CN111252254A - Small gas generating device for parachute of unmanned aerial vehicle - Google Patents

Small gas generating device for parachute of unmanned aerial vehicle Download PDF

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Publication number
CN111252254A
CN111252254A CN201811461119.3A CN201811461119A CN111252254A CN 111252254 A CN111252254 A CN 111252254A CN 201811461119 A CN201811461119 A CN 201811461119A CN 111252254 A CN111252254 A CN 111252254A
Authority
CN
China
Prior art keywords
container
parachute
aerial vehicle
unmanned aerial
gas generating
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.)
Pending
Application number
CN201811461119.3A
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Chinese (zh)
Inventor
周良玉
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.)
Harbin Huoying Technology Co ltd
Original Assignee
Harbin Huoying Technology Co ltd
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 Harbin Huoying Technology Co ltd filed Critical Harbin Huoying Technology Co ltd
Priority to CN201811461119.3A priority Critical patent/CN111252254A/en
Publication of CN111252254A publication Critical patent/CN111252254A/en
Pending legal-status Critical Current

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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

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

The invention discloses a small-sized gas generating device for an unmanned aerial vehicle parachute, which comprises a container 1, an ignition head 2 and a control panel 3, and is characterized in that: the container comprises an ignition head 2, ceramic fiber paper 4, gas generating agent 5 and flame control agent 6, the bottom of the container is provided with an ignition head control plate 3, and the top of the container is sealed with a silica gel sheet 7. The ceramic fiber paper 4 in the container 1 has a fireproof effect, the ignition head 2 is controlled by the control panel 3, and after the control panel 3 sends out an instruction, the ignition head 2 quickly ignites the gas generating agent 5, so that enough gas is generated to spray the parachute. The invention has the advantages that: simple structure, small volume, fast reaction speed and good umbrella opening effect.

Description

Small gas generating device for parachute of unmanned aerial vehicle
Technical Field
The invention relates to the field of unmanned aerial vehicle parachutes, in particular to a small gas generating device for an unmanned aerial vehicle parachute.
Background
Along with the growth in the unmanned aerial vehicle market, unmanned aerial vehicle safety problem arouses people's concern more and more, and the damage that unmanned aerial vehicle parachute can effectually reduce the unmanned aerial vehicle and fall, and the main use of present unmanned aerial vehicle parachute opening system is the mode of launching the parachute, and its mode of launching has the structure complicacy to influence duration, launches defects such as parachute opening time overlength, mechanical failure rate height.
Disclosure of Invention
The invention aims to solve the problem of the defects and provides a small gas generating device for an unmanned aerial vehicle parachute.
The technical scheme adopted for realizing the purpose is as follows: the utility model provides a small-size gas generator for unmanned aerial vehicle parachute, includes container, ignition head, control panel, its characterized in that: the container comprises an ignition head, ceramic fiber paper, a gas generating agent and a flame control agent, the bottom of the container is provided with a control plate, and the top of the container is sealed with a silica gel sheet.
A small-size gas generator for unmanned aerial vehicle parachute, gas generator is H type nitrocotton.
A small-size gas generator for unmanned aerial vehicle parachute, flame control agent contains NH4H2PO4、(NH4)SO4And talc.
The invention has the advantages that: simple structure, small volume, fast reaction speed and good umbrella opening effect.
Drawings
FIG. 1 is a schematic view of a small gas generator for a parachute of an unmanned aerial vehicle according to the present invention;
wherein: 1. a container; 2. an ignition head; 3. a control panel; 4. ceramic fiber paper; 5. a gas generating agent; 6. a flame control agent; 7. a silica gel sheet.
Detailed Description
The invention will be described in further detail with reference to the accompanying drawings and embodiments.
Referring to fig. 1, a small-sized gas generating device for an unmanned aerial vehicle parachute according to an embodiment of the present invention includes a container 1, an ignition head 2, and a control panel 3, and is characterized in that: the container comprises an ignition head 2, ceramic fiber paper 4, gas generating agent 5 and flame control agent 6, the bottom of the container is provided with an ignition head control plate 3, and the top of the container is sealed with a silica gel sheet 7. The ceramic fiber paper 4 in the container 1 has a fireproof effect, the ignition head 2 is controlled by the control panel 3, and after the control panel 3 sends out an instruction, the ignition head 2 quickly ignites the gas generating agent 5, so that enough gas is generated to spray the parachute.
A small-size gas generator for unmanned aerial vehicle parachute, gas generant 5 is H type nitrocotton. The gas generating agent 5 is combusted to generate sufficient gas to be ejected by the parachute.
A little for unmanned aerial vehicle parachuteIn the gas generator, the flame control agent 6 contains NH4H2PO4、(NH4)SO4And talc. The flame controller 6 can effectively control the flame generated by the combustion of the gas generating agent 5, prevent the parachute from being burnt by the flame, and reduce the potential safety hazard of the combustion.
It will be apparent to those skilled in the art that modifications and equivalents may be made in the embodiments and/or portions thereof without departing from the spirit and scope of the present invention.

Claims (3)

1. The utility model provides a small-size gas generator for unmanned aerial vehicle parachute, includes container, ignition head, control panel, its characterized in that: the container comprises an ignition head, ceramic fiber paper, a gas generating agent and a flame control agent, the bottom of the container is provided with a control plate, and the top of the container is sealed with a silica gel sheet.
2. A small gas generator for a parachute of an unmanned aerial vehicle according to claim 1, wherein: the gas generating agent is H-type nitrocotton.
3. A small gas generator for a parachute of an unmanned aerial vehicle according to claim 1, wherein: the flame control agent contains NH4H2PO4、(NH4)SO4And talc.
CN201811461119.3A 2018-12-01 2018-12-01 Small gas generating device for parachute of unmanned aerial vehicle Pending CN111252254A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811461119.3A CN111252254A (en) 2018-12-01 2018-12-01 Small gas generating device for parachute of unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811461119.3A CN111252254A (en) 2018-12-01 2018-12-01 Small gas generating device for parachute of unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN111252254A true CN111252254A (en) 2020-06-09

Family

ID=70948358

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811461119.3A Pending CN111252254A (en) 2018-12-01 2018-12-01 Small gas generating device for parachute of unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN111252254A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6565042B1 (en) * 2001-11-21 2003-05-20 Yamada Dobby Co., Ltd. Emergency parachute
CN203958622U (en) * 2014-07-03 2014-11-26 青岛宏百川金属精密制品有限公司 Depopulated helicopter parachute emission coefficient
CN105484267A (en) * 2015-12-31 2016-04-13 中交一航局第二工程有限公司 Deep-water high-flow-speed fixed-point accurate throwing and filling device and construction method
CN106828939A (en) * 2016-12-26 2017-06-13 河南大诚通用航空科技有限公司 A kind of unmanned plane and its parachute opener
CN107933933A (en) * 2017-11-26 2018-04-20 合肥赛为智能有限公司 A kind of unmanned plane parachute novel ejection constructional device
CN208021761U (en) * 2018-03-19 2018-10-30 北京中科遥数信息技术有限公司 A kind of unmanned plane parachute

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6565042B1 (en) * 2001-11-21 2003-05-20 Yamada Dobby Co., Ltd. Emergency parachute
CN203958622U (en) * 2014-07-03 2014-11-26 青岛宏百川金属精密制品有限公司 Depopulated helicopter parachute emission coefficient
CN105484267A (en) * 2015-12-31 2016-04-13 中交一航局第二工程有限公司 Deep-water high-flow-speed fixed-point accurate throwing and filling device and construction method
CN106828939A (en) * 2016-12-26 2017-06-13 河南大诚通用航空科技有限公司 A kind of unmanned plane and its parachute opener
CN107933933A (en) * 2017-11-26 2018-04-20 合肥赛为智能有限公司 A kind of unmanned plane parachute novel ejection constructional device
CN208021761U (en) * 2018-03-19 2018-10-30 北京中科遥数信息技术有限公司 A kind of unmanned plane parachute

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Application publication date: 20200609