CN111252254A - Small gas generating device for parachute of unmanned aerial vehicle - Google Patents
Small gas generating device for parachute of unmanned aerial vehicle Download PDFInfo
- 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
Links
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 18
- 239000000919 ceramic Substances 0.000 claims abstract description 7
- 239000000835 fiber Substances 0.000 claims abstract description 7
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 5
- 239000000741 silica gel Substances 0.000 claims abstract description 5
- 229910002027 silica gel Inorganic materials 0.000 claims abstract description 5
- LFVGISIMTYGQHF-UHFFFAOYSA-N ammonium dihydrogen phosphate Chemical compound [NH4+].OP(O)([O-])=O LFVGISIMTYGQHF-UHFFFAOYSA-N 0.000 claims description 3
- 229920001220 nitrocellulos Polymers 0.000 claims description 3
- 239000000454 talc Substances 0.000 claims description 3
- 229910052623 talc Inorganic materials 0.000 claims description 3
- 230000036632 reaction speed Effects 0.000 abstract description 2
- 239000007921 spray Substances 0.000 abstract description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Images
Classifications
-
- 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
-
- 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
Landscapes
- 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
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.
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 |
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CN (1) | CN111252254A (en) |
Citations (6)
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 |
-
2018
- 2018-12-01 CN CN201811461119.3A patent/CN111252254A/en active Pending
Patent Citations (6)
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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SE01 | Entry into force of request for substantive examination | ||
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WD01 | Invention patent application deemed withdrawn after publication | ||
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Application publication date: 20200609 |