PL422977A1 - Kinetic launcher for unmanned aerial vehicles - Google Patents

Kinetic launcher for unmanned aerial vehicles

Info

Publication number
PL422977A1
PL422977A1 PL422977A PL42297717A PL422977A1 PL 422977 A1 PL422977 A1 PL 422977A1 PL 422977 A PL422977 A PL 422977A PL 42297717 A PL42297717 A PL 42297717A PL 422977 A1 PL422977 A1 PL 422977A1
Authority
PL
Poland
Prior art keywords
kinetic
launcher
unmanned aerial
aerial vehicles
flywheel
Prior art date
Application number
PL422977A
Other languages
Polish (pl)
Other versions
PL233329B1 (en
Inventor
Mirosław Kondratiuk
Leszek Ambroziak
Zdzisław Gosiewski
Original Assignee
Politechnika Białostocka
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 Politechnika Białostocka filed Critical Politechnika Białostocka
Priority to PL422977A priority Critical patent/PL233329B1/en
Publication of PL422977A1 publication Critical patent/PL422977A1/en
Publication of PL233329B1 publication Critical patent/PL233329B1/en

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  • Forklifts And Lifting Vehicles (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Kinetyczna wyrzutnia dla bezzałogowych statków powietrznych zbudowana jest z systemu napędowego i zamontowanej na ramie części wyrzucającej złożonej z: kół zębatych, pasów zębatych z naciągiem, wózka na prowadnicach liniowych oraz nastawnej podpory do zmiany kąta wyrzutu. Na wale zamontowano koło zamachowe (1) magazynujące energię mechaniczną w formie kinetycznej. Aktywne sprzęgło elektromagnetyczne oraz hamulec elektromagnetyczny wraz z blokadą i wałem hamującym są elementami wykonawczymi układu sterowania parametrami startowymi wyrzutni. Enkoder obrotowy (12) mierzący przemieszczenie kątowe jest sensorycznym elementem zamkniętego układu sterowania. Ponadto, silnik elektryczny sprzęgnięty jest za pośrednictwem asynchronicznej przekładni pasowej z kołem zamachowym (1) do magazynowania energii kinetycznej w postaci wirującej masy.The kinetic launcher for unmanned aerial vehicles is made of a propulsion system and a frame-mounted ejection part consisting of: gears, toothed belts with tension, a carriage on linear guides and an adjustable support for changing the angle of discharge. A flywheel (1) storing mechanical energy in kinetic form is mounted on the shaft. An active electromagnetic clutch and an electromagnetic brake together with a blockage and a braking shaft are the executive elements of the launcher control parameters. The rotary encoder (12) measuring angular displacement is a sensory element of the closed control system. In addition, the electric motor is coupled via an asynchronous belt transmission with a flywheel (1) to store kinetic energy in the form of a rotating mass.

PL422977A 2017-09-26 2017-09-26 Kinetic launcher for unmanned aerial vehicles PL233329B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL422977A PL233329B1 (en) 2017-09-26 2017-09-26 Kinetic launcher for unmanned aerial vehicles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL422977A PL233329B1 (en) 2017-09-26 2017-09-26 Kinetic launcher for unmanned aerial vehicles

Publications (2)

Publication Number Publication Date
PL422977A1 true PL422977A1 (en) 2019-04-08
PL233329B1 PL233329B1 (en) 2019-09-30

Family

ID=65992093

Family Applications (1)

Application Number Title Priority Date Filing Date
PL422977A PL233329B1 (en) 2017-09-26 2017-09-26 Kinetic launcher for unmanned aerial vehicles

Country Status (1)

Country Link
PL (1) PL233329B1 (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4678143A (en) * 1982-12-17 1987-07-07 Frazer-Nash Ltd. Launcher for remotely piloted aircraft
CN105799948A (en) * 2016-03-18 2016-07-27 北京理工大学 Catapult of flywheel-type high-speed unmanned aerial vehicle

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4678143A (en) * 1982-12-17 1987-07-07 Frazer-Nash Ltd. Launcher for remotely piloted aircraft
CN105799948A (en) * 2016-03-18 2016-07-27 北京理工大学 Catapult of flywheel-type high-speed unmanned aerial vehicle

Also Published As

Publication number Publication date
PL233329B1 (en) 2019-09-30

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