PL418527A1 - Method for folding and unfolding wings of a drone starting from the tubular launcher and the wing of a drone starting from the launcher - Google Patents

Method for folding and unfolding wings of a drone starting from the tubular launcher and the wing of a drone starting from the launcher

Info

Publication number
PL418527A1
PL418527A1 PL418527A PL41852716A PL418527A1 PL 418527 A1 PL418527 A1 PL 418527A1 PL 418527 A PL418527 A PL 418527A PL 41852716 A PL41852716 A PL 41852716A PL 418527 A1 PL418527 A1 PL 418527A1
Authority
PL
Poland
Prior art keywords
launcher
wing
wings
folding
drone
Prior art date
Application number
PL418527A
Other languages
Polish (pl)
Inventor
Marcin Szender
Łukasz Stefanek
Jerzy Motłoch
Original Assignee
Szender Marcin Msp
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 Szender Marcin Msp filed Critical Szender Marcin Msp
Priority to PL418527A priority Critical patent/PL418527A1/en
Priority to PCT/PL2017/000054 priority patent/WO2018044182A2/en
Publication of PL418527A1 publication Critical patent/PL418527A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/50—Launching from storage containers, e.g. from submarine missile tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

Sposób składania i rozkładania skrzydeł samolotu bezzałogowego startującego z wyrzutni rurowej, charakteryzujący się tym, że skrzydła składa się wzdłuż kadłuba (2), następnie część skrzydła załamuje się wzdłuż rozpiętości. Złożony statek powietrzny umieszcza się w wyrzutni rurowej, po czym po starcie poprzez wyrzucenie statku powietrznego z wyrzutni rurowej, skrzydło rozkłada się w odwrotnej kolejności. Najpierw prostują się załamania profilu skrzydła, zaś przekrój poprzeczny przyjmuje prawidłowy dla profilu kształt. Następnie, skrzydła rozkładają się z położenia wzdłuż kadłuba (2) do położenia w poprzek kadłuba (2). Skrzydło samolotu bezzałogowego startującego z wyrzutni rurowej, charakteryzujące się tym, że posiada co najmniej jedno załamanie.The method of folding and unfolding the wings of an unmanned airplane taking off from a tube launcher, characterized in that the wings fold along the fuselage (2), then part of the wing breaks along the span. The assembled aircraft is placed in a tube launcher, after which after launching by throwing the aircraft out of the tube launcher, the wing unfolds in the reverse order. First, the folds of the wing profile are straightened, and the cross-section takes the correct shape for the profile. Then, the wings unfold from the position along the fuselage (2) to the position across the fuselage (2). Unmanned airplane wing taking off from a tube launcher, characterized by having at least one bend.

PL418527A 2016-09-01 2016-09-01 Method for folding and unfolding wings of a drone starting from the tubular launcher and the wing of a drone starting from the launcher PL418527A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL418527A PL418527A1 (en) 2016-09-01 2016-09-01 Method for folding and unfolding wings of a drone starting from the tubular launcher and the wing of a drone starting from the launcher
PCT/PL2017/000054 WO2018044182A2 (en) 2016-09-01 2017-05-23 A method of folding and deploying the wings of an unmanned aerial vehicle with tube-launcher take-off, and the wing of an unmanned aircraft with tube-launcher take-off

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL418527A PL418527A1 (en) 2016-09-01 2016-09-01 Method for folding and unfolding wings of a drone starting from the tubular launcher and the wing of a drone starting from the launcher

Publications (1)

Publication Number Publication Date
PL418527A1 true PL418527A1 (en) 2018-03-12

Family

ID=61157264

Family Applications (1)

Application Number Title Priority Date Filing Date
PL418527A PL418527A1 (en) 2016-09-01 2016-09-01 Method for folding and unfolding wings of a drone starting from the tubular launcher and the wing of a drone starting from the launcher

Country Status (2)

Country Link
PL (1) PL418527A1 (en)
WO (1) WO2018044182A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111111231A (en) * 2019-12-26 2020-05-08 河北科技大学 Tubular model rocket and launching method of tubular model rocket
DE102021001038B4 (en) * 2021-02-26 2023-01-19 Diehl Defence Gmbh & Co. Kg Aircraft with wing folding mechanism
WO2023096622A1 (en) * 2021-11-24 2023-06-01 Transvaro Elektron Aletleri̇ Sanayi̇ Ve Ti̇caret Anoni̇m Şi̇rketi̇ An unmanned aerial vehicle

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110226174A1 (en) * 2008-06-16 2011-09-22 Aurora Flight Sciences Corporation Combined submersible vessel and unmanned aerial vehicle
US8444082B1 (en) * 2009-08-19 2013-05-21 The United States Of America, As Represented By The Secretary Of The Navy High performance ‘X’-configuration airplane for storage and launch from a tubular container
CA2789726C (en) * 2009-09-09 2019-09-03 Aerovironment, Inc. Elevon control system
GB2534435B (en) * 2015-08-13 2017-09-06 Wirth Res Ltd An unmanned aerial vehicle with folding wing arrangement

Also Published As

Publication number Publication date
WO2018044182A3 (en) 2018-04-12
WO2018044182A2 (en) 2018-03-08

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