JP2016506335A5 - - Google Patents

Download PDF

Info

Publication number
JP2016506335A5
JP2016506335A5 JP2015549585A JP2015549585A JP2016506335A5 JP 2016506335 A5 JP2016506335 A5 JP 2016506335A5 JP 2015549585 A JP2015549585 A JP 2015549585A JP 2015549585 A JP2015549585 A JP 2015549585A JP 2016506335 A5 JP2016506335 A5 JP 2016506335A5
Authority
JP
Japan
Prior art keywords
tail boom
tail
surface profile
modified
modifying
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
Application number
JP2015549585A
Other languages
English (en)
Japanese (ja)
Other versions
JP2016506335A (ja
JP6376667B2 (ja
Filing date
Publication date
Priority claimed from US13/871,710 external-priority patent/US8991747B2/en
Application filed filed Critical
Publication of JP2016506335A publication Critical patent/JP2016506335A/ja
Publication of JP2016506335A5 publication Critical patent/JP2016506335A5/ja
Application granted granted Critical
Publication of JP6376667B2 publication Critical patent/JP6376667B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2015549585A 2012-12-18 2013-12-17 航空機安定化システム及びそれにより航空機を修正する方法 Active JP6376667B2 (ja)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201261738663P 2012-12-18 2012-12-18
US61/738,663 2012-12-18
US13/871,710 US8991747B2 (en) 2012-12-18 2013-04-26 Aircraft stabilization systems and methods of modifying an aircraft with the same
US13/871,710 2013-04-26
PCT/US2013/075783 WO2014123627A2 (en) 2012-12-18 2013-12-17 Aircraft stabilization systems and methods of modifying an aircraft with the same

Publications (3)

Publication Number Publication Date
JP2016506335A JP2016506335A (ja) 2016-03-03
JP2016506335A5 true JP2016506335A5 (enExample) 2017-02-09
JP6376667B2 JP6376667B2 (ja) 2018-08-22

Family

ID=50929804

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015549585A Active JP6376667B2 (ja) 2012-12-18 2013-12-17 航空機安定化システム及びそれにより航空機を修正する方法

Country Status (6)

Country Link
US (1) US8991747B2 (enExample)
EP (1) EP2935002B1 (enExample)
JP (1) JP6376667B2 (enExample)
KR (1) KR102144145B1 (enExample)
ES (1) ES2731631T3 (enExample)
WO (1) WO2014123627A2 (enExample)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3023827B1 (fr) * 2014-07-16 2017-12-29 Airbus Helicopters Poutre de queue de giravion, et giravion
CN104859864A (zh) * 2015-04-03 2015-08-26 南京航空航天大学 一种直升机旋翼流场显示介质发生、存储及输运装置
EP3909848B1 (en) 2015-07-02 2023-12-20 BLR Aerospace, LLC Helicopter and method of manufacturing a helicopter
CN110654569B (zh) * 2019-09-29 2022-01-07 中国直升机设计研究所 一种直升机尾段疲劳试验载荷模拟简化方法
CN115783323B (zh) * 2022-12-08 2023-10-20 常州大学怀德学院 一种遥感成像的航拍无人机

Family Cites Families (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1893064A (en) 1931-04-03 1933-01-03 Zap Dev Company Aircraft
US2338935A (en) 1937-08-16 1944-01-11 Hafner Raoul Helicorter
US2626766A (en) 1947-09-09 1953-01-27 Firestone Tire & Rubber Co Rotor arrangement for singlerotor helicopters
US2674421A (en) 1948-09-25 1954-04-06 Cenzo Herbert A De Jet-driven rotary wing arrangement for jet propelled convertible aircraft
US2862361A (en) 1952-05-16 1958-12-02 United Aircraft Corp Fluid coupling
US2959373A (en) 1954-12-10 1960-11-08 Daniel R Zuck Convertiplane
US3540680A (en) 1968-05-24 1970-11-17 Lockheed Aircraft Corp Dual rotor system for helicopters
US3807662A (en) 1972-11-13 1974-04-30 Lockheed Aircraft Corp Anti-torque, propulsion, and directional control system
US3966145A (en) 1975-02-28 1976-06-29 The Boeing Company Structure for cooling helicopter tail rotor gearbox
US4200252A (en) 1977-12-21 1980-04-29 Summa Corporation Helicopter antitorque system using circulation control
US4227665A (en) 1978-05-11 1980-10-14 Textron, Inc. Fixed leading edge slat spoiler for a horizontal stabilizer
USD278227S (en) 1980-08-05 1985-04-02 Bell Helicopter Textron Inc. Helicopter
DE3371771D1 (en) * 1982-07-05 1987-07-02 Westland Plc Helicopter
US4542868A (en) 1983-06-06 1985-09-24 Lockheed Corporation Trailing edge device for an airfoil
US4708305A (en) 1987-01-30 1987-11-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter anti-torque system using fuselage strakes
US4948068A (en) 1988-05-12 1990-08-14 Mcdonnell Douglas Corporation Circulation control slots in helicopter yaw control system
IL101069A (en) 1991-02-25 1996-09-12 Valsan Partners Purchase N Y A system for increasing the fuel efficiency of an aircraft and a kit for changing aircraft wings
US5209430A (en) 1991-11-07 1993-05-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter low-speed yaw control
DE69420603T2 (de) 1993-03-13 1999-12-30 Gkn Westland Helicopters Ltd., Yeovil Drehbare Blätter
USD425853S (en) 1998-04-17 2000-05-30 Finmeccanica S.P.A. Helicopter
US6352220B1 (en) 2000-06-02 2002-03-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof
AU2002237648A1 (en) 2000-10-10 2002-05-21 The Regents Of The University Of California Microfabricated translational stages for control of aerodynamic loading
GB0115130D0 (en) 2001-06-21 2001-08-15 Bae Systems Plc A winglet
JP2003212192A (ja) * 2002-01-18 2003-07-30 Nishimura Mutsuko 回転翼機における方向安定システム
RU2238221C2 (ru) * 2002-12-04 2004-10-20 Открытое акционерное общество "Казанский вертолётный завод" Вертолет и способ управления одновинтовым вертолетом
US20050116116A1 (en) 2003-11-11 2005-06-02 Supersonic Aerospace International, Llc Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
FR2862941B1 (fr) 2003-11-27 2007-02-23 Airbus France Procede permettant d'eviter les vibrations d'une gouverne de direction d'un aeronef et aeronef mettant en oeuvre ce procede
US6869045B1 (en) 2004-03-11 2005-03-22 Boudary Layer Research, Inc. Helicopter tail section and retrofit method
RU2281226C1 (ru) * 2005-03-23 2006-08-10 Открытое Акционерное Общество "Московский Вертолетный Завод Им. М.Л. Миля" Устройство дополнительной компенсации реактивного момента несущего винта одновинтового вертолета
US20090302167A1 (en) 2006-08-23 2009-12-10 Desroche Robert J Apparatus and method for use on aircraft with spanwise flow inhibitors
US8074926B2 (en) 2006-12-22 2011-12-13 Calvin Burgess Structural dynamic stability for an aircraft
WO2008156533A2 (en) 2007-05-14 2008-12-24 Blr Aerospace L.L.C. Aircraft stabilizer system and methods of using the same
JP2009045976A (ja) * 2007-08-16 2009-03-05 Mitsubishi Heavy Ind Ltd テールブーム
DE102008015073B4 (de) * 2008-03-19 2014-02-13 Eurocopter Deutschland Gmbh Hubschrauber mit Mitteln zur aerodynamischen Unterstützung des Drehmomentausgleichs
US8840058B2 (en) 2010-09-20 2014-09-23 Textron Innovations Inc. Airfoil shaped tail boom
WO2012039702A1 (en) * 2010-09-20 2012-03-29 Bell Helicopter Textron Inc. Airfoil shaped tail boom
EP2511177B1 (en) 2011-04-11 2013-06-05 Eurocopter Deutschland GmbH Helicopter with cycloidal rotor system

Similar Documents

Publication Publication Date Title
JP2016506335A5 (enExample)
NZ713226A (en) Vertical axis water/wind turbine motor using flight feather opening/closing wing system
FR2970699B1 (fr) Avion motorise a structure mixte hydrodynamique et aerodynamique pour le decollage et l'atterrissage sur l'eau, le sol ou la neige
CN204489176U (zh) 一种无尾飞翼布局飞机的阻力方向舵
WO2017027112A3 (en) Helicopter with anti-torque system, related kit and methods
EP2644502A3 (en) Enhanced performance rotorcraft rotor blade
CN105564632A (zh) 一种高升力自然层流翼型
WO2013134331A3 (en) Reversible camber soft wing sail
EA201001783A2 (ru) Роторная платформа аэродинамической силы и способ образования аэродинамической силы
CN103991540B (zh) 一种锥形旋转扑翼飞行器
JP6376667B2 (ja) 航空機安定化システム及びそれにより航空機を修正する方法
CN204726671U (zh) 一种高效风扇翼
CN205022848U (zh) 机翼减速挡板控制装置
CN202953169U (zh) 一种民用客机的新型匙形融合式翼梢小翼
CN104097770B (zh) 一种直升机主转翼用翼片
CN104002968B (zh) 一种小型锥形旋转扑翼飞行器
CN105620723A (zh) 一种襟副翼
CN104192294B (zh) 机翼结构及飞机
CN203854832U (zh) 一种可变攻角式t 型翼
CN202280643U (zh) 一种导叶器阀体结构
CN102642612A (zh) 飞机全弦长副翼
CN106240799A (zh) 一种提高带锯齿后掠翼跨声速横向飞行品质的机翼
CN203371114U (zh) 用于剪切宽窄钢板的剪刃
CN204937472U (zh) 一种针对于低速飞机的翼型
WO2014163724A3 (en) An aircraft wing