JP2010036890A5 - - Google Patents
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- Publication number
- JP2010036890A5 JP2010036890A5 JP2009136315A JP2009136315A JP2010036890A5 JP 2010036890 A5 JP2010036890 A5 JP 2010036890A5 JP 2009136315 A JP2009136315 A JP 2009136315A JP 2009136315 A JP2009136315 A JP 2009136315A JP 2010036890 A5 JP2010036890 A5 JP 2010036890A5
- Authority
- JP
- Japan
- Prior art keywords
- duct
- cross
- lip
- section
- ducted fan
- 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
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/187,172 | 2008-08-06 | ||
| US12/187,172 US8240597B2 (en) | 2008-08-06 | 2008-08-06 | UAV ducted fan lip shaping |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2010036890A JP2010036890A (ja) | 2010-02-18 |
| JP2010036890A5 true JP2010036890A5 (enExample) | 2012-05-31 |
| JP5580552B2 JP5580552B2 (ja) | 2014-08-27 |
Family
ID=41198816
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2009136315A Expired - Fee Related JP5580552B2 (ja) | 2008-08-06 | 2009-06-05 | 無人航空機(uav)ダクテッドファンのリップ成形 |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US8240597B2 (enExample) |
| EP (1) | EP2151381B1 (enExample) |
| JP (1) | JP5580552B2 (enExample) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120234984A1 (en) * | 2008-08-06 | 2012-09-20 | Honeywell International Inc. | Integrated Duct Design for an Unmanned Aerial Vehicle |
| US8543265B2 (en) * | 2008-10-20 | 2013-09-24 | Honeywell International Inc. | Systems and methods for unmanned aerial vehicle navigation |
| JP5645421B2 (ja) | 2010-02-23 | 2014-12-24 | キヤノン株式会社 | 超音波画像装置および遅延制御方法 |
| US8821123B2 (en) * | 2010-03-08 | 2014-09-02 | The Penn State Research Foundation | Double-ducted fan |
| SG2013004940A (en) * | 2013-01-21 | 2014-08-28 | Singapore Tech Aerospace Ltd | Method for improving crosswind stability of a propeller duct and a corresponding apparatus, system and computer readable medium |
| US10107196B2 (en) | 2014-08-08 | 2018-10-23 | Thomas International, Inc. | Adjustable size inlet system |
| BE1022965B1 (nl) * | 2015-04-21 | 2016-10-24 | Airobot | Samenstel voor onbemand luchtvaartuig, onbemand luchtvaartuig met het samenstel, en werkwijze voor het aansturen ervan |
| US10814966B2 (en) | 2015-05-25 | 2020-10-27 | Dotterel Technologies Limited | Shroud for an aircraft |
| US10676183B2 (en) * | 2016-05-13 | 2020-06-09 | Bell Helicopter Textron Inc. | Forward folding rotor blades |
| CN115303485B (zh) * | 2016-08-08 | 2026-03-10 | 克莱奥机器人公司 | 无人机和用于控制无人机的系统 |
| EP3366586B1 (en) | 2017-02-27 | 2020-08-19 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | A thrust producing unit with at least two rotor assemblies and a shrouding |
| JP2020530913A (ja) | 2017-07-24 | 2020-10-29 | ドテレル テクノロジーズ リミテッド | シュラウド |
| USD862361S1 (en) * | 2018-04-16 | 2019-10-08 | FanFlyer Inc. | Ducted fan flying machine |
| AU2019271730B2 (en) | 2018-05-16 | 2024-09-26 | Dotterel Technologies Limited | Systems and methods for audio capture |
| US11427306B2 (en) | 2019-03-20 | 2022-08-30 | The Boeing Company | Piezoelectric thrust vector control for dual-mode unmanned aerial vehicle |
| WO2021076250A2 (en) * | 2019-09-11 | 2021-04-22 | Alexandru Balan | 360° advanced rotation system |
| CN113859578B (zh) * | 2021-10-13 | 2024-05-14 | 西北工业大学 | 一种可减弱地面涡的工艺进气道及其设计方法 |
| CN114802735A (zh) * | 2022-04-07 | 2022-07-29 | 朱磊 | 一种用于垂直起降飞机的旋翼涵道 |
| US12145753B2 (en) * | 2022-08-09 | 2024-11-19 | Pete Bitar | Compact and lightweight drone delivery device called an ArcSpear electric jet drone system having an electric ducted air propulsion system and being relatively difficult to track in flight |
| WO2024117891A1 (en) | 2022-12-02 | 2024-06-06 | Topspin Robotics, Sia | An unmanned aerial vehicle with a variable gap duct unit |
Family Cites Families (49)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3127093A (en) * | 1964-03-31 | Ducted sustaining rotor for aircraft | ||
| US2996269A (en) * | 1956-04-12 | 1961-08-15 | Charles B Bolton | Helicopter with counter-rotating propeller |
| US3103327A (en) * | 1956-04-12 | 1963-09-10 | Charles B Bolton | Helicopter control system |
| US3108764A (en) * | 1961-09-18 | 1963-10-29 | Helipod Inc | Forward thrust means for ducted rotor sustained aircraft |
| US3167273A (en) | 1962-04-20 | 1965-01-26 | Calderon Alberto Alvarez | Stability and control system and apparatus for ducted fan aircraft |
| US3249323A (en) | 1962-04-25 | 1966-05-03 | Piasecki Aircraft Corp | Closure for vtol aircraft |
| US3559922A (en) | 1967-11-01 | 1971-02-02 | Eugene M Gluhareff | Flying platform construction |
| US3456902A (en) | 1967-11-27 | 1969-07-22 | Fioravante Visconti | Wingless vtol aircraft |
| US3524611A (en) * | 1968-07-22 | 1970-08-18 | Kurt Frank | Controllable air duct for vertical and short take-off and landing type of air vehicle |
| GB1382809A (en) | 1971-12-04 | 1975-02-05 | Rolls Royce | Air intakes for gas turbine engines |
| SE450480B (sv) * | 1982-08-30 | 1987-06-29 | Tech Gerete Und Entwicklungsge | Styvvingad flygkropp |
| US5152478A (en) * | 1990-05-18 | 1992-10-06 | United Technologies Corporation | Unmanned flight vehicle including counter rotating rotors positioned within a toroidal shroud and operable to provide all required vehicle flight controls |
| US5131604A (en) | 1991-04-11 | 1992-07-21 | United Technologies Corporation | Helicopter antitorque device |
| US5108044A (en) | 1991-04-11 | 1992-04-28 | United Technologies Corporation | Shroud-fin integration shelf for a helicopter empennage structure |
| US5150857A (en) | 1991-08-13 | 1992-09-29 | United Technologies Corporation | Shroud geometry for unmanned aerial vehicles |
| US5295643A (en) | 1992-12-28 | 1994-03-22 | Hughes Missile Systems Company | Unmanned vertical take-off and landing, horizontal cruise, air vehicle |
| RU2012512C1 (ru) * | 1993-09-07 | 1994-05-15 | Фирма "ВИСТ" | Комбинированный летательный аппарат |
| US5575438A (en) | 1994-05-09 | 1996-11-19 | United Technologies Corporation | Unmanned VTOL ground surveillance vehicle |
| US5890441A (en) | 1995-09-07 | 1999-04-06 | Swinson Johnny | Horizontal and vertical take off and landing unmanned aerial vehicle |
| US5695153A (en) | 1995-11-16 | 1997-12-09 | Northrop Grumman Corporation | Launcher system for an unmanned aerial vehicle |
| US5746390A (en) | 1996-03-20 | 1998-05-05 | Fran Rich Chi Associates, Inc. | Air-land vehicle with ducted fan vanes providing improved performance |
| US6089505A (en) * | 1997-07-22 | 2000-07-18 | Mcdonnell Douglas Corporation | Mission adaptive inlet |
| US6604706B1 (en) | 1998-08-27 | 2003-08-12 | Nicolae Bostan | Gyrostabilized self propelled aircraft |
| JP2003512215A (ja) | 1998-12-11 | 2003-04-02 | モラー・インターナショナル・インコーポレーテッド | ロボット制御または遠隔制御飛行プラットフォーム用の安定制御装置 |
| US6848649B2 (en) | 2000-10-03 | 2005-02-01 | Charles Gilpin Churchman | V/STOL biplane aircraft |
| GB2372019A (en) | 2001-02-10 | 2002-08-14 | Rolls Royce Plc | Turbofan engine negatively scarfed nacelle for uniform flow to the fan |
| US6464166B1 (en) | 2001-05-29 | 2002-10-15 | Romeo Yankee Ltd. | Ducted fan vehicles particularly useful as VTOL aircraft |
| US6691949B2 (en) | 2001-07-06 | 2004-02-17 | The Charles Stark Draper Laboratory, Inc. | Vertical takeoff and landing aerial vehicle |
| US6721646B2 (en) | 2001-09-27 | 2004-04-13 | Ernest A. Carroll | Unmanned aircraft with automatic fuel-to-air mixture adjustment |
| US6886776B2 (en) | 2001-10-02 | 2005-05-03 | Karl F. Milde, Jr. | VTOL personal aircraft |
| US7032861B2 (en) | 2002-01-07 | 2006-04-25 | Sanders Jr John K | Quiet vertical takeoff and landing aircraft using ducted, magnetic induction air-impeller rotors |
| US20040094662A1 (en) | 2002-01-07 | 2004-05-20 | Sanders John K. | Vertical tale-off landing hovercraft |
| US6666403B1 (en) | 2002-02-11 | 2003-12-23 | Robert E. Follensbee | Force-producing apparatus |
| CN1662419A (zh) | 2002-06-28 | 2005-08-31 | Vtol技术有限公司 | 管道式气流动力设备 |
| ITTO20030588A1 (it) | 2003-07-30 | 2005-01-31 | Fiat Ricerche | Macchina volante. |
| US7857253B2 (en) | 2003-10-27 | 2010-12-28 | Urban Aeronautics Ltd. | Ducted fan VTOL vehicles |
| DE202004017679U1 (de) | 2004-11-15 | 2006-03-23 | Dolmar Gmbh | Anlaufbremse für eine Heckenschere |
| US7658346B2 (en) | 2005-02-25 | 2010-02-09 | Honeywell International Inc. | Double ducted hovering air-vehicle |
| US7556218B2 (en) * | 2005-03-15 | 2009-07-07 | Entecho Pty Ltd. | Aerodynamic lifting device and airborne craft |
| US7520466B2 (en) | 2005-03-17 | 2009-04-21 | Nicolae Bostan | Gyro-stabilized air vehicle |
| US7748486B2 (en) | 2005-06-09 | 2010-07-06 | Honeywell International, Inc. | Landing gear for a hovercraft |
| US20070228214A1 (en) | 2005-09-26 | 2007-10-04 | Honeywell International Inc. | Autonomous launch pad for micro air vehicles |
| US7469725B2 (en) | 2006-02-22 | 2008-12-30 | Honeywell International Inc. | Method and apparatus for accurately delivering a predetermined amount of fuel to a vehicle |
| US7841563B2 (en) | 2006-03-27 | 2010-11-30 | Honeywell International Inc. | Ducted fan air data system |
| US20070244608A1 (en) | 2006-04-13 | 2007-10-18 | Honeywell International Inc. | Ground control station for UAV |
| US20070262195A1 (en) | 2006-05-11 | 2007-11-15 | Robert Bulaga | UAV With Control and Stability System |
| US8387911B2 (en) | 2008-07-25 | 2013-03-05 | Honeywell International Inc. | Ducted fan core for use with an unmanned aerial vehicle |
| US20120234984A1 (en) | 2008-08-06 | 2012-09-20 | Honeywell International Inc. | Integrated Duct Design for an Unmanned Aerial Vehicle |
| US20120153087A1 (en) | 2008-08-06 | 2012-06-21 | Honeywell International Inc. | Modular Pods for Use with an Unmanned Aerial Vehicle |
-
2008
- 2008-08-06 US US12/187,172 patent/US8240597B2/en not_active Expired - Fee Related
-
2009
- 2009-06-03 EP EP09161872.8A patent/EP2151381B1/en not_active Not-in-force
- 2009-06-05 JP JP2009136315A patent/JP5580552B2/ja not_active Expired - Fee Related
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