JP6486201B2 - 翼、フラップおよび航空機 - Google Patents
翼、フラップおよび航空機 Download PDFInfo
- Publication number
- JP6486201B2 JP6486201B2 JP2015108517A JP2015108517A JP6486201B2 JP 6486201 B2 JP6486201 B2 JP 6486201B2 JP 2015108517 A JP2015108517 A JP 2015108517A JP 2015108517 A JP2015108517 A JP 2015108517A JP 6486201 B2 JP6486201 B2 JP 6486201B2
- Authority
- JP
- Japan
- Prior art keywords
- flap
- vortex
- wing
- tip
- blade tip
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/20—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
- B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
-
- 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)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2015108517A JP6486201B2 (ja) | 2015-05-28 | 2015-05-28 | 翼、フラップおよび航空機 |
| US15/577,055 US10562606B2 (en) | 2015-05-28 | 2016-04-14 | Wing, flap, and aircraft |
| EP16799702.2A EP3305656B1 (en) | 2015-05-28 | 2016-04-14 | Wing, flap, and aircraft |
| PCT/JP2016/061970 WO2016189994A1 (ja) | 2015-05-28 | 2016-04-14 | 翼、フラップおよび航空機 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2015108517A JP6486201B2 (ja) | 2015-05-28 | 2015-05-28 | 翼、フラップおよび航空機 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2016222043A JP2016222043A (ja) | 2016-12-28 |
| JP2016222043A5 JP2016222043A5 (OSRAM) | 2018-04-12 |
| JP6486201B2 true JP6486201B2 (ja) | 2019-03-20 |
Family
ID=57394056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015108517A Active JP6486201B2 (ja) | 2015-05-28 | 2015-05-28 | 翼、フラップおよび航空機 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US10562606B2 (OSRAM) |
| EP (1) | EP3305656B1 (OSRAM) |
| JP (1) | JP6486201B2 (OSRAM) |
| WO (1) | WO2016189994A1 (OSRAM) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3241742B1 (en) * | 2016-05-06 | 2018-12-12 | Airbus Operations S.L. | Aircraft empennage |
| EP3666642A1 (en) * | 2018-12-10 | 2020-06-17 | Bombardier Inc. | Aircraft wing assemblies |
| US11111003B2 (en) * | 2019-05-17 | 2021-09-07 | The Boeing Company | Aeroseal and method of forming the same |
| CN112660363B (zh) * | 2020-12-31 | 2024-06-07 | 中国商用飞机有限责任公司 | 一种飞机襟翼 |
| CN114750931A (zh) * | 2022-04-14 | 2022-07-15 | 中国空气动力研究与发展中心空天技术研究所 | 一种无人机前襟翼舵面结构 |
| CN116424544B (zh) * | 2023-06-14 | 2023-08-15 | 清华大学 | 飞机襟翼 |
| CN119460084A (zh) * | 2024-11-29 | 2025-02-18 | 陕西飞机工业有限责任公司 | 一种飞机机头降噪涡流发生器装置 |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3578264A (en) * | 1968-07-09 | 1971-05-11 | Battelle Development Corp | Boundary layer control of flow separation and heat exchange |
| US3596854A (en) * | 1969-06-09 | 1971-08-03 | William R Haney Jr | Vortex generator for airfoil structures |
| JPS5433498A (en) | 1977-08-20 | 1979-03-12 | Masaaki Kusano | Method of producing high lift |
| US4477042A (en) * | 1981-01-19 | 1984-10-16 | Griswold Ii Roger W | Vortex alleviating wing tip |
| US4655419A (en) * | 1984-12-31 | 1987-04-07 | The Boeing Company | Vortex generator |
| JPH01285492A (ja) | 1988-05-12 | 1989-11-16 | Mitsubishi Heavy Ind Ltd | 翼端渦打消し翼 |
| JPH04103495A (ja) * | 1990-08-21 | 1992-04-06 | Mitsubishi Heavy Ind Ltd | ボルテクス・ジェネレータ |
| US6105904A (en) * | 1998-03-30 | 2000-08-22 | Orbital Research Inc. | Deployable flow control device |
| CA2622938C (en) | 2005-12-28 | 2010-11-09 | National University Corporation Nagoya University | Smart vortex generator and aircraft, vessel and rotary machine being equipped with the same |
| DE102007059455A1 (de) | 2007-12-10 | 2009-06-25 | Airbus Deutschland Gmbh | Flügelspitzenverlängerung zur Reduktion von Wirbelschleppen bei Flugzeugen |
| US20110006165A1 (en) * | 2009-07-10 | 2011-01-13 | Peter Ireland | Application of conformal sub boundary layer vortex generators to a foil or aero/ hydrodynamic surface |
| JP5286527B2 (ja) * | 2009-07-13 | 2013-09-11 | 三菱重工業株式会社 | 高揚力発生装置、翼および高揚力発生装置の騒音低減装置 |
| US8434723B2 (en) * | 2010-06-01 | 2013-05-07 | Applied University Research, Inc. | Low drag asymmetric tetrahedral vortex generators |
| BR112013025160B1 (pt) * | 2011-03-30 | 2021-06-15 | The Society Of Japanese Aerospace Companies | Dispositivo de hipersustentação para uma aeronave |
| US8632031B2 (en) | 2011-04-11 | 2014-01-21 | The Boeing Company | Systems and methods for attenuation of noise and wakes produced by aircraft |
| US20130037657A1 (en) * | 2011-07-09 | 2013-02-14 | Ramgen Power Systems, Llc | Vortex generators |
-
2015
- 2015-05-28 JP JP2015108517A patent/JP6486201B2/ja active Active
-
2016
- 2016-04-14 US US15/577,055 patent/US10562606B2/en active Active
- 2016-04-14 WO PCT/JP2016/061970 patent/WO2016189994A1/ja not_active Ceased
- 2016-04-14 EP EP16799702.2A patent/EP3305656B1/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| WO2016189994A1 (ja) | 2016-12-01 |
| EP3305656A4 (en) | 2019-02-06 |
| US20180170521A1 (en) | 2018-06-21 |
| JP2016222043A (ja) | 2016-12-28 |
| EP3305656B1 (en) | 2021-03-31 |
| US10562606B2 (en) | 2020-02-18 |
| EP3305656A1 (en) | 2018-04-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6486201B2 (ja) | 翼、フラップおよび航空機 | |
| US8061652B2 (en) | Rudder of a commercial aircraft | |
| US8651813B2 (en) | Fluid dynamic body having escapelet openings for reducing induced and interference drag, and energizing stagnant flow | |
| US8240125B2 (en) | Thrust vectoring system and method | |
| US10953982B2 (en) | Rotorcraft including auxiliary propulsor positioned to ingest boundary layer flow | |
| JP6569303B2 (ja) | フラップおよび航空機 | |
| EP2979974A1 (en) | Submerged vortex generator | |
| CN108001669A (zh) | 一种基于零质量射流控制的前缘缝翼噪声抑制方法 | |
| US6854687B1 (en) | Nacelle integration with reflexed wing for sonic boom reduction | |
| US20110186679A1 (en) | Aircraft with at least two propeller drives arranged at a distance from one another in the span width direction of the wings | |
| WO2011099276A1 (ja) | 高揚力発生装置、翼、スラット | |
| JP5286527B2 (ja) | 高揚力発生装置、翼および高揚力発生装置の騒音低減装置 | |
| JP5214025B2 (ja) | 固定部及び可動部を有する航空機のフィレット・フェアリング、及び関連システム及び方法 | |
| CN109415121B (zh) | 在其后区中具有突起的飞行器转子叶片套筒及具有此套筒的转子 | |
| JP5046115B2 (ja) | 舵面端騒音低減デバイス | |
| Murayama et al. | Computational Study on Noise From Natural Laminar Flow Infinite Wing With Krueger Flap and Comparison to Slat Noise | |
| US20240253769A1 (en) | Leading-edge high-lift device, wing, aircraft, and buffering member | |
| Murayama et al. | Computational Study on Track Noise From Infinite Wing with Leading-Edge Krueger Flap | |
| JP7249883B2 (ja) | 航空機の主翼および航空機 | |
| Keller | Numerical investigation of engine effects on the stability and controllability of a transport aircraft with circulation control | |
| JP2010228598A (ja) | 翼胴結合部騒音低減デバイス | |
| Allaei et al. | High Lift Device Modifications for Reducing Airport Noise-A Review |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20180221 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20180221 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20190212 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20190219 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 6486201 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |