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 PDFInfo
- 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
- Authority
- FR
- France
- Prior art keywords
- parachute
- envelope
- rupture
- container filled
- aircraft
- 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
Links
- 238000010438 heat treatment Methods 0.000 abstract 3
- 230000004308 accommodation Effects 0.000 abstract 1
- 238000012806 monitoring device Methods 0.000 abstract 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
- B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote 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.
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
ID=58162878
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)
Country | Link |
---|---|
FR (1) | FR3060530B1 (en) |
Families Citing this family (3)
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)
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 |
-
2016
- 2016-12-21 FR FR1663082A patent/FR3060530B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3060530A1 (en) | 2018-06-22 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20180622 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |