RU2005134065A - TURN-TAKE-OFF DEVICE - Google Patents

TURN-TAKE-OFF DEVICE Download PDF

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Publication number
RU2005134065A
RU2005134065A RU2005134065/11A RU2005134065A RU2005134065A RU 2005134065 A RU2005134065 A RU 2005134065A RU 2005134065/11 A RU2005134065/11 A RU 2005134065/11A RU 2005134065 A RU2005134065 A RU 2005134065A RU 2005134065 A RU2005134065 A RU 2005134065A
Authority
RU
Russia
Prior art keywords
take
turn
starter
aircraft
rails
Prior art date
Application number
RU2005134065/11A
Other languages
Russian (ru)
Other versions
RU2307770C2 (en
Inventor
Эдуард Дмитриевич Житников (RU)
Эдуард Дмитриевич Житников
Original Assignee
Эдуард Дмитриевич Житников (RU)
Эдуард Дмитриевич Житников
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 Эдуард Дмитриевич Житников (RU), Эдуард Дмитриевич Житников filed Critical Эдуард Дмитриевич Житников (RU)
Priority to RU2005134065/11A priority Critical patent/RU2307770C2/en
Publication of RU2005134065A publication Critical patent/RU2005134065A/en
Application granted granted Critical
Publication of RU2307770C2 publication Critical patent/RU2307770C2/en

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  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Mechanisms For Operating Contacts (AREA)
  • Component Parts Of Construction Machinery (AREA)

Claims (1)

Поворотно-взлетное устройство, содержащее шарнирно навешенную на поворотную башню консольную металлоконструкцию с направляющими, отличающееся тем, что устройство содержит стартер, перемещающийся по направляющим консоли с приводом от разового пирозаряда для взлетного разгона, установленного на стартер самолета с подключением двигателя самолета.A rotary take-off device comprising a cantilever metal structure with rails hinged on a turret, characterized in that the device comprises a starter that moves along the guide rails of the console driven by a single pyro charge for take-off acceleration mounted on the aircraft starter with the aircraft engine connected.
RU2005134065/11A 2005-11-03 2005-11-03 Rotating takeoff gear RU2307770C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005134065/11A RU2307770C2 (en) 2005-11-03 2005-11-03 Rotating takeoff gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005134065/11A RU2307770C2 (en) 2005-11-03 2005-11-03 Rotating takeoff gear

Publications (2)

Publication Number Publication Date
RU2005134065A true RU2005134065A (en) 2007-05-20
RU2307770C2 RU2307770C2 (en) 2007-10-10

Family

ID=38163703

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005134065/11A RU2307770C2 (en) 2005-11-03 2005-11-03 Rotating takeoff gear

Country Status (1)

Country Link
RU (1) RU2307770C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102874415A (en) * 2012-09-28 2013-01-16 王洪才 Explosive aircraft catapult for aircraft carriers

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106477064A (en) * 2016-12-05 2017-03-08 朱继琼 Aircraft is launched in explosive charge gas storage
CN111169298A (en) * 2020-01-31 2020-05-19 武汉大学 Tubular transmitting unmanned aerial vehicle wireless power supply system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102874415A (en) * 2012-09-28 2013-01-16 王洪才 Explosive aircraft catapult for aircraft carriers

Also Published As

Publication number Publication date
RU2307770C2 (en) 2007-10-10

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