CN111976979A - Wearable personal aircraft - Google Patents
Wearable personal aircraft Download PDFInfo
- Publication number
- CN111976979A CN111976979A CN201910422426.9A CN201910422426A CN111976979A CN 111976979 A CN111976979 A CN 111976979A CN 201910422426 A CN201910422426 A CN 201910422426A CN 111976979 A CN111976979 A CN 111976979A
- Authority
- CN
- China
- Prior art keywords
- engine
- handheld
- backpack
- control system
- wearable personal
- 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.)
- Withdrawn
Links
- 230000001681 protective effect Effects 0.000 claims description 8
- 238000009413 insulation Methods 0.000 claims description 6
- 239000002828 fuel tank Substances 0.000 claims description 2
- 239000003921 oil Substances 0.000 description 31
- 238000004321 preservation Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 239000012212 insulator Substances 0.000 description 2
- 230000008054 signal transmission Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/04—Arrangement thereof in or on aircraft
-
- 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
- B64D43/00—Arrangements or adaptations of instruments
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Helmets And Other Head Coverings (AREA)
Abstract
The invention discloses a wearable personal aircraft, which comprises a first handheld engine set, a second handheld engine set, a backpack engine, a control system, an engine bracket, an oil tank and a display helmet, wherein the backpack engine is installed on one side of the engine bracket, the oil tank is installed on both sides of the engine bracket, the control system is arranged on one side of the backpack engine, the first handheld engine set and the second handheld engine set are respectively connected to the control system and the oil tank through a power line and an oil pipe, and the display helmet is arranged at the top end of the engine bracket; the first handheld engine unit and the second handheld engine unit comprise handheld engines and hand fixing pieces; the hand fixing member is worn on the hand. The invention is easy to wear, is simple like wearing clothes, has small volume and convenient carrying, and has the advantages of simple structure, stable and safe performance and capability of being used in various environments.
Description
Technical Field
The invention relates to the technical field of personal aircrafts, in particular to a wearable personal aircraft.
Background
A personal aircraft is any flying object made by humans, capable of flying off the ground, flying in space, and controlled by humans, that is provided for personal use. With the popularity of aircraft, personal aircraft are certainly the direction of future development. The low-speed aircraft is a development direction of personal aircraft, and provides a new traffic mode for relieving the current urban traffic problem; the novel solution and the method are provided for avoiding disasters and accidents such as high-rise collapse, fire escape, earthquake disaster escape, flood disaster escape, forest search and rescue and the like, but the existing personal aircraft is inconvenient to wear, carry due to large volume, unstable and safe in performance and incapable of being used in various environments.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention provides the wearable personal aircraft, which solves the problems that the conventional personal aircraft is inconvenient to wear, large in size and carry, unstable and safe in performance and incapable of being used in various environments.
In order to achieve the purpose, the invention provides the following technical scheme: the portable engine comprises a first handheld engine set, a second handheld engine set, a backpack engine, a control system, an engine support, an oil tank and a display helmet, wherein the backpack engine is installed on one side of the engine support;
the first handheld engine unit and the second handheld engine unit respectively comprise a handheld engine and a hand fixing piece, the hand fixing piece is worn on a hand, an accelerator control system is integrated on the hand fixing piece, and the accelerator control system is electrically connected with the control system through a data line;
The backpack type engine comprises a backpack and a thrust engine, and the backpack is fixedly connected with the engine bracket;
control system includes controller, GPS locator, speedtransmitter, level sensor and altitude sensor, and one side of controller is provided with the GPS locator, and one side of GPS locator is provided with speedtransmitter, and one side of speedtransmitter is provided with altitude sensor, and level sensor installs in the inside of oil tank, the equal electric connection controller's of GPS locator, speedtransmitter, level sensor and altitude sensor output input, the output electric connection of controller shows the input of helmet.
According to the technical scheme, the backpack type engine, the control system, the engine bracket and the oil tank are all located inside the backpack.
According to the technical scheme, the engines in the first handheld engine unit, the second handheld engine unit and the backpack type engine are all turbojet engines.
According to the technical scheme, one side of the display helmet is provided with the warning lamp, the position above the other side of the display helmet is provided with the windshield, the upper side of the display helmet is provided with the imager, one side of the imager is provided with the camera, the heat insulator is wrapped on the inner wall of the display helmet, and the inside of the heat insulator is provided with the USB interface.
According to the technical scheme, the number of the warning lamps is two, and the two warning lamps are respectively arranged on one side of the display helmet and above the imager.
According to the technical scheme, the output ends of the imager and the camera are electrically connected with the input end of the controller, and the output end of the controller is electrically connected with the warning lamp and the USB interface.
According to the technical scheme, the number of the oil tanks is two, the top end of each oil tank is provided with an oil inlet, the outer side of each oil inlet is provided with a protective cover, and the outer side of each oil inlet is provided with a heat insulation layer.
According to the technical scheme, the oil inlet is in threaded connection with the protective cover.
The invention is easy to wear, is simple like wearing clothes, has small volume, is convenient to carry, and has the advantages of simple structure, stable and safe performance and capability of being used in various environments.
Drawings
The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:
FIG. 1 is a schematic three-dimensional structure of the present invention.
Fig. 2 is a schematic view of the structure of the helmet of the present invention.
Fig. 3 is a schematic structural diagram of the control system of the present invention.
Fig. 4 is a schematic structural view of the fuel tank of the present invention.
Detailed Description
The following description of the embodiments of the present invention will be made in detail with reference to the accompanying drawings 1 to 4.
In the first embodiment, as shown in fig. 1, 2, 3 and 4, the present invention includes a first handheld engine unit 1, a second handheld engine unit 2, a backpack engine 3, a control system 4, an engine mount 5, the portable engine comprises an oil tank 6 and a display helmet 7, wherein a backpack type engine 3 is installed on one side of an engine support 5, the oil tank 6 is installed on each of two sides of the engine support 5, a control system 4 is arranged on one side of the backpack type engine 3, a first handheld engine unit 1 and a second handheld engine unit 2 are respectively connected to the control system 4 and the oil tank 6 through power lines and oil pipes, the display helmet 7 is arranged at the top end of the engine support 5 and comprises the first handheld engine unit 1, the second handheld engine unit 2, the backpack type engine 3, the control system 4, the engine support 5, the oil tank 6 and the display helmet 7, and two engines are arranged on each hand; worn on the hand; and the engine 8 integrated behind the throttle control system 10 provides the main thrust, and the engine 8 and other control systems 4 are carried on the back; the angle of the hand-held engine 8 is changed to realize steering and front-back running, the thrust of the engine 8 is controlled by a hand-held throttle switch, the thrust balance of the engine 8 is realized by the control system 4, and the air is pushed by the turbojet engine 8 to fly; the aircraft is easy to wear, simple like wearing clothes, small in size and convenient to carry, and has the advantages of simple structure, stable and safe performance and capability of being used in various environments;
The first handheld engine unit 1 and the second handheld engine unit 2 both comprise a handheld engine 8 and a hand fixing piece 9, the hand fixing piece 9 is worn on a hand, an accelerator control system 1O is integrated on the hand fixing piece 9, and an accelerator control system 10 is electrically connected with the control system 4 through a data line;
the backpack type engine 3 comprises a backpack 11 and a thrust engine 12, and the backpack 11 is fixedly connected with the engine bracket 5;
According to the technical scheme, the backpack type engine 3, the control system 4, the engine bracket 5 and the oil tank 6 are all positioned in the backpack 11, so that the backpack type engine 3, the control system 4, the engine bracket 5 and the oil tank 6 are protected conveniently.
According to the technical scheme, the engines in the first handheld engine unit 1, the second handheld engine unit 2 and the backpack type engine 3 are turbojet engines, and power is conveniently and better provided through the turbojet engines.
According to the technical scheme, one side of the display helmet 7 is provided with the warning light 20, the upper position of the other side of the display helmet 7 is provided with the windshield 18, the upper side of the display helmet 7 is provided with the imager 22, one side of the imager 22 is provided with the camera 23, the heat preservation body 21 wraps up on the inner wall of the display helmet 7, the inside of the heat preservation body 21 is provided with the USB interface 19, the warning light 20 is passed through during use, the reminding function is convenient to have, the data abnormity can not be seen during use, the windshield 18 and the heat preservation body 21 are passed through, the head of a user can be protected conveniently, the flight video can be recorded conveniently through the imager 22 and the camera 23, the transmission is transmitted to the controller 13, the controller 13 is used for processing and storing, and the data transmission is facilitated through the USB interface 19.
According to the above technical solution, the warning lamps 20 are provided with two, and the two warning lamps 20 are respectively installed on one side of the display helmet 7 and above the imager 22, so as to have a better warning effect.
According to the above technical solution, the output ends of the imager 22 and the camera 23 are electrically connected to the input end of the controller 13, and the output end of the controller 13 is electrically connected to the warning light 20 and the USB interface 19, so as to facilitate signal transmission.
According to the technical scheme, the number of the oil tanks 6 is two, the top end of the oil tank 6 is provided with the oil inlet 24, the outer side of the oil inlet 24 is provided with the protective cover 25, the outer side of the oil inlet 24 is provided with the heat insulation layer 26, the oil is convenient to add through the oil inlet 24 during use, fuel oil leakage is convenient to prevent through the protective cover 25, the oil tank 6 is convenient to protect through the heat insulation layer 26 during use, and the oil tank 6 is prevented from being overheated.
According to the technical scheme, the oil inlet 24 is connected with the protective cover 25 through threads, and the protective cover 25 is convenient to mount and dismount through the threads.
The invention comprises a first handheld engine set 1, a second handheld engine set 2, a backpack type engine 3, a control system 4, an engine bracket 5, an oil tank 6 and a display helmet 7, wherein two engines are arranged on each hand; worn on the hand; and the engine 8 integrated behind the throttle control system 10 provides the main thrust, and the engine 8 and other control systems 4 are carried on the back; the angle of the hand-held engine 8 is changed to realize steering and front-back running, the thrust of the engine 8 is controlled by a hand-held throttle switch, the thrust balance of the engine 8 is realized by the control system 4, and the air is pushed by the turbojet engine 8 to fly; the aircraft is easy to wear, simple like wearing clothes, small in size and convenient to carry, and has the advantages of simple structure, stable and safe performance and capability of being used in various environments, the weight of each engine used by the first handheld engine unit 1 and the second handheld engine unit 2 is 1.6 kilograms, and the thrust of each engine is 22 kilograms; the weight of two engines in each hand and the weight of an engine bracket 5, a lead, an accelerator control and an oil pipe are 5 kilograms, the total thrust of the first handheld engine unit 1 and the second handheld engine unit 2 is 88 kilograms, the weight of the backpack type engine 3 is 2.6 kilograms, the bracket is 5 kilograms, the weight of the oil filled in the oil tank 6 is 18 kilograms, the thrust of the backpack type engine 3 is 55 kilograms, the maximum flying speed is 40 kilometers per hour, the flying time is 5-10 minutes, and the theoretical flying height is more than 500 meters.
The invention is easy to wear, is simple like wearing clothes, has small volume and convenient carrying, and has the advantages of simple structure, stable and safe performance and capability of being used in various environments.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. The wearable personal aircraft is characterized by comprising a first handheld engine set (1), a second handheld engine set (2), a backpack engine (3), a control system (4), an engine support (5), an oil tank (6) and a display helmet (7), wherein the backpack engine (3) is installed on one side of the engine support (5), the oil tank (6) is installed on two sides of the engine support (5), the control system (4) is arranged on one side of the backpack engine (3), the first handheld engine set (1) and the second handheld engine set (2) are respectively connected to the control system (4) and the oil tank (6) through power lines and oil pipes, and the display helmet (7) is arranged at the top end of the engine support (5);
The first handheld engine unit (1) and the second handheld engine unit (2) respectively comprise a handheld engine (8) and a hand fixing piece (9), the hand fixing piece (9) is worn on a hand, an accelerator control system (10) is integrated on the hand fixing piece (9), and the accelerator control system (10) is electrically connected with the control system (4) through a data line;
the backpack type engine (3) comprises a backpack (11) and a thrust engine (12), and the backpack (11) is fixedly connected with the engine bracket (5);
control system (4) are including controller (13), GPS locator (14), speedtransmitter (15), level sensor (16) and altitude sensor (17), one side of controller (13) is provided with GPS locator (14), one side of GPS locator (14) is provided with speedtransmitter (15), one side of speedtransmitter (15) is provided with altitude sensor (16), the inside at oil tank (6) is installed in level sensor (16), GPS locator (14), speedtransmitter (15), the equal electric connection of output of level sensor (16) and altitude sensor (17) controller (13)'s input, the input of output electric connection display helmet (7) of controller (13).
2. A wearable personal aircraft according to claim 1, characterized in that the backpack engine (3), control system (4), engine mounts (5) and fuel tanks (6) are located inside the backpack (11).
3. A wearable personal aircraft according to claim 1, characterized in that the engines in the first handheld engine block (1), the second handheld engine block (2) and the backpack engine (3) are all turbojet engines.
4. A wearable personal aircraft according to claim 1, characterized in that a warning light (20) is provided on one side of the display helmet (7), a windshield (18) is provided above the other side of the display helmet (7), an imager (22) is provided above the display helmet (7), a camera (23) is provided on one side of the imager (22), the thermal insulation body (21) is wrapped on the inner wall of the display helmet (7), and a USB interface (19) is provided inside the thermal insulation body (21).
5. A wearable personal aircraft according to claim 4, characterized in that there are two warning lights (20) and two warning lights (20) are mounted on one side of the display helmet (7) and above the imager (22), respectively.
6. A wearable personal aircraft according to claim 4, wherein the output of the imager (22) and the camera (23) are electrically connected to the input of the controller (13), and the output of the controller (13) is electrically connected to the warning light (20) and the USB interface (19).
7. A wearable personal aircraft according to claim 1, characterized in that the number of the oil tanks (6) is two, the top end of the oil tank (6) is provided with an oil inlet (24), the outside of the oil inlet (24) is provided with a protective cover (25), and the outside of the oil inlet (24) is provided with a thermal insulation layer (26).
8. A wearable personal aircraft according to claim 7, characterized in that the oil inlet (24) and the protective cover (25) are in threaded connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910422426.9A CN111976979A (en) | 2019-05-21 | 2019-05-21 | Wearable personal aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910422426.9A CN111976979A (en) | 2019-05-21 | 2019-05-21 | Wearable personal aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111976979A true CN111976979A (en) | 2020-11-24 |
Family
ID=73435873
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910422426.9A Withdrawn CN111976979A (en) | 2019-05-21 | 2019-05-21 | Wearable personal aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111976979A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112937862A (en) * | 2021-04-13 | 2021-06-11 | 国网河北省电力有限公司石家庄供电分公司 | Wearable jet-propelled insulation aircraft |
| CN113716039A (en) * | 2021-08-30 | 2021-11-30 | 山东元一动力科技有限公司 | Jet power flight pedal device |
| CN115738112A (en) * | 2022-10-24 | 2023-03-07 | 北京市科学技术研究院城市安全与环境科学研究所 | Rapid emergency device and method for maintenance operators in closed space |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040061023A1 (en) * | 2002-08-15 | 2004-04-01 | Kingting Lau | Superman air motor |
| US20040231903A1 (en) * | 2003-05-23 | 2004-11-25 | Shayan Shaahin Sean | Supplementary propulsion backpack and methods of use |
| US20080142644A1 (en) * | 2006-12-15 | 2008-06-19 | O'roark Corey | Flight apparatus having movable motors |
| WO2011002517A2 (en) * | 2009-07-03 | 2011-01-06 | Jon Kunowski | Turbine powered personal flight system |
| CN102556348A (en) * | 2010-12-23 | 2012-07-11 | 马世强 | Dynamic-suspension jet backpack |
| CN204411618U (en) * | 2015-01-30 | 2015-06-24 | 马鞍山市赛迪智能科技有限公司 | A kind of aircraft formula mountain-climbing booster |
| CN205554589U (en) * | 2016-04-21 | 2016-09-07 | 孟令成 | Jet -propelled knapsack of tape unit wing |
| US20170015419A1 (en) * | 2015-06-26 | 2017-01-19 | Nelson Tyler | Back Mounted Flight Machine |
| GB201702852D0 (en) * | 2017-02-22 | 2017-04-05 | Gravity Ind Ltd | A flight system |
| CN108791756A (en) * | 2017-04-29 | 2018-11-13 | 徐曙辉 | Portable pressure spraying machine |
-
2019
- 2019-05-21 CN CN201910422426.9A patent/CN111976979A/en not_active Withdrawn
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040061023A1 (en) * | 2002-08-15 | 2004-04-01 | Kingting Lau | Superman air motor |
| US20040231903A1 (en) * | 2003-05-23 | 2004-11-25 | Shayan Shaahin Sean | Supplementary propulsion backpack and methods of use |
| US20080142644A1 (en) * | 2006-12-15 | 2008-06-19 | O'roark Corey | Flight apparatus having movable motors |
| WO2011002517A2 (en) * | 2009-07-03 | 2011-01-06 | Jon Kunowski | Turbine powered personal flight system |
| CN102556348A (en) * | 2010-12-23 | 2012-07-11 | 马世强 | Dynamic-suspension jet backpack |
| CN204411618U (en) * | 2015-01-30 | 2015-06-24 | 马鞍山市赛迪智能科技有限公司 | A kind of aircraft formula mountain-climbing booster |
| US20170015419A1 (en) * | 2015-06-26 | 2017-01-19 | Nelson Tyler | Back Mounted Flight Machine |
| CN205554589U (en) * | 2016-04-21 | 2016-09-07 | 孟令成 | Jet -propelled knapsack of tape unit wing |
| GB201702852D0 (en) * | 2017-02-22 | 2017-04-05 | Gravity Ind Ltd | A flight system |
| CN108791756A (en) * | 2017-04-29 | 2018-11-13 | 徐曙辉 | Portable pressure spraying machine |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112937862A (en) * | 2021-04-13 | 2021-06-11 | 国网河北省电力有限公司石家庄供电分公司 | Wearable jet-propelled insulation aircraft |
| CN113716039A (en) * | 2021-08-30 | 2021-11-30 | 山东元一动力科技有限公司 | Jet power flight pedal device |
| CN115738112A (en) * | 2022-10-24 | 2023-03-07 | 北京市科学技术研究院城市安全与环境科学研究所 | Rapid emergency device and method for maintenance operators in closed space |
| CN115738112B (en) * | 2022-10-24 | 2023-12-15 | 北京市科学技术研究院城市安全与环境科学研究所 | Quick emergency device and method for maintenance operators in airtight space |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN111976979A (en) | Wearable personal aircraft | |
| KR102149586B1 (en) | Unmanned aerial vehicle for fire fighting and rescue | |
| US10059437B2 (en) | Multi-rotor safety shield | |
| CN102774492B (en) | A kind of small-sized depopulated helicopter fuselage | |
| WO2020052105A1 (en) | Fully electric driven fire-fighting unmanned aerial vehicle | |
| CN204497664U (en) | Based on the power transmission line block removing device of Multi-axis aircraft | |
| CN106628142A (en) | Unmanned aerial vehicle for air sampling detection and combustible and explosive gas pre-warning and monitoring | |
| CN110816823A (en) | Many rotor unmanned aerial vehicle with smog recognition function | |
| CN205366060U (en) | Make a video recording round clock and use unmanned aerial vehicle | |
| SE8402466D0 (en) | NEGATIVE INCREASE WARNING SYSTEM AFTER STARTING | |
| CN107942348B (en) | Road law enforcement system based on unmanned aerial vehicle and robot technique | |
| CN205545694U (en) | From electricity generation high altitude monitoring device | |
| CN107717942A (en) | A kind of small-sized scouting self-balance robot | |
| CN205615720U (en) | Unmanned aerial combustible gas listens thermal imaging ware of taking photo by plane | |
| CN210479049U (en) | Plant protection patrols and examines and uses oil-electricity hybrid unmanned aerial vehicle | |
| CN210882619U (en) | Fire control unmanned aerial vehicle | |
| CN207658061U (en) | A kind of unmanned plane for Fight Fire in Forest based on Internet of Things | |
| CN209305830U (en) | A kind of fire-fighting unmanned plane being driven by pure electric power | |
| CN207518687U (en) | A kind of aerospace camera | |
| CN107839887B (en) | Automatic unmanned aerial vehicle protector drops | |
| CN205203407U (en) | Unmanned aerial vehicle with firebreak device falls | |
| CN218734310U (en) | Ground control station picture transmission information processing terminal | |
| CN221043071U (en) | Satellite mapping camera | |
| CN204473168U (en) | A kind of camera case of holder for aerial photographing | |
| CN219020336U (en) | High-resistance fire-fighting safety helmet |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210408 Address after: No.323, Yuhe street, zenpu District, Guangzhou City, Guangdong Province Applicant after: Guangdong Huitian Aerospace Technology Co.,Ltd. Address before: 661300 602, unit 1, Family Planning Bureau community, Hekou County, Honghe Prefecture, Yunnan Province Applicant before: Liu Dongsheng |
|
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20201124 |