JP5358682B2 - 外気を航空機内に供給するための空気路 - Google Patents
外気を航空機内に供給するための空気路 Download PDFInfo
- Publication number
- JP5358682B2 JP5358682B2 JP2011515189A JP2011515189A JP5358682B2 JP 5358682 B2 JP5358682 B2 JP 5358682B2 JP 2011515189 A JP2011515189 A JP 2011515189A JP 2011515189 A JP2011515189 A JP 2011515189A JP 5358682 B2 JP5358682 B2 JP 5358682B2
- Authority
- JP
- Japan
- Prior art keywords
- flow control
- control flap
- air
- flow
- aircraft
- 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.)
- Expired - Fee Related
Links
- 238000000034 method Methods 0.000 claims description 5
- 230000005484 gravity Effects 0.000 claims description 4
- 238000009792 diffusion process Methods 0.000 description 6
- 230000003068 static effect Effects 0.000 description 5
- 238000005265 energy consumption Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
Images
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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
-
- 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
- B64D2241/00—NACA type air intakes
-
- 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
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air-Flow Control Members (AREA)
- Duct Arrangements (AREA)
- Check Valves (AREA)
Description
Claims (10)
- 外気を航空機内に供給するための空気路(10)であって、
空気吸入口(12)、
前記空気吸入口(12)の下流へ延びる流路部(16)、
前記空気吸入口(12)と前記流路部(16)を介して外気を供給するように設計された供給装置(22)、及び
第一の位置では前記空気吸入口(12)を閉じる流れ制御フラップ(24)を有し、
前記流れ制御フラップ(24)は第二の位置で前記空気吸入口(12)の第一の流れ断面を開き、第三の位置で前記第一の流れ断面より広い第二の流れ断面を開き、前記流れ制御フラップ(24)の前記第二の位置では前記流れ制御フラップ(24)の第一の表面部(28)が前記空気吸入口(12)の領域において前記空気吸入口(12)を囲む航空機外板部(18)と実質的に平行に、かつ実質的に同一平面に調整されるように、及び前記流れ制御フラップ(24)の前記第三の位置では前記流れ制御フラップ(24)の前記第一の表面部(28)が前記空気吸入口(12)の領域において前記空気吸入口(12)を囲む航空機外板部(18)に対して角度をなして調整されるように前記流れ制御フラップ(24)は設計され、設置されたものであることを特徴とする空気路。 - 前記流れ制御フラップ(24)の前記第二の位置では前記流れ制御フラップ(24)の第二の表面部(30)が、前記流路部(16)を流れる外気の流れ方向に前記流路部(16)の前記流れ断面が増加するように、前記流路部(16)の壁部(32)に対して角度をなして調整されるように前記流れ制御フラップ(24)は設計され、設置されたものであることを特徴とする請求項1に記載の空気路。
- 前記流れ制御フラップ(24)の前記第三の位置では前記流れ制御フラップ(24)の前記第二の表面部(30)が前記流路部(16)の前記壁部(32)と実質的に平行に調整されるように前記流れ制御フラップ(24)は設計され、設置されたものであることを特徴とする請求項1又は2に記載の空気路。
- 前記流れ制御フラップ(24)の前記第三の位置では前記流れ制御フラップ(24)の端が前記航空機の周囲の気流に突き出るように前記流れ制御フラップ(24)は設計され、設置されたものであることを特徴とする請求項1乃至請求項3のいずれか1項に記載の空気路。
- 前記流れ制御フラップ(24)は実質的に三角形の断面を有するものであることを特徴とする請求項1乃至請求項4のいずれか1項に記載の空気路。
- 前記流れ制御フラップ(24)は、前記流れ制御フラップ(24)の重心部分に設置される軸(26)の周りを回転可能なものであることを特徴とする請求項1乃至請求項5のいずれか1項に記載の空気路。
- 前記流れ制御フラップ(24)の前記回転軸(26)は実質的に前記流路部(16)へ延びた中心長軸(L)の領域に設置されるものであることを特徴とする請求項6に記載の空気路。
- 前記流れ制御フラップ(24)をその第一の位置と第三の位置の間で無段階に動かすように設計された駆動装置を有するものであること特徴とする請求項1乃至請求項7のいずれか1項に記載の空気路。
- 前記流れ制御フラップ(24)を所望の位置に保持するように設計された保持装置を有するものであること特徴とする請求項1乃至請求項8のいずれか1項に記載の空気路。
- 請求項1乃至請求項9のいずれか1項に記載の空気路を運転する方法であって、
前記空気路(10)を備える航空機の巡航中に、外気を航空機の装置へ供給するための前記流れ制御フラップ(24)をその第二の位置に動かし、前記空気路(10)を備える前記航空機の地上操縦中に、外気を前記航空機の装置へ供給するための前記流れ制御フラップ(24)を第三の位置に動かすことを特徴とする空気路の運転方法。
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US7581408P | 2008-06-26 | 2008-06-26 | |
DE102008030399.2 | 2008-06-26 | ||
DE102008030399.2A DE102008030399B4 (de) | 2008-06-26 | 2008-06-26 | Luftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
US61/075,814 | 2008-06-26 | ||
PCT/EP2009/004513 WO2009156120A2 (de) | 2008-06-26 | 2009-06-23 | Luftkanal zur umgebungsluftzufuhr in einem flugzeug |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2011525452A JP2011525452A (ja) | 2011-09-22 |
JP5358682B2 true JP5358682B2 (ja) | 2013-12-04 |
Family
ID=41396572
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2011515189A Expired - Fee Related JP5358682B2 (ja) | 2008-06-26 | 2009-06-23 | 外気を航空機内に供給するための空気路 |
Country Status (9)
Country | Link |
---|---|
US (1) | US8721406B2 (ja) |
EP (1) | EP2307276B1 (ja) |
JP (1) | JP5358682B2 (ja) |
CN (1) | CN102105358B (ja) |
BR (1) | BRPI0914270A2 (ja) |
CA (1) | CA2729473A1 (ja) |
DE (1) | DE102008030399B4 (ja) |
RU (1) | RU2011101954A (ja) |
WO (1) | WO2009156120A2 (ja) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102008030399B4 (de) * | 2008-06-26 | 2019-03-21 | Airbus Operations Gmbh | Luftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
GB2478978B (en) * | 2010-03-25 | 2012-02-29 | Toshiba Res Europ Ltd | Automated fault reporting in femto cells |
DE102011011879A1 (de) * | 2011-02-21 | 2012-08-23 | Airbus Operations Gmbh | Kühllufteinlass, Triebwerkzapfluftsystem und Verfahren zum Betreiben eines Kühllufteinlasses |
US9017893B2 (en) * | 2011-06-24 | 2015-04-28 | Watt Fuel Cell Corp. | Fuel cell system with centrifugal blower system for providing a flow of gaseous medium thereto |
ES2401015B1 (es) * | 2011-09-29 | 2014-03-13 | Airbus Operations, S.L. | Toma de aire con doble compuerta |
CN103057708B (zh) * | 2011-10-24 | 2015-07-15 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种用于大直径导管固定的调节结构 |
US9051057B2 (en) * | 2011-12-28 | 2015-06-09 | Embraer S.A. | Aircraft air inlet diverter assemblies with improved aerodynamic characteristics |
CN103625646A (zh) * | 2013-08-23 | 2014-03-12 | 中国航空工业集团公司西安飞机设计研究所 | 一种apu进气道风门 |
WO2015054334A1 (en) * | 2013-10-08 | 2015-04-16 | United Technologies Corporation | Acoustic controlled ice deflecting auxiliary power unit inlet system |
US9810147B2 (en) * | 2013-10-31 | 2017-11-07 | The Boeing Company | Angled inlet system for a precooler |
US9803546B2 (en) | 2013-10-31 | 2017-10-31 | The Boeing Company | Dual inlets for a turbofan precooler |
GB2529469A (en) * | 2014-08-22 | 2016-02-24 | Airbus Operations Ltd | Aircraft fuel tank inerting system |
GB2529468A (en) * | 2014-08-22 | 2016-02-24 | Airbus Operations Ltd | Aircraft fuel tank inerting system |
CN104251547B (zh) * | 2014-09-23 | 2017-03-22 | 中国商用飞机有限责任公司 | 用于飞机空调系统的除水装置 |
US9845144B2 (en) * | 2014-10-13 | 2017-12-19 | Gulfstream Aerospace Corporation | Aircraft and air exchange systems for ventilated cavities of aircraft |
US20160146511A1 (en) * | 2014-11-24 | 2016-05-26 | Hamilton Sundstrand Corporation | Heat exchanger assembly for aircraft ecs |
CN105644789B (zh) * | 2014-12-05 | 2017-10-13 | 石家庄飞机工业有限责任公司 | 飞机前冲压进气热交换装置 |
GB201518573D0 (en) | 2015-10-20 | 2015-12-02 | Rolls Royce Plc | Fluid system |
CN107201705B (zh) * | 2016-03-17 | 2023-03-21 | 中国科学院西北生态环境资源研究院 | 一种增进通风管路基通风效能的方法 |
FR3065438A1 (fr) * | 2017-04-25 | 2018-10-26 | Airbus Operations | Systeme de prise d'air multiposition pour un aeronef |
US10266275B1 (en) * | 2018-04-10 | 2019-04-23 | DMS Aviation Services, LLC | Pressure recovery device for an aircraft engine air intake |
CN110513162B (zh) | 2018-05-22 | 2022-06-14 | 通用电气公司 | 斗式入口 |
CA3064652A1 (en) | 2018-12-07 | 2020-06-07 | Pratt & Whitney Canada Corp. | Static take-off port |
CA3132274A1 (en) | 2019-03-01 | 2020-09-10 | Pratt & Whitney Canada Corp. | Circulating coolant fluid in hybrid electrical propulsion systems |
FR3095639B1 (fr) * | 2019-04-30 | 2021-04-02 | Airbus Helicopters | Giravion équipé d’un dispositif aérodynamique comportant carénage présentant une entrée d’air |
US11649064B2 (en) | 2019-08-02 | 2023-05-16 | Hamilton Sundstrand Corporation | Integrated motor drive cooling |
CA3144868A1 (en) | 2021-01-05 | 2022-07-05 | Pratt & Whitney Canada Corp. | Parallel hybrid power plant with hollow motor |
Family Cites Families (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR850267A (ja) * | 1939-12-12 | |||
GB516099A (en) * | 1938-02-14 | 1939-12-21 | Fr Hispano Suiza Soc | Improvements in and relating to engine-driven vehicles, especially aircraft, having radiators for cooling the engines thereof |
US3752422A (en) * | 1971-06-30 | 1973-08-14 | Boeing Co | Jet augmented ram air scoop |
US4174083A (en) | 1977-04-29 | 1979-11-13 | The Boeing Company | Flow deflector for fluid inlet |
US4203566A (en) * | 1978-08-21 | 1980-05-20 | United Aircraft Products, Inc. | Air inlet control for aircraft or the like |
JPS55156800A (en) * | 1979-05-23 | 1980-12-06 | Kawasaki Heavy Ind Ltd | Air inlet port for jet engine of aircraft |
US4307743A (en) * | 1980-10-01 | 1981-12-29 | The Boeing Company | Device to start an overcontracted mixed compression supersonic inlet |
US4667900A (en) * | 1981-03-05 | 1987-05-26 | Kyusik Kim | Ram constriction vane diffuser for jet engine |
DE3444822A1 (de) * | 1984-12-08 | 1986-06-12 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Regelbarer diffusor fuer einen lufteinlauf an einem flugzeug |
US4628954A (en) * | 1985-03-28 | 1986-12-16 | Rachels Industries, Inc. | Multi-use damper |
DE3529463A1 (de) * | 1985-08-16 | 1987-02-26 | Opel Adam Ag | Ausstroemduese an belueftungsvorrichtungen oder klimaanlagen |
US5088660A (en) * | 1989-08-04 | 1992-02-18 | United Technologies Corporation | Bleed stability door |
US5277658A (en) * | 1992-12-21 | 1994-01-11 | Goettl George M | Barometric damper apparatus |
US5603371A (en) * | 1995-06-05 | 1997-02-18 | Gregg; Richard D. | Electronic power angling rod for a window blind |
US5865398A (en) * | 1997-01-14 | 1999-02-02 | Mcdonnell Douglas Corporation | Multi-function engine air inlet control |
FR2763098B1 (fr) * | 1997-05-07 | 1999-06-11 | Snecma | Systeme d'admission d'air dans une veine de turbomachine |
US6050527A (en) * | 1997-12-19 | 2000-04-18 | The Boeing Company | Flow control device to eliminate cavity resonance |
DE19850093C1 (de) * | 1998-10-30 | 2000-05-04 | Daimler Chrysler Aerospace | Lufteinlaß |
US6349899B1 (en) * | 2000-04-04 | 2002-02-26 | The Boeing Company | Aircraft auxiliary air intake with ram and flush opening door |
DE10119433C1 (de) * | 2001-04-20 | 2002-08-22 | Liebherr Aerospace Gmbh | Stauluftkanal für eine Flugzeugklimaanlage |
US20020166923A1 (en) * | 2001-05-08 | 2002-11-14 | Munoz Jules Ricardo | Reduced bleed vapor compression cycle environmental control system for aircraft |
US6634597B2 (en) * | 2002-01-11 | 2003-10-21 | The Boeing Company | Method and apparatus for controlling aircraft airflow |
DE10201426B8 (de) * | 2002-01-16 | 2004-09-02 | Liebherr-Aerospace Lindenberg Gmbh | Klimatisierungssystem |
US6699013B2 (en) * | 2002-05-31 | 2004-03-02 | Quantum Corporation | Forced air cooling fan having pivotal fan blades for unidirectional air flow |
US7198062B2 (en) * | 2002-11-21 | 2007-04-03 | The Boeing Company | Fluid control valve |
US7014144B2 (en) * | 2003-07-22 | 2006-03-21 | Honeywell International, Inc. | Dual action inlet door and method for use thereof |
DE10361722B4 (de) | 2003-12-30 | 2009-06-10 | Airbus Deutschland Gmbh | Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
DE10361657B4 (de) * | 2003-12-30 | 2008-06-26 | Airbus Deutschland Gmbh | Kühlungsluftversorgungssystem für die Kühlung verschiedener Kühlungsluft benötigender Systeme in einem Flugzeug |
JP2006036032A (ja) * | 2004-07-27 | 2006-02-09 | Calsonic Kansei Corp | 自動車用空調装置 |
US7344107B2 (en) * | 2004-10-26 | 2008-03-18 | The Boeing Company | Dual flow APU inlet and associated systems and methods |
US7600713B2 (en) * | 2005-03-04 | 2009-10-13 | Honeywell International Inc. | Pre-hung inlet door system |
US7469545B2 (en) * | 2005-09-27 | 2008-12-30 | Honeywell International Inc. | Auxiliary power unit inlet door position control system and method |
US7540142B2 (en) * | 2006-02-21 | 2009-06-02 | Honeywell International Inc. | Multiple auxiliary power unit system inlet ducts controlled by a single actuator |
US7600714B2 (en) * | 2006-04-20 | 2009-10-13 | Honeywell International Inc. | Diffusing air inlet door assembly |
US7624944B2 (en) * | 2006-10-26 | 2009-12-01 | The Boeing Company | Tandem air inlet apparatus and method for an airborne mobile platform |
US7861968B2 (en) * | 2006-10-26 | 2011-01-04 | The Boeing Company | Air inlet and method for a highspeed mobile platform |
US7618006B2 (en) * | 2006-11-13 | 2009-11-17 | The Boeing Company | Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems |
JP2010513119A (ja) * | 2006-12-21 | 2010-04-30 | エアバス・オペレーションズ・ゲーエムベーハー | ラムエアに基づく航空機用冷却及び換気システム |
US8141816B2 (en) * | 2008-04-30 | 2012-03-27 | Honeywell International Inc. | AFT inlet duct mounted door actuator |
DE102008002116B4 (de) * | 2008-05-30 | 2014-04-10 | Airbus Operations Gmbh | Vorrichtung und Verfahren zur Abluftkühlung von Flugzeugklimaanlagen |
DE102008030399B4 (de) * | 2008-06-26 | 2019-03-21 | Airbus Operations Gmbh | Luftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
US8245976B2 (en) * | 2009-01-19 | 2012-08-21 | The Boeing Company | Door assembly for laminar flow control system |
US8322981B2 (en) * | 2009-03-02 | 2012-12-04 | Hamilton Sundstrand Corporation | Aircraft fluid diversion inlet louver |
-
2008
- 2008-06-26 DE DE102008030399.2A patent/DE102008030399B4/de active Active
-
2009
- 2009-06-23 JP JP2011515189A patent/JP5358682B2/ja not_active Expired - Fee Related
- 2009-06-23 CA CA2729473A patent/CA2729473A1/en not_active Abandoned
- 2009-06-23 WO PCT/EP2009/004513 patent/WO2009156120A2/de active Application Filing
- 2009-06-23 EP EP09768969.9A patent/EP2307276B1/de active Active
- 2009-06-23 US US13/001,353 patent/US8721406B2/en active Active
- 2009-06-23 RU RU2011101954/11A patent/RU2011101954A/ru unknown
- 2009-06-23 CN CN200980128747.2A patent/CN102105358B/zh active Active
- 2009-06-23 BR BRPI0914270A patent/BRPI0914270A2/pt not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
WO2009156120A4 (de) | 2010-05-20 |
JP2011525452A (ja) | 2011-09-22 |
EP2307276A2 (de) | 2011-04-13 |
WO2009156120A3 (de) | 2010-04-01 |
US20110151764A1 (en) | 2011-06-23 |
CA2729473A1 (en) | 2009-12-30 |
DE102008030399B4 (de) | 2019-03-21 |
RU2011101954A (ru) | 2012-08-10 |
CN102105358B (zh) | 2014-05-21 |
WO2009156120A2 (de) | 2009-12-30 |
DE102008030399A1 (de) | 2010-01-07 |
US8721406B2 (en) | 2014-05-13 |
BRPI0914270A2 (pt) | 2015-11-03 |
EP2307276B1 (de) | 2017-08-09 |
CN102105358A (zh) | 2011-06-22 |
WO2009156120A8 (de) | 2010-07-15 |
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