FR3066125B1 - FIXED-WHEEL DRONE HAVING A NEW CONFIGURATION FENDER ASSEMBLY - Google Patents

FIXED-WHEEL DRONE HAVING A NEW CONFIGURATION FENDER ASSEMBLY Download PDF

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Publication number
FR3066125B1
FR3066125B1 FR1754027A FR1754027A FR3066125B1 FR 3066125 B1 FR3066125 B1 FR 3066125B1 FR 1754027 A FR1754027 A FR 1754027A FR 1754027 A FR1754027 A FR 1754027A FR 3066125 B1 FR3066125 B1 FR 3066125B1
Authority
FR
France
Prior art keywords
fixed
drone
wheel
new configuration
fender assembly
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
FR1754027A
Other languages
French (fr)
Other versions
FR3066125A1 (en
Inventor
Michael De Lagarde
Maxime Piton
Pierre-Yves Fulchiron
Alexandre Lapadu
Benjamin MICHEL
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.)
Delair Fr
Original Assignee
Delair Tech
Delair-Tech
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 Delair Tech, Delair-Tech filed Critical Delair Tech
Priority to FR1754027A priority Critical patent/FR3066125B1/en
Priority to PCT/EP2018/062144 priority patent/WO2018206726A1/en
Publication of FR3066125A1 publication Critical patent/FR3066125A1/en
Application granted granted Critical
Publication of FR3066125B1 publication Critical patent/FR3066125B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
    • 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
    • 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
    • B64U70/10—Launching, take-off or landing arrangements for releasing or capturing UAVs by hand
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Body Structure For Vehicles (AREA)
  • Toys (AREA)

Abstract

L'invention concerne un drone à voilure fixe comportant un corps auquel est monté solidaire un ensemble empennage, tel que : - l'ensemble empennage comporte : ○ un empennage gauche, comportant un élément de structure s'étendant longitudinalement, dit poutrelle gauche, solidaire à une extrémité avec le corps du drone à voilure fixe, et solidaire à une deuxième extrémité avec une unique surface gauche, ○ un empennage droit, comportant un élément de structure s'étendant longitudinalement, dit poutrelle droite, solidaire à une extrémité avec le corps du drone à voilure fixe, et solidaire à une deuxième extrémité avec une unique surface droite, - l'empennage gauche et l'empennage droit sont sans aucune liaison entre eux.The invention relates to a fixed-wing drone comprising a body to which a tail unit is mounted, such that: - the tail unit comprises: ○ a left tail unit, comprising a structural element extending longitudinally, said left beam, integral at one end with the body of the fixed-wing drone, and secured at a second end with a single left surface, ○ a right tail unit, comprising a structural element extending longitudinally, called straight beam, secured at one end with the body of the fixed-wing drone, and secured at a second end with a single right surface, - the left tail and the right tail are without any connection between them.

FR1754027A 2017-05-09 2017-05-09 FIXED-WHEEL DRONE HAVING A NEW CONFIGURATION FENDER ASSEMBLY Active FR3066125B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1754027A FR3066125B1 (en) 2017-05-09 2017-05-09 FIXED-WHEEL DRONE HAVING A NEW CONFIGURATION FENDER ASSEMBLY
PCT/EP2018/062144 WO2018206726A1 (en) 2017-05-09 2018-05-09 Fixed-wing drone comprising an empennage assembly with a novel configuration

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1754027A FR3066125B1 (en) 2017-05-09 2017-05-09 FIXED-WHEEL DRONE HAVING A NEW CONFIGURATION FENDER ASSEMBLY
FR1754027 2017-05-09

Publications (2)

Publication Number Publication Date
FR3066125A1 FR3066125A1 (en) 2018-11-16
FR3066125B1 true FR3066125B1 (en) 2020-05-29

Family

ID=60138416

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1754027A Active FR3066125B1 (en) 2017-05-09 2017-05-09 FIXED-WHEEL DRONE HAVING A NEW CONFIGURATION FENDER ASSEMBLY

Country Status (2)

Country Link
FR (1) FR3066125B1 (en)
WO (1) WO2018206726A1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1563813A (en) * 1977-05-19 1980-04-02 British Aircraft Corp Ltd Aircraft
US5765777A (en) * 1991-11-20 1998-06-16 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with variable pitch propulsion means
US6666406B2 (en) * 2000-06-29 2003-12-23 The Boeing Company Blended wing and multiple-body airplane configuration
KR100743583B1 (en) * 2003-03-28 2007-07-27 모제이브 에어로스페이스 벤쳐스, 엘엘씨 Winged spacecraft

Also Published As

Publication number Publication date
WO2018206726A1 (en) 2018-11-15
FR3066125A1 (en) 2018-11-16

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