JP2010524763A - 飛行機の揚力部材を胴体に固定する装置 - Google Patents
飛行機の揚力部材を胴体に固定する装置 Download PDFInfo
- Publication number
- JP2010524763A JP2010524763A JP2010503559A JP2010503559A JP2010524763A JP 2010524763 A JP2010524763 A JP 2010524763A JP 2010503559 A JP2010503559 A JP 2010503559A JP 2010503559 A JP2010503559 A JP 2010503559A JP 2010524763 A JP2010524763 A JP 2010524763A
- Authority
- JP
- Japan
- Prior art keywords
- fuselage
- wing structure
- airplane
- joint
- wing
- 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
- 230000033001 locomotion Effects 0.000 claims abstract description 12
- 230000008878 coupling Effects 0.000 description 9
- 238000010168 coupling process Methods 0.000 description 9
- 238000005859 coupling reaction Methods 0.000 description 9
- 229920001971 elastomer Polymers 0.000 description 7
- 239000000806 elastomer Substances 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000000712 assembly Effects 0.000 description 2
- 238000000429 assembly Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 238000003475 lamination Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 238000004904 shortening Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Tires In General (AREA)
- Connection Of Plates (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Axle Suspensions And Sidecars For Cycles (AREA)
- Vehicle Body Suspensions (AREA)
- Toys (AREA)
- Transmission Devices (AREA)
Abstract
Description
− 弾性ジョイントが積層ジョイントである
− 前記ジョイントの長手軸が飛行機の長手方向軸に対して横方向に延びるように前記ジョイントの向きが決められる
− 揚力部材が飛行機の翼構造である
− 弾性ジョイントにより胴体の右サイドおよび左サイドが翼構造のうちの右翼および左翼にそれぞれ結合される
− 翼構造が胴体上で低位置にある
− 弾性ジョイントにより胴体の中央長手方向ビームが翼構造のセンター・ボックスに結合される
− 翼が胴体上で高位置にある
− 翼構造が一体構造である、すなわち翼および翼構造のセンター・ボックスが一続きで作製された後に胴体に固定される
−揚力部材が前記飛行機の水平尾翼である
4 リーフ; 5 第1のエラストマー層; 6 第2のエラストマー層;
8 胴体; 9 翼構造; 10,11 翼; 12 センター・ボックス;
13 凹部; 14 アッパー・サイド・レッジ; 15 側面壁。
Claims (9)
- 直線移動時および回転時の剛性が軸方向(X)、垂直方向(Z)および横方向(Y)にパラメータ化可能である弾性ジョイント(1)を含む、揚力部材(9)を胴体(8)に固定する少なくとも1つの装置を具備すること、および
弾性ジョイントが積層ジョイントであること
を特徴とする飛行機。 - ジョイントの長手方向軸(A)が飛行機の長手方向軸(X)に対して横方向に延びるように前記ジョイントの向きが決められることを特徴とする請求項1に記載の飛行機。
- 揚力部材が翼構造(9)であることを特徴とする請求項1または2に記載の飛行機。
- 弾性ジョイントにより胴体の右サイドおよび左サイドが翼構造のうちの右翼および左翼(10、11)にそれぞれ結合されることを特徴とする請求項3に記載の飛行機。
- 翼構造が胴体上で低位置にあることを特徴とする請求項3または4に記載の飛行機。
- 弾性ジョイントにより胴体の中央長手方向ビーム(16)が翼構造のセンター・ボックスに結合されることを特徴とする請求項5に記載の飛行機。
- 翼が胴体上で高位置にあることを特徴とする請求項3または4に記載の飛行機。
- 翼構造が一体構造であることを特徴とする請求項3から7のいずれか一項に記載の飛行機。
- 揚力部材が前記飛行機の水平尾翼であることを特徴とする請求項1から8のいずれか一項に記載の飛行機。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0754529A FR2915173B1 (fr) | 2007-04-17 | 2007-04-17 | Dispositif de fixation d'un organe de sustentation au fuselage d'un avion. |
FR0754529 | 2007-04-17 | ||
PCT/FR2008/050668 WO2008145892A1 (fr) | 2007-04-17 | 2008-04-15 | Dispositif de fixation d'un organe de sustentation au fuselage d'un avion |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2010524763A true JP2010524763A (ja) | 2010-07-22 |
JP5427771B2 JP5427771B2 (ja) | 2014-02-26 |
Family
ID=38653266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2010503559A Expired - Fee Related JP5427771B2 (ja) | 2007-04-17 | 2008-04-15 | 飛行機の揚力部材を胴体に固定する装置 |
Country Status (10)
Country | Link |
---|---|
US (1) | US8544789B2 (ja) |
EP (1) | EP2137065B1 (ja) |
JP (1) | JP5427771B2 (ja) |
CN (1) | CN101663197B (ja) |
AT (1) | ATE555983T1 (ja) |
BR (1) | BRPI0810474A2 (ja) |
CA (1) | CA2683596C (ja) |
FR (1) | FR2915173B1 (ja) |
RU (1) | RU2415774C1 (ja) |
WO (1) | WO2008145892A1 (ja) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7398586B2 (en) * | 2005-11-01 | 2008-07-15 | The Boeing Company | Methods and systems for manufacturing a family of aircraft wings and other composite structures |
US8016236B2 (en) * | 2007-04-04 | 2011-09-13 | The Boeing Company | Method and apparatus for attaching a wing to a body |
US7887009B2 (en) * | 2007-12-05 | 2011-02-15 | The Boeing Company | Methods and systems for attaching aircraft wings to fuselages |
FR2946008B1 (fr) | 2009-05-28 | 2012-12-28 | Airbus France | Aeronef comprenant des traverses de support de plancher |
FR2962409B1 (fr) * | 2010-07-09 | 2012-09-21 | Airbus Operations Sas | Procede de realisation d'un caisson central de voilure |
FR2966425B1 (fr) | 2010-10-26 | 2013-08-16 | Eurocopter France | Aeronef muni d'un empennage comprenant un moyen de lutte contre le flottement aeroelastique. |
US9180956B1 (en) | 2012-04-11 | 2015-11-10 | The Boeing Company | Methods and apparatus for attaching an aircraft wing assembly to an aircraft body |
US8857765B2 (en) * | 2012-10-16 | 2014-10-14 | The Boeing Company | Method and apparatus for attaching an aircraft fuselage frame to a wing box |
US9399508B2 (en) * | 2013-10-09 | 2016-07-26 | The Boeing Company | Aircraft wing-to-fuselage joint with active suspension and method |
US9315254B2 (en) * | 2013-10-11 | 2016-04-19 | The Boeing Company | Joint assembly and method of assembling same |
US20190276157A1 (en) * | 2018-03-08 | 2019-09-12 | Bell Helicopter Textron Inc. | Flexible radial inlet plenum |
US11136107B2 (en) | 2018-10-05 | 2021-10-05 | The Boeing Company | Method and apparatus for attaching a fuselage frame to a wing box |
US11787523B2 (en) * | 2021-01-06 | 2023-10-17 | The Boeing Company | Aircraft keel beam assembly |
FR3130753A1 (fr) * | 2021-12-17 | 2023-06-23 | Airbus Operations (S.A.S.) | Aéronef comprenant au moins un meuble système relié par au moins un système de liaison à un rail d’un plancher |
Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR801893A (fr) * | 1936-02-14 | 1936-08-20 | Montage élastique pour la liaison de divers éléments d'un avion | |
FR859103A (fr) * | 1939-03-30 | 1940-12-11 | Dispositif pneumatique de raccordement des ailes au fuselage des avions | |
JPS5673700U (ja) * | 1979-11-12 | 1981-06-16 | ||
US4390153A (en) * | 1979-08-11 | 1983-06-28 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Apparatus for securing a wing to the body of a craft |
FR2645930A1 (fr) * | 1989-04-15 | 1990-10-19 | Btr Plc | Bague elastique |
JPH02275127A (ja) * | 1989-04-15 | 1990-11-09 | Btr Plc | 弾性ブッシュ |
EP0483049A1 (en) * | 1990-10-23 | 1992-04-29 | United Technologies Corporation | An improved clevis joint capable of accommodating substantial pivotal motion between its joined members and loading along its axis |
JPH04321488A (ja) * | 1991-04-22 | 1992-11-11 | Mitsubishi Heavy Ind Ltd | 航空機の非対称剛性翼 |
CA2121823A1 (en) * | 1994-04-21 | 1995-10-22 | Paul Wesley Dawson | Soft wing suspension |
US7887009B2 (en) * | 2007-12-05 | 2011-02-15 | The Boeing Company | Methods and systems for attaching aircraft wings to fuselages |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2584666A (en) * | 1944-03-11 | 1952-02-05 | George E Bockrath | Aircraft gust alleviating control means |
US2584667A (en) * | 1947-02-14 | 1952-02-05 | George E Bockrath | Gust alleviating control means for airplanes |
US3529790A (en) * | 1969-02-18 | 1970-09-22 | Gen Dynamics Corp | Means for changing wing incidence for varying angles of attack |
US4247061A (en) * | 1978-07-12 | 1981-01-27 | United Technologies Corporation | Helicopter with stabilator detuned in antisymmetric vibration modes from main rotor wake excitation frequency |
-
2007
- 2007-04-17 FR FR0754529A patent/FR2915173B1/fr not_active Expired - Fee Related
-
2008
- 2008-04-15 EP EP08788184A patent/EP2137065B1/fr not_active Not-in-force
- 2008-04-15 RU RU2009142224/11A patent/RU2415774C1/ru not_active IP Right Cessation
- 2008-04-15 JP JP2010503559A patent/JP5427771B2/ja not_active Expired - Fee Related
- 2008-04-15 US US12/595,261 patent/US8544789B2/en not_active Expired - Fee Related
- 2008-04-15 CN CN200880012305.7A patent/CN101663197B/zh not_active Expired - Fee Related
- 2008-04-15 CA CA2683596A patent/CA2683596C/fr not_active Expired - Fee Related
- 2008-04-15 BR BRPI0810474-3A2A patent/BRPI0810474A2/pt not_active IP Right Cessation
- 2008-04-15 AT AT08788184T patent/ATE555983T1/de active
- 2008-04-15 WO PCT/FR2008/050668 patent/WO2008145892A1/fr active Application Filing
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR801893A (fr) * | 1936-02-14 | 1936-08-20 | Montage élastique pour la liaison de divers éléments d'un avion | |
FR859103A (fr) * | 1939-03-30 | 1940-12-11 | Dispositif pneumatique de raccordement des ailes au fuselage des avions | |
US4390153A (en) * | 1979-08-11 | 1983-06-28 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Apparatus for securing a wing to the body of a craft |
JPS5673700U (ja) * | 1979-11-12 | 1981-06-16 | ||
FR2645930A1 (fr) * | 1989-04-15 | 1990-10-19 | Btr Plc | Bague elastique |
JPH02275127A (ja) * | 1989-04-15 | 1990-11-09 | Btr Plc | 弾性ブッシュ |
EP0483049A1 (en) * | 1990-10-23 | 1992-04-29 | United Technologies Corporation | An improved clevis joint capable of accommodating substantial pivotal motion between its joined members and loading along its axis |
JPH04321488A (ja) * | 1991-04-22 | 1992-11-11 | Mitsubishi Heavy Ind Ltd | 航空機の非対称剛性翼 |
CA2121823A1 (en) * | 1994-04-21 | 1995-10-22 | Paul Wesley Dawson | Soft wing suspension |
US7887009B2 (en) * | 2007-12-05 | 2011-02-15 | The Boeing Company | Methods and systems for attaching aircraft wings to fuselages |
Also Published As
Publication number | Publication date |
---|---|
CA2683596A1 (fr) | 2008-12-04 |
BRPI0810474A2 (pt) | 2014-11-18 |
EP2137065A1 (fr) | 2009-12-30 |
FR2915173A1 (fr) | 2008-10-24 |
US20100200691A1 (en) | 2010-08-12 |
EP2137065B1 (fr) | 2012-05-02 |
JP5427771B2 (ja) | 2014-02-26 |
CA2683596C (fr) | 2013-02-26 |
CN101663197B (zh) | 2015-10-21 |
US8544789B2 (en) | 2013-10-01 |
ATE555983T1 (de) | 2012-05-15 |
FR2915173B1 (fr) | 2009-10-23 |
RU2415774C1 (ru) | 2011-04-10 |
CN101663197A (zh) | 2010-03-03 |
WO2008145892A1 (fr) | 2008-12-04 |
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