-06 United Technologies Corporation Integral half vane, ringcase, and id shroud
US10781707B2 (en) * 2018-09-14 2020-09-22 United Technologies Corporation Integral half vane, ringcase, and id shroud
CN109058159B (zh) * 2018-09-21 2024-07-23 特灵空调系统(中国)有限公司 风机和空调系统
US10815802B2 (en) * 2018-12-17 2020-10-27 Raytheon Technologies Corporation Variable vane assemblies configured for non-axisymmetric actuation
CN110296525A (zh) * 2019-06-21 2019-10-01 珠海格力电器股份有限公司 具有降低噪音效果的导风叶片及其控制方法、空调机组
US10851705B1 (en) 2019-07-12 2020-12-01 Gm Global Technology Operations, Llc Variable inlet guide vane system for a turbocharger used in a motor vehicle
BE1027876B1 (fr) * 2019-12-18 2021-07-26 Safran Aero Boosters Sa Module pour turbomachine
CN111022189B (zh) * 2019-12-24 2022-11-01 哈尔滨工程大学 一种输水槽带导流管的进气滤清装置惯性级叶片
TWI775377B (zh) * 2021-04-06 2022-08-21 宏碁股份有限公司 散熱風扇
CN113819487B (zh) * 2021-08-17 2024-09-20 南京航空航天大学 进气余旋角度和温度分布耦合的瞬态可调畸变发生装置
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CN115717604B (zh) * 2022-09-28 2023-06-13 广东顺威精密塑料股份有限公司 一种带襟叶的后向离心风轮及其叶片叶型设计方法

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Also Published As

Publication number Publication date
EP1780378A2 (en) 2007-05-02
CN1955441A (zh) 2007-05-02
EP2460978A1 (en) 2012-06-06
US7549839B2 (en) 2009-06-23
RU2006130698A (ru) 2008-02-27
BRPI0603516A (pt) 2007-08-14
EP1780378A3 (en) 2010-10-13
CA2555074A1 (en) 2007-04-25
IL177592A0 (en) 2006-12-10
EP2460977A1 (en) 2012-06-06
EP2460978B1 (en) 2016-01-20
JP2007120494A (ja) 2007-05-17
KR20070044765A (ko) 2007-04-30
AU2006230736A1 (en) 2007-05-10
EP1780378B1 (en) 2012-03-28
EP2460977B1 (en) 2016-01-20
US20070092372A1 (en) 2007-04-26

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