EA200600088A1 - METHODS OF TAKING AND LANDING OF AIRCRAFT - Google Patents

METHODS OF TAKING AND LANDING OF AIRCRAFT

Info

Publication number
EA200600088A1
EA200600088A1 EA200600088A EA200600088A EA200600088A1 EA 200600088 A1 EA200600088 A1 EA 200600088A1 EA 200600088 A EA200600088 A EA 200600088A EA 200600088 A EA200600088 A EA 200600088A EA 200600088 A1 EA200600088 A1 EA 200600088A1
Authority
EA
Eurasian Patent Office
Prior art keywords
aircraft
cable
landing
guide
damping
Prior art date
Application number
EA200600088A
Other languages
Russian (ru)
Other versions
EA009128B1 (en
Inventor
Валентин Афанасьевич Сухолитко
Original Assignee
Валентин Афанасьевич Сухолитко
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 Валентин Афанасьевич Сухолитко filed Critical Валентин Афанасьевич Сухолитко
Publication of EA200600088A1 publication Critical patent/EA200600088A1/en
Publication of EA009128B1 publication Critical patent/EA009128B1/en

Links

Landscapes

  • Ropes Or Cables (AREA)
  • Toys (AREA)

Abstract

Изобретение относится к транспортно-буксировочным авиационным средствам, взаимодействующим с летательными аппаратами (ЛА). Предлагаемый способ взлета включает соединение ЛА с тросом, выпущенным из воздушной гавани, подъем ЛА на высоту его горизонтального полета, включение двигателей ЛА, его разгон и освобождение от троса. Способ посадки включает соединение троса с ЛА при подлете ЛА к воздушной гавани, гашение скорости ЛА путем выпуска и торможения троса и плавное опускание ЛА на поверхность земли. Воздушную гавань размещают выше высоты горизонтального полета ЛА. Со стороны земли к ней крепят направляющую с подвижными на ней приводами, соединенными тросами с захватными устройствами для ЛА. При этом одновременно с разгоном ЛА при взлете выпускают трос из привода, перемещая привод по направляющей. Гашение горизонтальной скорости ЛА при посадке производят, перемещая привод по направляющей. Технический результат изобретения состоит в обеспечении безопасных укороченных взлета и посадки ЛА.The invention relates to a towing aviation means, interacting with aircraft (LA). The proposed take-off method includes connecting the aircraft with a cable released from the air harbor, raising the aircraft to the height of its horizontal flight, turning on the aircraft engines, accelerating it and releasing the cable. The landing method includes connecting the cable with the aircraft when the aircraft approaches the air harbor, damping the speed of the aircraft by releasing and braking the cable and smoothly lowering the aircraft to the ground. The air harbor is located above the height of the horizontal flight of the LA. On the side of the earth, a guide is attached to it with drives driven on it, connected by cables with gripping devices for an aircraft. In this case, simultaneously with the acceleration of the aircraft during takeoff, the cable is released from the actuator, moving the actuator along the guide. The damping of the horizontal speed of the aircraft during landing is made by moving the drive along the guide. The technical result of the invention is to provide a safe shortened takeoff and landing of the aircraft.

EA200600088A 2005-12-12 2005-12-12 Methods of take-off and landing of aerial vehicles EA009128B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005000632 2005-12-12

Publications (2)

Publication Number Publication Date
EA200600088A1 true EA200600088A1 (en) 2007-06-29
EA009128B1 EA009128B1 (en) 2007-10-26

Family

ID=41203601

Family Applications (1)

Application Number Title Priority Date Filing Date
EA200600088A EA009128B1 (en) 2005-12-12 2005-12-12 Methods of take-off and landing of aerial vehicles

Country Status (1)

Country Link
EA (1) EA009128B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112937897A (en) * 2020-12-25 2021-06-11 北京泊松技术有限公司 Engine for cylinder-shooting unmanned aerial vehicle and shooting method

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB123833A (en) * 1918-03-09 1919-03-10 Eustace Henry Tennyso Eyncourt Improvements in Means for Starting the Flight of Aeroplanes, Seaplanes and the like.
US1680473A (en) * 1927-11-23 1928-08-14 Parker Orin Aeroplane landing and launching device
US1792738A (en) * 1928-02-07 1931-02-17 Hall Engineering & Aircraft Co Aircraft
US1912723A (en) * 1931-03-23 1933-06-06 Willis B Perkins Jr Airplane landing and launching appliance
SU1740251A1 (en) * 1989-09-27 1992-06-15 В.В. Андреев Non-expendable aerospace take-off system, flying vehicle of aerospace system
RU2247059C2 (en) * 2003-04-23 2005-02-27 Калько Иван Петрович Aircraft take-off method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112937897A (en) * 2020-12-25 2021-06-11 北京泊松技术有限公司 Engine for cylinder-shooting unmanned aerial vehicle and shooting method

Also Published As

Publication number Publication date
EA009128B1 (en) 2007-10-26

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Legal Events

Date Code Title Description
MM4A Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s)

Designated state(s): AM AZ BY KZ KG MD TJ TM RU