JP4657192B2 - 飛行機の主翼構造 - Google Patents
飛行機の主翼構造 Download PDFInfo
- Publication number
- JP4657192B2 JP4657192B2 JP2006302637A JP2006302637A JP4657192B2 JP 4657192 B2 JP4657192 B2 JP 4657192B2 JP 2006302637 A JP2006302637 A JP 2006302637A JP 2006302637 A JP2006302637 A JP 2006302637A JP 4657192 B2 JP4657192 B2 JP 4657192B2
- Authority
- JP
- Japan
- Prior art keywords
- wiring
- piping
- main wing
- spar
- pylon
- 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.)
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Links
- 230000004308 accommodation Effects 0.000 claims description 27
- 239000002828 fuel tank Substances 0.000 claims description 13
- 238000005192 partition Methods 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 description 2
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 2
- 239000000446 fuel Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000002452 interceptive effect 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/32—Wings specially adapted for mounting power plant
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
Description
論文 AIAA 2003−2530(Design and Development of the HondaJet) 藤野 道格 Honda R&D Americas,Inc. 2003年7月
12 主翼
13 パイロン
14 エンジン
17 メインスパー(スパー)
17a,17b 第2の配線・配管案内孔
18 フロントスパー(スパー)
18a,18b 第2の配線・配管案内孔
19 リヤスパー(スパー)
20A〜20I リブ
21 アッパースキン
22 ロアスキン
21a,21b 第1の配線・配管案内孔
23 前縁スキン
28 着陸装置収容室
32 着陸装置
34A,34B 配線・配管収容室
35A〜35D 燃料タンク
37 配線
38 配管
Claims (2)
- 主翼(12)の上面または下面にパイロン(13)を介してエンジン(14)を支持した飛行機の主翼構造において、
主翼(12)の内部にスパン方向に延びる複数のスパー(17,18,19)とコード方向に延びる複数のリブ(20A〜20I)とによって複数の領域を区画し、前記パイロン(13)の主翼取付部から前縁スキン(23)の内部空間に連なる所定の領域をエンジン(14)と胴体(11)とを接続する配線(37)や配管(38)を集約して収容する配線・配管収容室(34A,34B)とし、前記配線・配管収容室(34A,34B)の一部に隣接する所定の領域を着陸装置(32)を収容する着陸装置収容室(28)とし、前記配線・配管収容室(34A,34B)の他の一部に隣接する所定の領域を燃料タンク(35A〜35D)としたことを特徴とする飛行機の主翼構造。 - 主翼(12)の上面または下面に配置された前記パイロン(13)の主翼取付部に対応する主翼(12)のアッパースキン(21)またはロアスキン(22)に前記配線(37)や配管(38)が通過する第1の配線・配管案内孔(21a,21b)を形成するとともに、前記配線・配管収容室(34A,34B)を区画あるいは横切るスパー(17,18)に前記配線(37)や配管(38)が通過する第2の配線・配管案内孔(17a,17b;18a,18b)を形成したことを特徴とする、請求項1に記載の飛行機の主翼構造。
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006302637A JP4657192B2 (ja) | 2006-11-08 | 2006-11-08 | 飛行機の主翼構造 |
US11/978,717 US7938360B2 (en) | 2006-11-08 | 2007-10-30 | Main wing structure of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006302637A JP4657192B2 (ja) | 2006-11-08 | 2006-11-08 | 飛行機の主翼構造 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2008120108A JP2008120108A (ja) | 2008-05-29 |
JP4657192B2 true JP4657192B2 (ja) | 2011-03-23 |
Family
ID=39505374
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2006302637A Active JP4657192B2 (ja) | 2006-11-08 | 2006-11-08 | 飛行機の主翼構造 |
Country Status (2)
Country | Link |
---|---|
US (1) | US7938360B2 (ja) |
JP (1) | JP4657192B2 (ja) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2942772B1 (fr) * | 2009-03-03 | 2012-09-28 | Airbus France | Procede pour l'amelioration des performances d'un aeronef |
US8991191B2 (en) * | 2009-11-24 | 2015-03-31 | General Electric Company | Thermally actuated passive gas turbine engine compartment venting |
ES2391967B1 (es) * | 2010-01-14 | 2013-10-10 | Airbus Operations, S.L. | Pilón de soporte de motores de aeronaves. |
FR3059981A1 (fr) * | 2016-12-14 | 2018-06-15 | Airbus Operations | Aeronef comportant une structure commune pour supporter un groupe propulseur et un element de train d'atterrissage |
EP4059834A1 (en) * | 2021-03-17 | 2022-09-21 | The Boeing Company | Electrical pass-through assembly for traversing a structure |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1850012A (en) * | 1930-06-03 | 1932-03-15 | Ford Motor Co | Airplane |
GB546794A (en) * | 1941-06-28 | 1942-07-30 | Constant Speed Airscrews Ltd | Improvements in fuel and oil tanks for aircraft |
US3579215A (en) * | 1966-09-26 | 1971-05-18 | Denis R Brasket | Method and apparatus for conducting a signal |
US4624425A (en) * | 1984-05-23 | 1986-11-25 | Michael Austin | Fixed wing light aircraft |
JPS63135479A (ja) * | 1986-11-14 | 1988-06-07 | コートタウルズ アエロスペース, インコーポレイテッド | 貯蔵容器およびその密封方法 |
US5000400A (en) * | 1989-12-15 | 1991-03-19 | The Boeing Company | Four-post wing-stowed main landing gear for high speed aircraft |
EP0941922A1 (en) * | 1996-10-07 | 1999-09-15 | Xinyun Wang | Prestressed structure for aircraft and the method of producing the same |
US6923403B1 (en) * | 2004-03-18 | 2005-08-02 | Faruk Dizdarevic | Tailed flying wing aircraft |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2397184A (en) * | 1940-10-31 | 1946-03-26 | Cons Vultee Aircraft Corp | Fuel container |
US2372143A (en) * | 1943-03-17 | 1945-03-20 | Budd Edward G Mfg Co | Airfoil nose construction |
US2514105A (en) * | 1945-12-07 | 1950-07-04 | Thomas Wilfred | Airfoil conditioning means |
US2613893A (en) * | 1948-04-01 | 1952-10-14 | Curtiss Wright Corp | Airfoil construction |
US2995320A (en) * | 1958-04-14 | 1961-08-08 | Eldon W Gottschalk | Supersonic aircraft having extensible nose cone |
US3067968A (en) * | 1958-12-29 | 1962-12-11 | Heppenstall Charles William | Retractable jet engine noise suppressor |
GB1294324A (en) * | 1969-05-03 | 1972-10-25 | Dowty Rotol Ltd | Engine installations |
GB1328410A (en) * | 1969-11-29 | 1973-08-30 | Ver Flugtechnische Werke | Aircraft engine mounting means |
US4481703A (en) * | 1980-02-25 | 1984-11-13 | Rockwell International Corporation | Method of making rib structures for an airfoil |
US5484121A (en) * | 1993-11-12 | 1996-01-16 | Padawer; Jacques | Icing detector for aircraft surfaces |
US5921502A (en) * | 1996-06-19 | 1999-07-13 | Cox & Company, Inc. | Hybrid ice-protection system for use on roughness-sensitive airfoils |
-
2006
- 2006-11-08 JP JP2006302637A patent/JP4657192B2/ja active Active
-
2007
- 2007-10-30 US US11/978,717 patent/US7938360B2/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1850012A (en) * | 1930-06-03 | 1932-03-15 | Ford Motor Co | Airplane |
GB546794A (en) * | 1941-06-28 | 1942-07-30 | Constant Speed Airscrews Ltd | Improvements in fuel and oil tanks for aircraft |
US3579215A (en) * | 1966-09-26 | 1971-05-18 | Denis R Brasket | Method and apparatus for conducting a signal |
US4624425A (en) * | 1984-05-23 | 1986-11-25 | Michael Austin | Fixed wing light aircraft |
JPS63135479A (ja) * | 1986-11-14 | 1988-06-07 | コートタウルズ アエロスペース, インコーポレイテッド | 貯蔵容器およびその密封方法 |
US5000400A (en) * | 1989-12-15 | 1991-03-19 | The Boeing Company | Four-post wing-stowed main landing gear for high speed aircraft |
EP0941922A1 (en) * | 1996-10-07 | 1999-09-15 | Xinyun Wang | Prestressed structure for aircraft and the method of producing the same |
US6923403B1 (en) * | 2004-03-18 | 2005-08-02 | Faruk Dizdarevic | Tailed flying wing aircraft |
Also Published As
Publication number | Publication date |
---|---|
US20080149761A1 (en) | 2008-06-26 |
JP2008120108A (ja) | 2008-05-29 |
US7938360B2 (en) | 2011-05-10 |
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