JP6376667B2 - 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 - Google Patents

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 Download PDF

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Publication number
JP6376667B2
JP6376667B2 JP2015549585A JP2015549585A JP6376667B2 JP 6376667 B2 JP6376667 B2 JP 6376667B2 JP 2015549585 A JP2015549585 A JP 2015549585A JP 2015549585 A JP2015549585 A JP 2015549585A JP 6376667 B2 JP6376667 B2 JP 6376667B2
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tail boom
tail
modified
boom
surface profile
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JP2016506335A (ja
JP2016506335A5 (enExample
Inventor
ロバート ジェイ デスロシュ
ロバート ジェイ デスロシュ
Original Assignee
ビーエルアール エアロスペース リミテッド ライアビリティ カンパニー
ビーエルアール エアロスペース リミテッド ライアビリティ カンパニー
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8245Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft using air jets
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49616Structural member making
    • Y10T29/49622Vehicular structural member making

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Catching Or Destruction (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Mobile Radio Communication Systems (AREA)
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 JP2016506335A5 (enExample) 2017-02-09
JP6376667B2 true 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
EP3317180B1 (en) 2015-07-02 2021-09-01 BLR Aerospace, LLC Helicopter with anti-torque system, related kit and methods
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

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US4200252A (en) 1977-12-21 1980-04-29 Summa Corporation Helicopter antitorque system using circulation control
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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
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USD425853S (en) 1998-04-17 2000-05-30 Finmeccanica S.P.A. Helicopter
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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
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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
EP2595881B1 (en) 2010-09-20 2016-09-07 Bell Helicopter Textron Inc. Airfoil shaped tail boom
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Also Published As

Publication number Publication date
EP2935002B1 (en) 2019-03-20
ES2731631T3 (es) 2019-11-18
WO2014123627A3 (en) 2014-10-23
JP2016506335A (ja) 2016-03-03
KR20150097685A (ko) 2015-08-26
KR102144145B1 (ko) 2020-08-12
US20140166804A1 (en) 2014-06-19
EP2935002A4 (en) 2016-02-24
US8991747B2 (en) 2015-03-31
EP2935002A2 (en) 2015-10-28
WO2014123627A2 (en) 2014-08-14

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