FR3060530B1 - PARACHUTE EJECTION DEVICE PROPELLED BY THE RUPTURE OF A CONTAINER FILLED WITH GAS UNDER PRESSURE AND EQUIPPING AN AIRCRAFT WITHOUT A PILOT - Google Patents

PARACHUTE EJECTION DEVICE PROPELLED BY THE RUPTURE OF A CONTAINER FILLED WITH GAS UNDER PRESSURE AND EQUIPPING AN AIRCRAFT WITHOUT A PILOT Download PDF

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Publication number
FR3060530B1
FR3060530B1 FR1663082A FR1663082A FR3060530B1 FR 3060530 B1 FR3060530 B1 FR 3060530B1 FR 1663082 A FR1663082 A FR 1663082A FR 1663082 A FR1663082 A FR 1663082A FR 3060530 B1 FR3060530 B1 FR 3060530B1
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France
Prior art keywords
parachute
envelope
rupture
container filled
aircraft
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Active
Application number
FR1663082A
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French (fr)
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FR3060530A1 (en
Inventor
Eric Parmentier
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Pixiel
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Pixiel
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Publication date
Application filed by Pixiel filed Critical Pixiel
Priority to FR1663082A priority Critical patent/FR3060530B1/en
Publication of FR3060530A1 publication Critical patent/FR3060530A1/en
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Publication of FR3060530B1 publication Critical patent/FR3060530B1/en
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Classifications

    • 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
    • B64D17/00Parachutes
    • B64D17/62Deployment
    • B64D17/72Deployment by explosive or inflatable means
    • 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
    • B64D17/00Parachutes
    • B64D17/80Parachutes in association with aircraft, e.g. for braking thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00Launching, take-off or landing arrangements
    • B64U70/80Vertical take-off or landing, e.g. using rockets
    • B64U70/83Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • B64U10/13Flying platforms
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Burglar Alarm Systems (AREA)

Abstract

L'invention concerne un dispositif d'éjection d'un parachute équipant un aéronef sans pilote, comportant un logement doté d'une ouverture orientée vers le haut, et un dispositif de contrôle détectant un événement provoquant l'éjection d'un parachute contenu dans la partie haute du logement. Le dispositif d'éjection comporte en outre un récipient rempli de gaz sous pression placé sous le parachute et doté d'une enveloppe destinée à être rompue, et un dispositif de rupture de ladite enveloppe activé par le dispositif de contrôle pour rompre ladite enveloppe. Selon un perfectionnement, le dispositif de rupture comporte un élément chauffant qui est plaqué sur ladite enveloppe afin de la rompre en chauffant. Selon une autre caractéristique, l'élément chauffant est une résistance électrique plaquée contre une partie au moins du pourtour de l'enveloppe du récipient.The invention relates to a device for ejecting a parachute fitted to an unmanned aircraft, comprising a housing provided with an opening facing upwards, and a monitoring device detecting an event causing the ejection of a parachute contained in it. the upper part of the accommodation. The ejection device further comprises a container filled with pressurized gas placed under the parachute and provided with an envelope intended to be broken, and a device for breaking said envelope activated by the control device in order to rupture said envelope. According to an improvement, the breaking device comprises a heating element which is pressed against said envelope in order to break it by heating. According to another characteristic, the heating element is an electrical resistance pressed against at least part of the periphery of the casing of the container.

FR1663082A 2016-12-21 2016-12-21 PARACHUTE EJECTION DEVICE PROPELLED BY THE RUPTURE OF A CONTAINER FILLED WITH GAS UNDER PRESSURE AND EQUIPPING AN AIRCRAFT WITHOUT A PILOT Active FR3060530B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1663082A FR3060530B1 (en) 2016-12-21 2016-12-21 PARACHUTE EJECTION DEVICE PROPELLED BY THE RUPTURE OF A CONTAINER FILLED WITH GAS UNDER PRESSURE AND EQUIPPING AN AIRCRAFT WITHOUT A PILOT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1663082A FR3060530B1 (en) 2016-12-21 2016-12-21 PARACHUTE EJECTION DEVICE PROPELLED BY THE RUPTURE OF A CONTAINER FILLED WITH GAS UNDER PRESSURE AND EQUIPPING AN AIRCRAFT WITHOUT A PILOT
FR1663082 2016-12-21

Publications (2)

Publication Number Publication Date
FR3060530A1 FR3060530A1 (en) 2018-06-22
FR3060530B1 true FR3060530B1 (en) 2021-04-23

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
FR1663082A Active FR3060530B1 (en) 2016-12-21 2016-12-21 PARACHUTE EJECTION DEVICE PROPELLED BY THE RUPTURE OF A CONTAINER FILLED WITH GAS UNDER PRESSURE AND EQUIPPING AN AIRCRAFT WITHOUT A PILOT

Country Status (1)

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FR (1) FR3060530B1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109436342B (en) * 2018-12-20 2024-05-28 北京科新信息技术有限公司 Gas release device and unmanned aerial vehicle
CN110155342A (en) * 2019-05-23 2019-08-23 穆康乐 Multi-rotor unmanned aerial vehicle safety guarantee system and method used under a kind of unsteady state
CN112550729B (en) * 2021-02-23 2021-05-11 成都飞航智云科技有限公司 Aircraft with pneumatic appearance is impaired later to prevent weighing down function

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3811212A1 (en) * 1988-04-02 1989-10-26 Wulf Seiffert Device for releasing an aircraft rescue parachute from a container
DE10026469C1 (en) * 2000-05-27 2002-01-10 Eurocopter Deutschland Method of deploying a parachute to a drone
US6685140B2 (en) * 2001-09-27 2004-02-03 Ernest A. Carroll Miniature, unmanned aircraft with automatically deployed parachute
FR3012423B1 (en) * 2013-10-25 2018-01-26 Roque Canales DEVICE FOR SECURING CIVIL DRONES IN FLIGHT, CUTTING THE PROPULSION AND FORCING A PARACHUTE IF THE DRONE COMES OUT OF ITS NORMAL FLIGHT DOMAIN OR IF THE TELEPILOTE REQUIRES THE EMERGENCY STOP OF THE FLIGHT
DE202015001833U1 (en) * 2015-03-10 2015-09-10 Kapi Electronics Gmbh Intelligent compressed air parachute rescue system for manned and unmanned aerial vehicles
WO2016182750A1 (en) * 2015-04-28 2016-11-17 SkyFallX, LLC Autonomous safety and recovery system for unmanned aerial vehicles

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Publication number Publication date
FR3060530A1 (en) 2018-06-22

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