FR3096960B1 - Drone comprenant au moins une pale pourvue d’une portion interne en matériau alvéolaire moussé logeant une batterie électrique - Google Patents

Drone comprenant au moins une pale pourvue d’une portion interne en matériau alvéolaire moussé logeant une batterie électrique Download PDF

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Publication number
FR3096960B1
FR3096960B1 FR1905930A FR1905930A FR3096960B1 FR 3096960 B1 FR3096960 B1 FR 3096960B1 FR 1905930 A FR1905930 A FR 1905930A FR 1905930 A FR1905930 A FR 1905930A FR 3096960 B1 FR3096960 B1 FR 3096960B1
Authority
FR
France
Prior art keywords
blade
drone
electric battery
internal portion
rotor
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
FR1905930A
Other languages
English (en)
Other versions
FR3096960A1 (fr
Inventor
Philippe Crochat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR1905930A priority Critical patent/FR3096960B1/fr
Priority to CN202010501198.7A priority patent/CN111634411A/zh
Publication of FR3096960A1 publication Critical patent/FR3096960A1/fr
Application granted granted Critical
Publication of FR3096960B1 publication Critical patent/FR3096960B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • B64C27/16Drive of rotors by means, e.g. propellers, mounted on rotor blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • 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
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/21Rotary wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20Rotors; Rotor supports
    • B64U30/29Constructional aspects of rotors or rotor supports; Arrangements thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C2027/4733Rotor blades substantially made from particular materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U40/00On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration
    • B64U40/20On-board mechanical arrangements for adjusting control surfaces or rotors; On-board mechanical arrangements for in-flight adjustment of the base configuration for in-flight adjustment of the base configuration

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)
  • Battery Mounting, Suspending (AREA)

Abstract

L’invention concerne un dispositif volant (1) à voilure rotative (3) de type drone comprenant un châssis central formant un rotor (2) autour duquel tourne au moins une pale (4) s’étendant extérieurement à partir dudit rotor (2), chaque pale (4) étant munie à son extrémité libre (4a) d’un moyen de propulsion électrique à hélice (5) permettant à ladite pale (4) de tourner autour du rotor (2) pour faire décoller/voler le dispositif (1), caractérisé en ce que ladite pale (4) comporte une structure interne (4c) présentant localement au moins un logement interne creux (8) renfermant au moins une batterie électrique (7) reliée au moyen de propulsion à hélice (5) de la pale (4) considérée. Figure pour l’abrégé : Fig. 1
FR1905930A 2019-06-04 2019-06-04 Drone comprenant au moins une pale pourvue d’une portion interne en matériau alvéolaire moussé logeant une batterie électrique Active FR3096960B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1905930A FR3096960B1 (fr) 2019-06-04 2019-06-04 Drone comprenant au moins une pale pourvue d’une portion interne en matériau alvéolaire moussé logeant une batterie électrique
CN202010501198.7A CN111634411A (zh) 2019-06-04 2020-06-04 一种具有无人机类型的旋转翼的飞行装置

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1905930 2019-06-04
FR1905930A FR3096960B1 (fr) 2019-06-04 2019-06-04 Drone comprenant au moins une pale pourvue d’une portion interne en matériau alvéolaire moussé logeant une batterie électrique

Publications (2)

Publication Number Publication Date
FR3096960A1 FR3096960A1 (fr) 2020-12-11
FR3096960B1 true FR3096960B1 (fr) 2021-06-18

Family

ID=68654574

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1905930A Active FR3096960B1 (fr) 2019-06-04 2019-06-04 Drone comprenant au moins une pale pourvue d’une portion interne en matériau alvéolaire moussé logeant une batterie électrique

Country Status (2)

Country Link
CN (1) CN111634411A (fr)
FR (1) FR3096960B1 (fr)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4524499A (en) * 1981-11-16 1985-06-25 Trw Inc. Method of fabricating an aircraft propeller assembly with composite blades
US5297759A (en) * 1992-04-06 1994-03-29 Neil Tilbor Rotary aircraft passively stable in hover
US7946526B2 (en) * 2004-11-05 2011-05-24 Nachman Zimet Rotary-wing vehicle system
KR101217804B1 (ko) * 2010-06-01 2013-01-22 (주)선택이앤티 하방 조정프로펠러형 비행체
CN202529145U (zh) * 2011-12-14 2012-11-14 中国人民解放军总参谋部第六十研究所 无人直升机复合材料旋翼桨叶
FR3048956B1 (fr) * 2016-03-18 2019-07-12 Centre National D'etudes Spatiales C N E S Aeronef a voilure tournante
CN107054643A (zh) * 2016-12-16 2017-08-18 黄鹏 自平衡扭矩多倍增升力直升机旋翼动力结构
CN206615593U (zh) * 2017-03-28 2017-11-07 重庆建工集团股份有限公司 便携式无人机收纳箱
WO2019005467A2 (fr) * 2017-06-09 2019-01-03 Zornes David Allen Production de poussée de profil aérodynamique à trajectoire de pointe dans un aéronef à voilure tournante

Also Published As

Publication number Publication date
FR3096960A1 (fr) 2020-12-11
CN111634411A (zh) 2020-09-08

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