JP2007537084A - 流体管システムを有する航空機 - Google Patents
流体管システムを有する航空機 Download PDFInfo
- Publication number
- JP2007537084A JP2007537084A JP2007512087A JP2007512087A JP2007537084A JP 2007537084 A JP2007537084 A JP 2007537084A JP 2007512087 A JP2007512087 A JP 2007512087A JP 2007512087 A JP2007512087 A JP 2007512087A JP 2007537084 A JP2007537084 A JP 2007537084A
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- cabin
- fluid
- valve
- pipe system
- 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.)
- Granted
Links
- 239000012530 fluid Substances 0.000 title claims abstract description 31
- 238000005086 pumping Methods 0.000 claims abstract description 4
- 238000002347 injection Methods 0.000 claims description 17
- 239000007924 injection Substances 0.000 claims description 17
- 230000006835 compression Effects 0.000 claims description 5
- 238000007906 compression Methods 0.000 claims description 5
- 238000000605 extraction Methods 0.000 description 6
- 108010066057 cabin-1 Proteins 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 239000000284 extract Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000033228 biological regulation Effects 0.000 description 1
- 230000000740 bleeding effect Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 108010066114 cabin-2 Proteins 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
- B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
- B64C21/025—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- Cleaning In General (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Paper (AREA)
- Pipeline Systems (AREA)
Abstract
【選択図】図1
Description
2 逆止弁
3 噴射ポンプ
4 噴出弁
5 抽気弁
6 停止弁
7 制御ユニット
8 圧縮空気管
9 保護弁
10 駆動噴射
10 排出管
14、15、16 切替可能弁4、5、6に対する制御線
18 20内の開口
19 相互連結管
20 航空機の外板
22 航空機エンジン
25 抽気管
26 流体管システム
28 圧縮設備
Claims (7)
- 外板の不安定箇所で流体の層流層を抽出し及び/又は流体を噴出させる流体管システムを有する航空機であって、
該流体管システム(26、19、18)は、切替可能弁(6)を用いて、キャビンの排出空気によって駆動されて層流層を抽出するための所望の減圧を発生させるポンプ設備(3)に連結することができる航空機。 - 前記ポンプ設備は噴射ポンプ(3)であり、該噴射ポンプの駆動噴射(10)は前記キャビンからの排出空気によって形成される請求項1に記載の航空機。
- 前記流体管システムは、噴出用の超過圧力を得るために、切替可能弁(4、5、6)を用いて、航空機エンジン(22)からの圧縮空気(8、25)を誘導する導管及び/又は追加の圧縮設備(28)に連結することができる請求項1又は2に記載の航空機。
- 前記圧縮空気は高温空気として具現化される請求項3に記載の航空機。
- 飛行状態パラメータ、キャビン圧力、周囲パラメータ(温度T、圧力P)、及び航空機エンジン(22)の動作パラメータBLのような入力パラメータに応じて、切替可能弁(4、5、6)を、制御線(14、15、16)を用いて作動させる制御ユニット(7)又は調整ユニットが設けられた請求項1、2、3又は4に記載の航空機。
- 切替可能弁(4、5、6)の通路の断面を調整することができる請求項1、2、3、4又は5に記載の航空機。
- キャビン(1)から前記噴射ポンプ(3)に誘導する排出管(12)内に、空気がキャビンに流入するのを防止する逆止弁(2)が配置された請求項1、2、3、4、5又は6に記載の航空機。
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004024057.4 | 2004-05-13 | ||
DE102004024057A DE102004024057B3 (de) | 2004-05-13 | 2004-05-13 | Luftfahrzeug mit einem Fluidkanalsystem |
US60666804P | 2004-09-02 | 2004-09-02 | |
US60/606,668 | 2004-09-02 | ||
PCT/EP2005/005097 WO2005113334A1 (en) | 2004-05-13 | 2005-05-11 | Aircraft with a fluid-duct-system |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2007537084A true JP2007537084A (ja) | 2007-12-20 |
JP4989463B2 JP4989463B2 (ja) | 2012-08-01 |
Family
ID=34854137
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007512087A Expired - Fee Related JP4989463B2 (ja) | 2004-05-13 | 2005-05-11 | 流体管システムを有する航空機 |
Country Status (10)
Country | Link |
---|---|
US (1) | US7988102B2 (ja) |
EP (1) | EP1744952B1 (ja) |
JP (1) | JP4989463B2 (ja) |
CN (1) | CN1950253A (ja) |
AT (1) | ATE402070T1 (ja) |
BR (1) | BRPI0510562A (ja) |
CA (1) | CA2563571C (ja) |
DE (2) | DE102004024057B3 (ja) |
RU (1) | RU2389648C2 (ja) |
WO (1) | WO2005113334A1 (ja) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1966044B1 (en) | 2005-12-20 | 2009-08-05 | North-West University | Controlling the boundary layer of an airfoil |
DE102006028167A1 (de) * | 2006-06-16 | 2007-12-20 | Daubner & Stommel Gbr Bau-Werk-Planung | Verfahren zum Betreiben einer zumindest einen fluiddynamischen Auftriebskörper aufweisenden Vorrichtung, insbesondere einer Windenergieanlage |
DE102008019146A1 (de) | 2008-04-16 | 2009-11-05 | Airbus Deutschland Gmbh | Enteisungssystem für ein Flugzeug |
DE102009039769A1 (de) * | 2009-09-02 | 2011-03-17 | Airbus Operations Gmbh | Strömungskörper, Stellklappe oder Hauptflügel oder Flosse eines Flugzeugs sowie Strukturbauteil mit einem solchen Strömungskörper |
DE102009057405A1 (de) * | 2009-12-08 | 2011-06-09 | Airbus Operations Gmbh | Flugzeug mit einer Anordnung von Strömungsbeeinflussungs-Vorrichtungen |
FR2968634B1 (fr) * | 2010-12-08 | 2013-08-02 | Snecma | Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees |
US8776835B2 (en) | 2012-12-05 | 2014-07-15 | Hamilton Sundstrand Corporation | Fluid duct with improved connecting bead |
AU2016338382B2 (en) * | 2015-09-02 | 2021-04-01 | Jetoptera, Inc. | Ejector and airfoil configurations |
DE102019102634B3 (de) | 2019-02-04 | 2020-01-09 | Airbus Defence and Space GmbH | Anordnung zur mechanischen Veränderung einer Oberfläche sowie System und Luftfahrzeug mit einer solchen Anordnung |
CN111017198B (zh) * | 2019-12-24 | 2023-05-23 | 中国航空工业集团公司西安飞机设计研究所 | 一种用于高空飞行飞机机翼混合层流流动控制的吊舱 |
CN111806700B (zh) * | 2020-07-08 | 2023-04-07 | 中国商用飞机有限责任公司 | 适用于飞机的空调组件舱的通风系统及包括其的飞机 |
PL437531A1 (pl) * | 2021-04-06 | 2022-10-10 | Sieć Badawcza Łukasiewicz-Instytut Lotnictwa | Układ i sposób aktywnego sterowania przepływem na powierzchni aerodynamicznej |
WO2024006164A1 (en) * | 2022-06-27 | 2024-01-04 | Melcher Thomas W | Industrial aerial robot systems and methods |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04110299A (ja) * | 1989-12-29 | 1992-04-10 | Boeing Co:The | 航空機用着氷防止装置 |
JPH05139385A (ja) * | 1991-11-19 | 1993-06-08 | Mitsubishi Heavy Ind Ltd | 航空機の抵抗低減装置 |
US5884873A (en) * | 1996-05-04 | 1999-03-23 | Daimler-Benz Aerospace Airbus Gmbh | Suction generator system in an aircraft for maintaining a laminar boundary flow |
JP2000203495A (ja) * | 1999-01-18 | 2000-07-25 | Shimadzu Corp | 航空機の環境制御装置 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2575541A (en) * | 1948-06-26 | 1951-11-20 | Northrop Aircraft Inc | Airplane cabin cooling system |
US3423011A (en) * | 1967-01-10 | 1969-01-21 | Bell Aerospace Corp | Jet pump |
US3752422A (en) * | 1971-06-30 | 1973-08-14 | Boeing Co | Jet augmented ram air scoop |
DE3412101A1 (de) * | 1984-03-31 | 1985-10-10 | Deutsche Airbus GmbH, 8000 München | Einbauanordnung eines hilfstriebwerkes im rumpfheck von transportflugzeugen zur wirtschaftlichen erzeugung von klimaluft und von vortriebsschub im flug |
US5143329A (en) * | 1990-06-01 | 1992-09-01 | General Electric Company | Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
US5348256A (en) * | 1992-05-13 | 1994-09-20 | The Boeing Company | Supersonic aircraft and method |
RU2084377C1 (ru) | 1992-11-02 | 1997-07-20 | Александр Николаевич Гришин | Силовая установка летательного аппарата с системой ламинаризации обтекания аэродинамических поверхностей |
DE4320302C2 (de) * | 1993-06-18 | 1996-09-12 | Daimler Benz Aerospace Airbus | Anordnung zur Energiegewinnung an Bord eines Flugzeuges, insbesondere eines Passagierflugzeuges |
US6128896A (en) * | 1998-01-14 | 2000-10-10 | Saiz; Manuel Munoz | Aircraft air conditioner energy recovery device |
US5967461A (en) * | 1997-07-02 | 1999-10-19 | Mcdonnell Douglas Corp. | High efficiency environmental control systems and methods |
DE19820097C2 (de) * | 1998-05-06 | 2003-02-13 | Airbus Gmbh | Anordnung zur Grenzschichtabsaugung und Stoßgrenzschichtkontrolle für ein Flugzeug |
ES2149120B1 (es) * | 1998-12-22 | 2001-06-01 | Saiz Manuel Munoz | Dispositivo recuperador de la energia del aire acondicionado de los aviones. |
-
2004
- 2004-05-13 DE DE102004024057A patent/DE102004024057B3/de not_active Expired - Fee Related
-
2005
- 2005-05-11 BR BRPI0510562-5A patent/BRPI0510562A/pt not_active IP Right Cessation
- 2005-05-11 AT AT05741832T patent/ATE402070T1/de not_active IP Right Cessation
- 2005-05-11 US US11/596,134 patent/US7988102B2/en not_active Expired - Fee Related
- 2005-05-11 RU RU2006142769/11A patent/RU2389648C2/ru not_active IP Right Cessation
- 2005-05-11 CN CNA2005800143841A patent/CN1950253A/zh active Pending
- 2005-05-11 EP EP05741832A patent/EP1744952B1/en not_active Not-in-force
- 2005-05-11 DE DE602005008420T patent/DE602005008420D1/de active Active
- 2005-05-11 JP JP2007512087A patent/JP4989463B2/ja not_active Expired - Fee Related
- 2005-05-11 CA CA2563571A patent/CA2563571C/en not_active Expired - Fee Related
- 2005-05-11 WO PCT/EP2005/005097 patent/WO2005113334A1/en active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04110299A (ja) * | 1989-12-29 | 1992-04-10 | Boeing Co:The | 航空機用着氷防止装置 |
JPH05139385A (ja) * | 1991-11-19 | 1993-06-08 | Mitsubishi Heavy Ind Ltd | 航空機の抵抗低減装置 |
US5884873A (en) * | 1996-05-04 | 1999-03-23 | Daimler-Benz Aerospace Airbus Gmbh | Suction generator system in an aircraft for maintaining a laminar boundary flow |
JP2000203495A (ja) * | 1999-01-18 | 2000-07-25 | Shimadzu Corp | 航空機の環境制御装置 |
Also Published As
Publication number | Publication date |
---|---|
RU2389648C2 (ru) | 2010-05-20 |
WO2005113334A1 (en) | 2005-12-01 |
US7988102B2 (en) | 2011-08-02 |
CN1950253A (zh) | 2007-04-18 |
DE602005008420D1 (de) | 2008-09-04 |
DE102004024057B3 (de) | 2005-09-15 |
US20090008505A1 (en) | 2009-01-08 |
BRPI0510562A (pt) | 2007-11-20 |
EP1744952A1 (en) | 2007-01-24 |
CA2563571A1 (en) | 2005-12-01 |
JP4989463B2 (ja) | 2012-08-01 |
EP1744952B1 (en) | 2008-07-23 |
ATE402070T1 (de) | 2008-08-15 |
CA2563571C (en) | 2014-02-11 |
RU2006142769A (ru) | 2008-06-20 |
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