PL439361A1 - Wing of an unmanned aerial vehicle with a slotted flap, especially of a gyrodin - Google Patents

Wing of an unmanned aerial vehicle with a slotted flap, especially of a gyrodin

Info

Publication number
PL439361A1
PL439361A1 PL439361A PL43936121A PL439361A1 PL 439361 A1 PL439361 A1 PL 439361A1 PL 439361 A PL439361 A PL 439361A PL 43936121 A PL43936121 A PL 43936121A PL 439361 A1 PL439361 A1 PL 439361A1
Authority
PL
Poland
Prior art keywords
wing
slotted flap
aerial vehicle
unmanned aerial
gyrodin
Prior art date
Application number
PL439361A
Other languages
Polish (pl)
Inventor
Jan Muchowski
Original Assignee
Stowarzyszenie B-4
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 Stowarzyszenie B-4 filed Critical Stowarzyszenie B-4
Priority to PL439361A priority Critical patent/PL439361A1/en
Priority to DE102021133417.9A priority patent/DE102021133417A1/en
Publication of PL439361A1 publication Critical patent/PL439361A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/17—Helicopters
    • 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
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U40/00—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration
    • B64U40/10—On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration for adjusting control surfaces or rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/40—Empennages, e.g. V-tails
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers

Abstract

Przedmiotem wynalazku jest skrzydło bezzałogowego aparatu latającego z klapą szczelinową, zwłaszcza gyrodyny wykonane z kompozytu składające się z części nośnej i połączonej z nią zawiasowo klapy szczelinowej, wychylanej poprzez serwomechanizmy z popychaczem charakteryzujące się tym, że odległość osi obrotu (14) klapy szczelinowej od przedniej krawędzi skrzydła wynosi a = 0,45 – 0,7 długości (c) cięciwy (15) skrzydła, a jej odległość od cięciwy (15) skrzydła wynosi b = 0,01 – 0,1 długości (c) cięciwy (15), zaś kąt α wychylenia klapy szczelinowej skrzydła wynosi 0 - 105°.The subject of the invention is a wing of an unmanned aerial vehicle with a slotted flap, in particular gyrodins made of a composite, consisting of a carrier part and a hinged slotted flap, tilted by servo-mechanisms with a pusher, characterized in that the distance between the axis of rotation (14) of the slotted flap from the front edge is a = 0.45 - 0.7 the length (c) of the chord (15) of the wing, and its distance from the chord (15) of the wing is b = 0.01 - 0.1 the length (c) of the chord (15), and the swing angle α of the wing slotted flap is 0 - 105°.

PL439361A 2021-10-29 2021-10-29 Wing of an unmanned aerial vehicle with a slotted flap, especially of a gyrodin PL439361A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL439361A PL439361A1 (en) 2021-10-29 2021-10-29 Wing of an unmanned aerial vehicle with a slotted flap, especially of a gyrodin
DE102021133417.9A DE102021133417A1 (en) 2021-10-29 2021-12-16 Wing of an unmanned aerial vehicle with split flap, especially a flight screw

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL439361A PL439361A1 (en) 2021-10-29 2021-10-29 Wing of an unmanned aerial vehicle with a slotted flap, especially of a gyrodin

Publications (1)

Publication Number Publication Date
PL439361A1 true PL439361A1 (en) 2023-05-02

Family

ID=85983931

Family Applications (1)

Application Number Title Priority Date Filing Date
PL439361A PL439361A1 (en) 2021-10-29 2021-10-29 Wing of an unmanned aerial vehicle with a slotted flap, especially of a gyrodin

Country Status (2)

Country Link
DE (1) DE102021133417A1 (en)
PL (1) PL439361A1 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5094412A (en) 1989-10-13 1992-03-10 Bell Helicopter Textron Inc. Flaperon system for tilt rotor wings
US20050151001A1 (en) 2003-07-02 2005-07-14 Loper Arthur W. Compound helicopter
EP3674202B1 (en) 2018-12-28 2021-03-17 LEONARDO S.p.A. Aircraft wing

Also Published As

Publication number Publication date
DE102021133417A1 (en) 2023-05-04

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