ATE378508T1 - Doppelter einlass eines strahltriebwerks - Google Patents

Doppelter einlass eines strahltriebwerks

Info

Publication number
ATE378508T1
ATE378508T1 AT02075713T AT02075713T ATE378508T1 AT E378508 T1 ATE378508 T1 AT E378508T1 AT 02075713 T AT02075713 T AT 02075713T AT 02075713 T AT02075713 T AT 02075713T AT E378508 T1 ATE378508 T1 AT E378508T1
Authority
AT
Austria
Prior art keywords
boundary layer
engine
air inlet
turbofan
inlet
Prior art date
Application number
AT02075713T
Other languages
English (en)
Inventor
Gerhard E Seidel
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=25222095&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ATE378508(T1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE378508T1 publication Critical patent/ATE378508T1/de

Links

Classifications

    • 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
    • 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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft
    • B64C2039/105—All-wing aircraft of blended wing body type
    • 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
    • B64D2033/0253—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
    • B64D2033/026—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic 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
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Means For Warming Up And Starting Carburetors (AREA)
  • Percussion Or Vibration Massage (AREA)
AT02075713T 2001-03-23 2002-02-22 Doppelter einlass eines strahltriebwerks ATE378508T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/816,985 US6527224B2 (en) 2001-03-23 2001-03-23 Separate boundary layer engine inlet

Publications (1)

Publication Number Publication Date
ATE378508T1 true ATE378508T1 (de) 2007-11-15

Family

ID=25222095

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02075713T ATE378508T1 (de) 2001-03-23 2002-02-22 Doppelter einlass eines strahltriebwerks

Country Status (5)

Country Link
US (1) US6527224B2 (de)
EP (1) EP1243782B2 (de)
AT (1) ATE378508T1 (de)
DE (1) DE60223439T3 (de)
ES (1) ES2292685T5 (de)

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US20060157613A1 (en) * 2005-01-19 2006-07-20 Adamson Eric E Supersonic aircraft with active lift distribution control for reducing sonic boom
US7721989B2 (en) * 2006-03-01 2010-05-25 The Boeing Company Multi-path inlet for aircraft engine
WO2008017567A1 (de) * 2006-08-11 2008-02-14 Team Smartfish Gmbh Lufteinlass eines strahltriebwerks
US7861968B2 (en) * 2006-10-26 2011-01-04 The Boeing Company Air inlet and method for a highspeed mobile platform
US7624944B2 (en) * 2006-10-26 2009-12-01 The Boeing Company Tandem air inlet apparatus and method for an airborne mobile platform
US7665689B2 (en) * 2006-11-24 2010-02-23 The Boeing Company Unconventional integrated propulsion systems and methods for blended wing body aircraft
US7784732B2 (en) * 2007-01-04 2010-08-31 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Boundary-layer-ingesting inlet flow control system
ITTO20080142A1 (it) * 2008-02-28 2009-08-29 Alenia Aeronautica Spa Presa d'aria, in particolare per un espulsore di chaff per velivolo
GB2461718A (en) * 2008-07-10 2010-01-13 Rolls Royce Plc An aircraft propulsion arrangement having a single fan located within a curved guide path
FR2938824A1 (fr) * 2008-11-26 2010-05-28 Aircelle Sa Nacelle integree sur aile volante
US7793884B2 (en) * 2008-12-31 2010-09-14 Faruk Dizdarevic Deltoid main wing aerodynamic configurations
US8511603B2 (en) * 2009-01-14 2013-08-20 Lewis E. Blomeley Roadable aircraft with collapsible wings and ductless fan
US8052083B1 (en) * 2009-09-17 2011-11-08 John Patrick Moran Bird deflector and air replacement system technical field
US8844262B2 (en) * 2009-12-29 2014-09-30 Rolls-Royce North American Technologies, Inc. Exhaust for a gas turbine engine
US8056852B1 (en) * 2011-02-21 2011-11-15 Faruk Dizdarevic Longitudinal flying wing aircraft
GB201117104D0 (en) * 2011-10-05 2011-11-16 Rolls Royce Plc A duct
US9291101B2 (en) * 2013-02-28 2016-03-22 United Technologies Corporation Gas turbine engine inlet wall design
US10907544B2 (en) 2014-03-27 2021-02-02 Raytheon Technologies Corporation Gas turbine engine inlet wall design
CN103950542B (zh) * 2014-04-04 2017-01-04 张鑫宇 用于减小飞机在飞行中空气阻力的装置
US10421553B2 (en) * 2015-01-20 2019-09-24 United Technologies Corporation Pusher fan engine with in wing configuration
JP6128568B2 (ja) * 2015-03-26 2017-05-17 株式会社Ｓｕｂａｒｕ 航空機のインテーク構造
US9758253B2 (en) 2015-06-25 2017-09-12 Northrop Grumman Systems Corporation Swept gradient boundary layer diverter
RU2605653C1 (ru) * 2015-08-28 2016-12-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Способ размещения двигателя на летательном аппарате типа "летающее крыло"
US10556702B2 (en) * 2016-07-13 2020-02-11 General Electric Company Aircraft having an airflow duct
US10436055B2 (en) 2016-12-21 2019-10-08 United Technologies Corporation Distributed fan lubrication system
CN109720586A (zh) * 2017-10-30 2019-05-07 成都飞机工业（集团）有限责任公司 一种附面层隔道
US10807013B2 (en) 2017-12-20 2020-10-20 Francis A. Alonso Modified delta wing kite with inflatable fuselage
USD873350S1 (en) * 2018-08-23 2020-01-21 Francis A. Alonso Zig-zagged swept wing kite
USD875183S1 (en) * 2018-08-23 2020-02-11 Francis A. Alonso Zig-zagged swept wing kite
USD874578S1 (en) * 2018-08-23 2020-02-04 Francis A. Alonso Swept wing kite
USD874577S1 (en) * 2018-08-23 2020-02-04 Francis A. Alonso Swept wing kite
US11124291B2 (en) 2018-12-13 2021-09-21 Raytheon Technologies Corporation System to promote accelerated boundary layer ingestion
US11247776B2 (en) * 2019-04-01 2022-02-15 The Boeing Company Aircraft having embedded engines
WO2021007216A1 (en) * 2019-07-08 2021-01-14 DZYNE Technologies Incorporated Drag recovery scheme using boundary layer ingestion
CN110304267B (zh) * 2019-07-19 2020-08-11 中国人民解放军国防科技大学 高超声速飞行器设计方法及系统
CN111412066B (zh) * 2020-04-27 2023-04-04 南昌航空大学 一种带环向自适应引流管的三维内转进气道及设计方法
US11767776B2 (en) * 2020-09-04 2023-09-26 The Boeing Company Propulsion flow path duct systems and methods
US12552534B2 (en) 2022-04-12 2026-02-17 General Electric Company Blended wing body aircraft
DE102022113595A1 (de) 2022-05-30 2023-11-30 Reiner Brach Luftfahrzeug zum Fliegen in Umgebungsluft mittels dynamischen Auftriebs
US11827339B1 (en) 2023-01-27 2023-11-28 Jetzero, Inc. Apparatus for ingesting boundary layer flow for an aircraft
CN119305713A (zh) * 2024-11-05 2025-01-14 中国航空工业集团公司西安飞机设计研究所 一种翼身融合布局飞机动力装置及其操控方法

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Also Published As

Publication number Publication date
EP1243782B1 (de) 2007-11-14
ES2292685T3 (es) 2008-03-16
DE60223439T2 (de) 2008-10-02
EP1243782A3 (de) 2005-03-02
US20020134886A1 (en) 2002-09-26
ES2292685T5 (es) 2013-11-14
US6527224B2 (en) 2003-03-04
DE60223439T3 (de) 2013-12-12
EP1243782A2 (de) 2002-09-25
DE60223439D1 (de) 2007-12-27
EP1243782B2 (de) 2013-07-10

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