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JPS6428096A - Vertical stabilizer for aircraft - Google Patents

Vertical stabilizer for aircraft

Info

Publication number
JPS6428096A
JPS6428096A JP18229787A JP18229787A JPS6428096A JP S6428096 A JPS6428096 A JP S6428096A JP 18229787 A JP18229787 A JP 18229787A JP 18229787 A JP18229787 A JP 18229787A JP S6428096 A JPS6428096 A JP S6428096A
Authority
JP
Japan
Prior art keywords
vertical stabilizer
airframe
vertical
axis
aircraft
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.)
Pending
Application number
JP18229787A
Other languages
Japanese (ja)
Inventor
Mitsuru Hamada
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP18229787A priority Critical patent/JPS6428096A/en
Publication of JPS6428096A publication Critical patent/JPS6428096A/en
Pending legal-status Critical Current

Links

Landscapes

  • Consolidation Of Soil By Introduction Of Solidifying Substances Into Soil (AREA)

Abstract

PURPOSE: To change a vertical stabilizer to the optimum fitting angle according to flight conditions by fitting the lower end section of the vertical stabilizer to an airframe rotatably around the axis nearly parallel with the vertical axis of the airframe. CONSTITUTION: The lower end section of a vertical stabilizer 2 is fitted to an airframe 1 rotatably around the axis nearly parallel with the vertical axis in the longitudinal direction of the airframe 1. The vertical stabilizer 2 is rotated to change its fitting angle according to the flight conditions such as the elevation angle and speed of an aircraft, and the optimum effective position of the vertical stabilizer 2 can be provided. The vertical stabilizer 2 itself can be minimized due to its efficiency, radar invisibility can be improved, and drag and airframe height can be reduced.
JP18229787A 1987-07-23 1987-07-23 Vertical stabilizer for aircraft Pending JPS6428096A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP18229787A JPS6428096A (en) 1987-07-23 1987-07-23 Vertical stabilizer for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18229787A JPS6428096A (en) 1987-07-23 1987-07-23 Vertical stabilizer for aircraft

Publications (1)

Publication Number Publication Date
JPS6428096A true JPS6428096A (en) 1989-01-30

Family

ID=16115821

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18229787A Pending JPS6428096A (en) 1987-07-23 1987-07-23 Vertical stabilizer for aircraft

Country Status (1)

Country Link
JP (1) JPS6428096A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010280252A (en) * 2009-06-02 2010-12-16 Keiji Shigemiya Vertical tail of aircraft
JP2013504472A (en) * 2009-09-09 2013-02-07 エアロバイロメント，インコーポレイテッド Elevon control system
GB2565768A (en) * 2017-08-15 2019-02-27 Bae Systems Plc A vehicle
GB2565769A (en) * 2017-08-15 2019-02-27 Bae Systems Plc Actuating system
CN109823514A (en) * 2019-02-02 2019-05-31 北京航空航天大学 A kind of quick detachable tail structure of adjustable established angle
US10703506B2 (en) 2009-09-09 2020-07-07 Aerovironment, Inc. Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube
US10899429B2 (en) 2017-08-15 2021-01-26 Bae Systems Plc Vehicle
US11555672B2 (en) 2009-02-02 2023-01-17 Aerovironment, Inc. Multimode unmanned aerial vehicle

Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11555672B2 (en) 2009-02-02 2023-01-17 Aerovironment, Inc. Multimode unmanned aerial vehicle
US12013212B2 (en) 2009-02-02 2024-06-18 Aerovironment, Inc. Multimode unmanned aerial vehicle
JP2010280252A (en) * 2009-06-02 2010-12-16 Keiji Shigemiya Vertical tail of aircraft
US11577818B2 (en) 2009-09-09 2023-02-14 Aerovironment, Inc. Elevon control system
US11040766B2 (en) 2009-09-09 2021-06-22 Aerovironment, Inc. Elevon control system
US12103678B2 (en) 2009-09-09 2024-10-01 Aerovironment, Inc. Elevon control system
US12043382B2 (en) 2009-09-09 2024-07-23 Aerovironment, Inc. Elevon control system
US10583910B2 (en) 2009-09-09 2020-03-10 Aerovironment, Inc. Elevon control system
US10696375B2 (en) 2009-09-09 2020-06-30 Aerovironment, Inc. Elevon control system
US10703506B2 (en) 2009-09-09 2020-07-07 Aerovironment, Inc. Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube
JP2013504472A (en) * 2009-09-09 2013-02-07 エアロバイロメント，インコーポレイテッド Elevon control system
US11731784B2 (en) 2009-09-09 2023-08-22 Aerovironment, Inc. Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube
US10953976B2 (en) 2009-09-09 2021-03-23 Aerovironment, Inc. Air vehicle system having deployable airfoils and rudder
US10960968B2 (en) 2009-09-09 2021-03-30 Aerovironment, Inc. Elevon control system
US11667373B2 (en) 2009-09-09 2023-06-06 Aerovironment, Inc. Elevon control system
US11319087B2 (en) 2009-09-09 2022-05-03 Aerovironment, Inc. Systems and devices for remotely operated unmanned aerial vehicle report-suppressing launcher with portable RF transparent launch tube
US8985504B2 (en) 2009-09-09 2015-03-24 Tony Shuo Tao Elevon control system
US9108713B2 (en) 2009-09-09 2015-08-18 Aerovironment, Inc. Elevon control system
GB2565768B (en) * 2017-08-15 2022-05-18 Bae Systems Plc A vehicle
GB2565768A (en) * 2017-08-15 2019-02-27 Bae Systems Plc A vehicle
US10899429B2 (en) 2017-08-15 2021-01-26 Bae Systems Plc Vehicle
GB2565769A (en) * 2017-08-15 2019-02-27 Bae Systems Plc Actuating system
CN109823514B (en) * 2019-02-02 2021-01-12 北京航空航天大学 Quick detachable fin structure of adjustable installation angle
CN109823514A (en) * 2019-02-02 2019-05-31 北京航空航天大学 A kind of quick detachable tail structure of adjustable established angle

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