BR112012013143A2 - helicóptero desmontável e método de acionamento de um rotor de compensação de torque de um helicóptero uav - Google Patents

helicóptero desmontável e método de acionamento de um rotor de compensação de torque de um helicóptero uav

Info

Publication number
BR112012013143A2
BR112012013143A2 BR112012013143A BR112012013143A BR112012013143A2 BR 112012013143 A2 BR112012013143 A2 BR 112012013143A2 BR 112012013143 A BR112012013143 A BR 112012013143A BR 112012013143 A BR112012013143 A BR 112012013143A BR 112012013143 A2 BR112012013143 A2 BR 112012013143A2
Authority
BR
Brazil
Prior art keywords
helicopter
torque compensation
uav
demountable
driving
Prior art date
Application number
BR112012013143A
Other languages
English (en)
Inventor
Stenbom Kjell
Cardell Per-Erik
Lidström Robert
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Publication of BR112012013143A2 publication Critical patent/BR112012013143A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • 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
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/60—UAVs characterised by the material
    • B64U20/65—Composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/70—Constructional aspects of the UAV body
    • 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
    • B64U50/23—Transmission of mechanical power to rotors or propellers with each propulsion means having an individual motor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/20—Constructional aspects of UAVs for noise reduction
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)
  • Toys (AREA)
  • Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)

Abstract

helicóptero desmontável e método de acionamento de um rotor de compensação de torque de um helicóptero uav. a presente invenção refere-se a um helicóptero de veículo aéreo não tripulado (uav) compreendendo uma seção de cauda (3) desmontável incluindo um rotor de compensação de torque (5), em que a transmissão de força do motor (4) para o rotor de compensação de torque (5) é realizada por disposições de transmissão de polia e correia (7, 8).
BR112012013143A 2009-12-02 2009-12-02 helicóptero desmontável e método de acionamento de um rotor de compensação de torque de um helicóptero uav BR112012013143A2 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/SE2009/051365 WO2011068445A1 (en) 2009-12-02 2009-12-02 Dismountable helicopter

Publications (1)

Publication Number Publication Date
BR112012013143A2 true BR112012013143A2 (pt) 2017-03-21

Family

ID=44115146

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012013143A BR112012013143A2 (pt) 2009-12-02 2009-12-02 helicóptero desmontável e método de acionamento de um rotor de compensação de torque de um helicóptero uav

Country Status (5)

Country Link
US (1) US9067677B2 (pt)
EP (1) EP2507129B1 (pt)
BR (1) BR112012013143A2 (pt)
ES (1) ES2527960T3 (pt)
WO (1) WO2011068445A1 (pt)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109070991A (zh) * 2017-09-30 2018-12-21 深圳市大疆创新科技有限公司 无人机的机架组件及无人机

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202270360U (zh) * 2011-09-29 2012-06-13 深圳市沈氏彤创航天模型有限公司 遥控模型像真直升机的尾旋翼传动装置
FR2983171B1 (fr) * 2011-11-30 2014-03-21 Eurocopter France Dispositif anti-couple a poussee longitudinale pour un giravion
JP5801851B2 (ja) * 2013-06-28 2015-10-28 ヤマハ発動機株式会社 無人ヘリコプタ
CN105346712B (zh) * 2015-12-03 2023-12-15 江苏神铸智能科技有限公司 小型单旋翼无人直升机变速系统
EP3199455B1 (en) * 2016-01-29 2020-04-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotary aircraft with an interface frame joining the fuselage tail boom and the tail cone
WO2017147769A1 (zh) * 2016-03-01 2017-09-08 深圳市大疆创新科技有限公司 电机的控制方法、装置及系统
US11829337B2 (en) 2016-11-16 2023-11-28 Sap Se Minimizing downtime in migrating content of databases systems
CN106956772B (zh) * 2017-04-15 2023-07-21 上海量明科技发展有限公司 可折叠的无人机及其实现方法
CN108591388A (zh) * 2018-07-16 2018-09-28 飞瑞航空科技（江苏）有限公司 一种无人机皮带传动系统用可调式涨紧机构
CN112238948A (zh) * 2020-10-16 2021-01-19 中国直升机设计研究所 一种快卸式直升机尾传动轴组件
CN113060272B (zh) * 2021-05-19 2021-11-16 宜宾职业技术学院 一种无人机机臂折叠结构
RU208636U1 (ru) * 2021-10-04 2021-12-28 Общество с ограниченной ответственностью «РД-Хели» Беспилотный винтокрылый летательный аппарат (бвла)

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2947497A (en) * 1957-05-06 1960-08-02 Omega Aircraft Corp Dual engine drive means for helicopters
US3029047A (en) * 1958-01-17 1962-04-10 Hiller Aircraft Corp Collapsible and portable rotary wing aircraft
US3162400A (en) * 1962-06-12 1964-12-22 Wood Benjamin Graham Reciprocating wing helicopter adapted to be manually powered
GB1472540A (en) * 1973-08-28 1977-05-04 Westland Aircraft Ltd Helicopters
JPS582706B2 (ja) 1977-09-06 1983-01-18 マブチモ−タ−株式会社 ヘリコプタ模型装置
US4245801A (en) * 1979-02-15 1981-01-20 United Technologies Corporation Tail rotor control cable-pylon fold accommodation
US5609312A (en) * 1991-09-30 1997-03-11 Arlton; Paul E. Model helicopter
IT1293676B1 (it) 1997-08-01 1999-03-08 Finmeccanica Spa Innesto rilasciabile per una linea di trasmissione del moto ad un rotore di coda di un elicottero.
US6065718A (en) 1998-03-23 2000-05-23 Piasecki; Michael W. Universal VTOL power and rotor system module
US6126113A (en) * 1998-09-21 2000-10-03 Navickas; Thomas Joseph Helicopter removable drive train platform
CA2301350A1 (en) * 2000-02-25 2001-08-25 Michael W. Piasecki Universal vtol power and rotor system module
DE20213638U1 (de) * 2002-08-30 2002-11-21 Guzicki Gerd Heckwinkelgetriebe für einen Modellhubschrauber
GB0710499D0 (en) 2007-06-01 2007-07-11 Broadbent Michael C Aircraft and method for storing the aircraft
ATE552896T1 (de) * 2007-11-26 2012-04-15 Zhihong Luo Modellhelikopter

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109070991A (zh) * 2017-09-30 2018-12-21 深圳市大疆创新科技有限公司 无人机的机架组件及无人机
CN109070991B (zh) * 2017-09-30 2021-09-14 深圳市大疆创新科技有限公司 无人机的机架组件及无人机

Also Published As

Publication number Publication date
EP2507129B1 (en) 2014-11-26
US9067677B2 (en) 2015-06-30
EP2507129A4 (en) 2013-11-13
ES2527960T3 (es) 2015-02-02
US20120298792A1 (en) 2012-11-29
WO2011068445A1 (en) 2011-06-09
EP2507129A1 (en) 2012-10-10

Similar Documents

Publication Publication Date Title
BR112012013143A2 (pt) helicóptero desmontável e método de acionamento de um rotor de compensação de torque de um helicóptero uav
WO2011144692A3 (de) Hybrides antriebs- und energiesystem für fluggeräte
BR112013002327A8 (pt) dispositivo de acionamento elétrico para uma aeronave
EA200900826A1 (ru) Система привода воздушного винта летательного аппарата, способ привода воздушного винта летательного аппарата, применение подшипника и применение электрической машины для привода воздушного винта летательного аппарата
FR2952907B1 (fr) Installation motrice, helicoptere comportant une telle installation motrice, et procede mis en oeuvre par cette installation motrice
IN2015DN01835A (pt)
BR112012004964A8 (pt) Girocóptero
BR112015021688A8 (pt) aeronave híbrida, método para operação de voo de um sistema de propulsão híbrido, e, conjunto de embreagem híbrida
BR112019024856A2 (pt) unidade de acionamento híbrido e processo para operação de um veículo com acionamento híbrido
WO2015014614A3 (de) Verfahren und vorrichtung zur ankupplung eines verbrennungsmotors bei einem verzögerungsvorgang
BR112014032553A2 (pt) sistema de transmissão e método de acionamento de um veículo
BR112015006124A2 (pt) conjunto de conexão, motor de turbina a gás, e, método para fazer manutenção num motor de turbina a gás
WO2012061407A3 (en) Vehicle and transmission for a vehicle
WO2012076548A3 (de) Startvorrichtung
BR102015014138A8 (pt) Unidade propulsora híbrida para veículos a motor com dispositivos de engate em lados opostos da máquina elétrica
SE0801426L (sv) Förfarande och system för transmissionsstyrning vid lågt effektbehov
WO2014128433A3 (en) Electric drive system
WO2015051860A3 (de) Antriebsstrang eines hybrid-kraftfahrzeuges
BR112018015322A2 (pt) método para controlar um trem de potência híbrido, um trem de potência híbrido, e um veículo compreendendo tal trem de potência híbrido
FR2957585B1 (fr) Procede et dispositif d'entrainement d'au moins une roue de train d'atterrissage d'un aeronef par un moteur de roue
EP3587159A3 (de) Antriebsstrangmodul für ein kraftfahrzeug und montage- und demontageverfahren für ein antriebsstrangmodul
BR112012027358A2 (pt) roda livre com sistema de amortecimento integrado
BR112018014725A2 (pt) métodos de inicialização de um motor de combustão e conjunto do acionador de partida de ar de turbina
DE202007001923U1 (de) Antriebssystem der Motor-Kühlung für schwere Kraftfahrzeuge
BR102012010234A8 (pt) Veículo e método para sincronizar a operação do motor e do sistema de transmissão dentro de um veículo agrícola

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]