PL443310A1 - Zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania - Google Patents

Zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania

Info

Publication number
PL443310A1
PL443310A1 PL443310A PL44331022A PL443310A1 PL 443310 A1 PL443310 A1 PL 443310A1 PL 443310 A PL443310 A PL 443310A PL 44331022 A PL44331022 A PL 44331022A PL 443310 A1 PL443310 A1 PL 443310A1
Authority
PL
Poland
Prior art keywords
unmanned aerial
aerial vehicle
landing
vertical take
automated unmanned
Prior art date
Application number
PL443310A
Other languages
English (en)
Inventor
Maciej Podsędkowski
Rafał Konopiński
Leszek PODSĘDKOWSKI
Damian Obidowski
Michał Lipian
Krzysztof Bortnowski
Original Assignee
Politechnika Łódzka
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 Łódzka filed Critical Politechnika Łódzka
Priority to PL443310A priority Critical patent/PL443310A1/pl
Publication of PL443310A1 publication Critical patent/PL443310A1/pl

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/44Blade pitch-changing mechanisms electric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/02Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02Dropping, ejecting, or releasing articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/20Vertical take-off and landing [VTOL] aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/25Fixed-wing aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/15UAVs specially adapted for particular uses or applications for conventional or electronic warfare
    • B64U2101/16UAVs specially adapted for particular uses or applications for conventional or electronic warfare for controlling, capturing or immobilising other vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Abstract

Przedmiotem zgłoszenia jest przedstawiony na rysunku zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania, wyposażony w co najmniej jeden płat nośny z dwoma skrzydłami rozmieszczonymi po obu stronach kadłuba, co najmniej dwa zespoły napędowe zawierające silniki napędowe ze śmigłami, zamocowane symetrycznie po obu stronach kadłuba, których śmigła są wyposażone w układ regulacji kąta obrotu łopat śmigła względem osi wirnika silnika, zmieniający tak samo kąt obrotu wszystkich łopat pojedynczego śmigła, charakteryzuje się tym, że jest wyposażony w system neutralizacji innych bezzałogowych pojazdów latających.
PL443310A 2022-12-29 2022-12-29 Zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania PL443310A1 (pl)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL443310A PL443310A1 (pl) 2022-12-29 2022-12-29 Zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL443310A PL443310A1 (pl) 2022-12-29 2022-12-29 Zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania

Publications (1)

Publication Number Publication Date
PL443310A1 true PL443310A1 (pl) 2024-07-01

Family

ID=91719433

Family Applications (1)

Application Number Title Priority Date Filing Date
PL443310A PL443310A1 (pl) 2022-12-29 2022-12-29 Zautomatyzowany bezzałogowy pojazd latający pionowego startu i lądowania

Country Status (1)

Country Link
PL (1) PL443310A1 (pl)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120091257A1 (en) * 2009-05-27 2012-04-19 Israel Aerospace Industries Ltd. Air vehicle
PL432723A1 (pl) * 2020-01-30 2021-08-02 Politechnika Łódzka Zautomatyzowany pojazd latający pionowego startu i lądowania
CN217294912U (zh) * 2021-08-13 2022-08-26 孙柏原 一种有火箭发射架和捕捉网的小型固定翼无人机

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120091257A1 (en) * 2009-05-27 2012-04-19 Israel Aerospace Industries Ltd. Air vehicle
PL432723A1 (pl) * 2020-01-30 2021-08-02 Politechnika Łódzka Zautomatyzowany pojazd latający pionowego startu i lądowania
CN217294912U (zh) * 2021-08-13 2022-08-26 孙柏原 一种有火箭发射架和捕捉网的小型固定翼无人机

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