JP4897830B2 - 航空機のための気流により駆動するよう構成したラムエアタービンおよびエネルギー変換器を有する非常用電源ユニット - Google Patents
航空機のための気流により駆動するよう構成したラムエアタービンおよびエネルギー変換器を有する非常用電源ユニット Download PDFInfo
- Publication number
- JP4897830B2 JP4897830B2 JP2008551715A JP2008551715A JP4897830B2 JP 4897830 B2 JP4897830 B2 JP 4897830B2 JP 2008551715 A JP2008551715 A JP 2008551715A JP 2008551715 A JP2008551715 A JP 2008551715A JP 4897830 B2 JP4897830 B2 JP 4897830B2
- Authority
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- Japan
- Prior art keywords
- emergency power
- aircraft
- power supply
- supply unit
- air turbine
- 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
- 230000000903 blocking effect Effects 0.000 claims description 30
- 239000003570 air Substances 0.000 description 88
- 238000009434 installation Methods 0.000 description 9
- 230000008859 change Effects 0.000 description 7
- 239000011295 pitch Substances 0.000 description 4
- 239000000446 fuel Substances 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 239000012080 ambient air Substances 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000035939 shock Effects 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
- B64D41/00—Power installations for auxiliary purposes
- B64D41/007—Ram air turbines
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2220/00—Application
- F05B2220/70—Application in combination with
- F05B2220/706—Application in combination with an electrical generator
-
- 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
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
-
- 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
- Y02T50/40—Weight reduction
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Turbines (AREA)
- Fluid-Pressure Circuits (AREA)
- Stand-By Power Supply Arrangements (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Description
2 ラムエアタービン
3 駆動軸
4 エネルギー変換器
5 ケーシング
6 流路
7 翼
8 着陸用フラップレールカバー
9 エア流入口
10 エアロフォイル(翼)の前縁部
11 遮断部材(エア流入口側)
12 回動ポイント
13 方向矢印
14 気流
15 エア流出口
16 遮断部材(エア流出口側)
17 エア流出口
18 エア流入口
19 エア流出口
20 エア流出口
21 遮断部材
22 遮断部材
23 遮断部材
24 遮断部材
25 流入路
26 流入路
27 流出路
28 流出路
29 フローコーン
30 フローコーン
Claims (9)
- 航空機の非常用電源ユニット(1)であって、
気流(14)により駆動するよう構成し、流路(6)を形成するケーシング(5)によりほぼ同心状に包囲したラムエアタービン(2)と、
非常事態において航空機搭載の油圧系統および電気系統のうち少なくとも一方の機能を少なくとも部分的に維持するため、前記ラムエアタービン(2)によって駆動するよう構成し、また駆動軸(3)により直接前記ラムエアタービン(2)に連結したエネルギー変換器(4)と、
前記航空機の非常用電源ユニット(1)を選択的にスタンバイモードまたは動作モードに切り替えるときに、前記ラムエアタービン(2)の空間的位置が不変となるように、ケーシング(5)内の適切な位置に前記ラムエアタービン(2)を設置する手段と、
前記気流(14)を前記ラムエアタービン(2)に送給することができる少なくとも1個のエア流入口(9;17,18)と、
前記エア流入口(9;17,18)を閉鎖する少なくとも1個の遮断部材(11;21,22)であって、前記航空機の非常用電源ユニット(1)のスタンバイモードにおいて空力特性を最適化するため航空機の外側輪郭に適合可能に構成した、該エア流入口(9;17,18)の遮断部材(11;21,22)と、
エア流出口(15;19,20)と、
を備えた該非常用電源ユニットにおいて、さらに、
前記エア流出口(15;19,20)を閉鎖する遮断部材(16;23,24)であって、前記航空機の非常用電源ユニット(1)のスタンバイモードにおいて空力特性を最適化するため航空機の外側輪郭に適合可能に構成した、該エア流出口(15;19,20)の遮断部材(16;23,24)と、
第1流入路(25)と、及び
第2流入路(26)と
を備え、前記第1及び第2の流入路(25,26)を前記流路(6)に合流させるとともに、前記第1及び第2の流入路(25,26)はそれぞれ前記流路(6)よりも小さい断面を有する構成とした
ことを特徴とする航空機の非常用電源ユニット(1)。 - 請求項1に記載の航空機の非常用電源ユニットにおいて、前記エネルギー変換器(4)は、油圧ポンプおよび発電機のうち少なくとも一方を有するものとしたことを特徴とする、航空機の非常用電源ユニット。
- 請求項1または2に記載の航空機の非常用電源ユニットにおいて、前記エネルギー変換器(4)を、ラムエアタービン(2)一体の部分としたことを特徴とする、航空機の非常用電源ユニット。
- 請求項1〜3に記載の航空機の非常用電源ユニットにおいて、前記第1及び第2の流入路(25,26)を、Y字状に配置したことを特徴とする、航空機の非常用電源ユニット。
- 請求項1〜4に記載の航空機の非常用電源ユニットにおいて、前記流路(6)内の前記気流(14)を前記遮断部材(11,16;21〜24)により制御可能にしたことを特徴とする、航空機の非常用電源ユニット。
- 請求項1〜5に記載の航空機の非常用電源ユニットにおいて、前記遮断部材(11,16;21〜24)を、機械的および/または電気的に遠隔制御により操作可能にしたことを特徴とした、航空機の非常用電源ユニット。
- 請求項1〜6に記載の航空機の非常用電源ユニットにおいて、前記非常用電源ユニット(1)は、航空機翼の下方の着陸用フラップレールカバー(8)内に固定して一体化可能にしたことを特徴とする、航空機の非常用電源ユニット。
- 請求項1〜7に記載の航空機の非常用電源ユニットにおいて、前記非常用電源ユニット(1)は、ウィングボックスの領域における航空機体内部に固定して一体化可能としたことを特徴とする、航空機の非常用電源ユニット。
- 請求項1〜7に記載の航空機の非常用電源ユニットにおいて、前記非常用電源ユニット(1)は、航空機の胴体機首の領域に固定して込み込み可能としたことを特徴とする、航空機の非常用電源ユニット。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006003138.5 | 2006-01-24 | ||
DE102006003138A DE102006003138A1 (de) | 2006-01-24 | 2006-01-24 | Notversorgungsaggregat mit einer durch einen Luftstrom antreibbaren Staudruckturbine und mit einem Energiewandler für Luftfahrzeuge |
PCT/EP2007/000558 WO2007085422A1 (en) | 2006-01-24 | 2007-01-23 | Emergency supply unit with a ram-air turbine adapted to be driven by an air stream and with an energy converter for aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009523659A JP2009523659A (ja) | 2009-06-25 |
JP4897830B2 true JP4897830B2 (ja) | 2012-03-14 |
Family
ID=38171217
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008551715A Expired - Fee Related JP4897830B2 (ja) | 2006-01-24 | 2007-01-23 | 航空機のための気流により駆動するよう構成したラムエアタービンおよびエネルギー変換器を有する非常用電源ユニット |
Country Status (9)
Country | Link |
---|---|
US (1) | US7982328B2 (ja) |
EP (1) | EP1976759B1 (ja) |
JP (1) | JP4897830B2 (ja) |
CN (1) | CN101374724B (ja) |
BR (1) | BRPI0706297A2 (ja) |
CA (1) | CA2630545C (ja) |
DE (2) | DE102006003138A1 (ja) |
RU (1) | RU2402463C2 (ja) |
WO (1) | WO2007085422A1 (ja) |
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FR2913412B1 (fr) * | 2007-03-05 | 2012-12-07 | Airbus France | Container pour le transport aerien de fret et fuselage d'aeronef pour le transport de fret. |
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CN101363410B (zh) * | 2008-09-01 | 2012-08-01 | 黄金伦 | 高空机翼风筝发电装置 |
CN101368545B (zh) * | 2008-10-04 | 2012-05-09 | 黄金伦 | 集成翼发电风筝 |
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2006
- 2006-01-24 DE DE102006003138A patent/DE102006003138A1/de not_active Ceased
-
2007
- 2007-01-23 WO PCT/EP2007/000558 patent/WO2007085422A1/en active Application Filing
- 2007-01-23 JP JP2008551715A patent/JP4897830B2/ja not_active Expired - Fee Related
- 2007-01-23 BR BRPI0706297-4A patent/BRPI0706297A2/pt not_active IP Right Cessation
- 2007-01-23 CN CN2007800034133A patent/CN101374724B/zh not_active Expired - Fee Related
- 2007-01-23 CA CA2630545A patent/CA2630545C/en not_active Expired - Fee Related
- 2007-01-23 EP EP07702967A patent/EP1976759B1/en not_active Not-in-force
- 2007-01-23 DE DE602007013001T patent/DE602007013001D1/de active Active
- 2007-01-23 RU RU2008129177/11A patent/RU2402463C2/ru not_active IP Right Cessation
- 2007-01-23 US US12/161,902 patent/US7982328B2/en not_active Expired - Fee Related
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US2164545A (en) * | 1937-11-13 | 1939-07-04 | Aviat Mfg Corp | Airplane |
DE1032033B (de) * | 1956-07-12 | 1958-06-12 | Plessey Co Ltd | Stauluftturbine als Kraftquelle fuer Hilfsapparate bei einem Gasturbinenflugzeug |
Also Published As
Publication number | Publication date |
---|---|
CA2630545C (en) | 2010-12-07 |
CN101374724B (zh) | 2012-04-04 |
EP1976759A1 (en) | 2008-10-08 |
EP1976759B1 (en) | 2011-03-09 |
US20090026770A1 (en) | 2009-01-29 |
RU2402463C2 (ru) | 2010-10-27 |
WO2007085422B1 (en) | 2007-10-11 |
JP2009523659A (ja) | 2009-06-25 |
US7982328B2 (en) | 2011-07-19 |
DE102006003138A1 (de) | 2007-08-02 |
DE602007013001D1 (de) | 2011-04-21 |
RU2008129177A (ru) | 2010-02-27 |
WO2007085422A1 (en) | 2007-08-02 |
BRPI0706297A2 (pt) | 2011-03-22 |
CA2630545A1 (en) | 2007-08-02 |
CN101374724A (zh) | 2009-02-25 |
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