WO2013098736A3 - A four-rotor helicopter - Google Patents

A four-rotor helicopter Download PDF

Info

Publication number
WO2013098736A3
WO2013098736A3 PCT/IB2012/057589 IB2012057589W WO2013098736A3 WO 2013098736 A3 WO2013098736 A3 WO 2013098736A3 IB 2012057589 W IB2012057589 W IB 2012057589W WO 2013098736 A3 WO2013098736 A3 WO 2013098736A3
Authority
WO
WIPO (PCT)
Prior art keywords
rotors
frame
helicopter
rotor
propellers
Prior art date
Application number
PCT/IB2012/057589
Other languages
French (fr)
Other versions
WO2013098736A2 (en
Inventor
Fabrizio GIULIETTI
Giulio AVANZINI
Original Assignee
Alma Mater Studiorum - Universita' Di Bologna
Politecnico Di Torino
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
Priority claimed from IT000769A external-priority patent/ITBO20110769A1/en
Priority claimed from IT000768A external-priority patent/ITBO20110768A1/en
Application filed by Alma Mater Studiorum - Universita' Di Bologna, Politecnico Di Torino filed Critical Alma Mater Studiorum - Universita' Di Bologna
Publication of WO2013098736A2 publication Critical patent/WO2013098736A2/en
Publication of WO2013098736A3 publication Critical patent/WO2013098736A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • 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
    • B64U30/20—Rotors; Rotor supports
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296—Rotors with variable spatial positions relative to the UAV body
    • B64U30/297—Tilting rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/20—Transmission of mechanical power to rotors or propellers
    • B64U50/27—Transmission of mechanical power to rotors or propellers with a single motor serving two or more rotors or propellers

Landscapes

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

Abstract

Described is a four-rotor helicopter (1) comprising: a frame (2), four rotors (3) equipped with propellers (8) and designed for generating a lift, the rotors (3) being connected to the frame in such a way as to be grouped in two pairs (4), the rotors (3) of each pair (4) being positioned diametrically opposite a corresponding operating axis (X, Y), for allowing a rotation of the helicopter about the corresponding operating axis (X, Y), the operating axes (X, Y) not being parallel to each other. According to a first aspect of the invention, the helicopter comprises actuator means (9) associated with the propellers (8) of at least one of the pairs of rotors for varying, relatively, the pitch, the rotors of the at least one pair being connected by a kinematic mechanism to a same motor (5), for being rotated at the same angular speed. According to another aspect of the invention, the helicopter comprises a plurality of drive elements (10) connected to the rotors for tilting them relative to the frame, each rotor (3) being tiltable relative to the frame (2) so as to vary the orientation of the axis of rotation of the corresponding propeller.
PCT/IB2012/057589 2011-12-29 2012-12-21 A four-rotor helicopter WO2013098736A2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
ITBO2011A000769 2011-12-29
IT000769A ITBO20110769A1 (en) 2011-12-29 2011-12-29 HELICOPTER QUADRIROTORE (SOLUTION B).
ITBO2011A000768 2011-12-29
IT000768A ITBO20110768A1 (en) 2011-12-29 2011-12-29 HELICOPTER QUADRIROTORE (SOLUTION A).

Publications (2)

Publication Number Publication Date
WO2013098736A2 WO2013098736A2 (en) 2013-07-04
WO2013098736A3 true WO2013098736A3 (en) 2013-08-29

Family

ID=47678932

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2012/057589 WO2013098736A2 (en) 2011-12-29 2012-12-21 A four-rotor helicopter

Country Status (1)

Country Link
WO (1) WO2013098736A2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104925251A (en) * 2015-07-04 2015-09-23 苏州科锐恒机械科技有限公司 Low-altitude flight device

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US10723442B2 (en) 2013-12-26 2020-07-28 Flir Detection, Inc. Adaptive thrust vector unmanned aerial vehicle
US10839336B2 (en) 2013-12-26 2020-11-17 Flir Detection, Inc. Unmanned delivery
CN103935513B (en) * 2014-05-13 2015-10-28 江苏艾锐泰克无人飞行器科技有限公司 The control method of many rotary wing changing distance aircraft and control setup
CN105314107B (en) * 2014-06-24 2019-03-05 王泽民 A method of realizing the vertical landing of existing unmanned aerial vehicle
DE102015006511A1 (en) * 2015-05-26 2016-12-01 Airbus Defence and Space GmbH Vertical launching aircraft
CN105292468A (en) * 2015-11-06 2016-02-03 极翼机器人(上海)有限公司 Multi-rotor-wing unmanned aircraft
CN105292454A (en) * 2015-11-06 2016-02-03 极翼机器人(上海)有限公司 Multi-rotor-wing unmanned plane
CN105292453A (en) * 2015-11-06 2016-02-03 极翼机器人(上海)有限公司 Multi-rotor-wing aircraft
CN105382423B (en) * 2015-12-16 2017-03-29 上海嘉强自动化技术有限公司 A kind of four rotor laser cutting devices
CN107226206B (en) * 2016-03-24 2023-08-04 广东泰一高新技术发展有限公司 Multi-rotor unmanned aerial vehicle safety landing system and method
JP6825000B2 (en) * 2016-03-28 2021-02-03 アマゾン テクノロジーズ インコーポレイテッド Selective pressing propulsion unit for aircraft
US9663236B1 (en) 2016-03-28 2017-05-30 Amazon Technologies, Inc. Selectively thrusting propulsion units for aerial vehicles
US9840324B2 (en) 2016-03-28 2017-12-12 Amazon Technologies, Inc. Selectively thrusting propulsion units for aerial vehicles
US10450062B1 (en) 2017-06-28 2019-10-22 Amazon Technologies, Inc. Versatile multirotor aerial vehicles
US10829200B2 (en) * 2017-11-09 2020-11-10 Bell Helicopter Textron Inc. Multirotor aircraft with collective for autorotation
US20200329690A1 (en) * 2017-11-21 2020-10-22 Basf Agro Trademarks Gmbh Unmanned aerial vehicle
CN108341054B (en) * 2018-04-27 2023-05-02 安徽工程大学 Unmanned aerial vehicle rotor cutting angle adjustment mechanism
CN109108990A (en) * 2018-07-24 2019-01-01 西北工业大学 A kind of station module inner machine people with non-co-planar more rotors
JP7417292B2 (en) 2018-08-26 2024-01-18 エアーボーン モーター ワークス インク． Electromagnetic gyroscope stabilized propulsion system method and apparatus
CN113316443A (en) 2019-01-20 2021-08-27 航空电机有限责任公司 Medical stabilizer banding method and apparatus
JP6669916B2 (en) * 2019-04-01 2020-03-18 株式会社フジタ Radio-controlled rotary wing aircraft
CN110525643A (en) * 2019-09-18 2019-12-03 深圳飞马机器人科技有限公司 A kind of vertical take-off and landing drone and its manufacturing method
US20220315207A1 (en) * 2021-04-05 2022-10-06 Beta Air, Llc Aircraft for neutralizing vertical flight
CN115071960B (en) * 2022-06-10 2023-07-18 四川大学 Coaxial aircraft with variable pitch

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5419514A (en) * 1993-11-15 1995-05-30 Duncan; Terry A. VTOL aircraft control method
JP2001071998A (en) * 1999-06-29 2001-03-21 Rokuro Hosoda Aircraft and rotating force transmitting device
US20040167682A1 (en) * 2003-02-21 2004-08-26 Lockheed Martin Corporation Virtual sensor mast
WO2006112578A1 (en) * 2005-04-20 2006-10-26 Won-Sup Oh Vertical take-off and landing aircraft
DE102005022706A1 (en) * 2005-05-18 2006-11-23 Dolch, Stefan, Dipl.-Ing. (FH) Helicopter especially for observation has multi rotor drive with rotor location outside the field of forward view of an onboard camera
WO2010128489A2 (en) * 2009-05-08 2010-11-11 Aermatica S.P.A. Aerial robotic system

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5419514A (en) * 1993-11-15 1995-05-30 Duncan; Terry A. VTOL aircraft control method
JP2001071998A (en) * 1999-06-29 2001-03-21 Rokuro Hosoda Aircraft and rotating force transmitting device
US20040167682A1 (en) * 2003-02-21 2004-08-26 Lockheed Martin Corporation Virtual sensor mast
WO2006112578A1 (en) * 2005-04-20 2006-10-26 Won-Sup Oh Vertical take-off and landing aircraft
DE102005022706A1 (en) * 2005-05-18 2006-11-23 Dolch, Stefan, Dipl.-Ing. (FH) Helicopter especially for observation has multi rotor drive with rotor location outside the field of forward view of an onboard camera
WO2010128489A2 (en) * 2009-05-08 2010-11-11 Aermatica S.P.A. Aerial robotic system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104925251A (en) * 2015-07-04 2015-09-23 苏州科锐恒机械科技有限公司 Low-altitude flight device

Also Published As

Publication number Publication date
WO2013098736A2 (en) 2013-07-04

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