CN208377064U - A kind of unmanned plane of taking photo by plane with high stability - Google Patents
A kind of unmanned plane of taking photo by plane with high stability Download PDFInfo
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- CN208377064U CN208377064U CN201820925641.1U CN201820925641U CN208377064U CN 208377064 U CN208377064 U CN 208377064U CN 201820925641 U CN201820925641 U CN 201820925641U CN 208377064 U CN208377064 U CN 208377064U
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Abstract
This application involves a kind of unmanned plane of taking photo by plane with high stability, including fuselage, control mainboard, motor, screw blade, spiral rowlock, battery, the two sides of fuselage are provided with several spiral rowlocks, motor is connected with by bracket respectively in spiral rowlock, each motor drive is connected to screw blade, the inside of fuselage is equipped with battery, battery is through control mainboard respectively for being electrically connected to each motor, the receiving storehouse of the upper end of fuselage is built-in with life saving gas cushion, life saving gas cushion includes several air bags, orlop portion is accommodated in fuselage is equipped with several high pressure gas cylinders, and each high pressure gas cylinder is connected to connection with the gas nozzle of each air bag through each safety corkage means of deflation respectively.The remote controlled flight of this unmanned plane is to rescue region and can land in the water surface, the life saving gas cushion of several air bags is set in being provided in fuselage accommodating chamber, so that high pressure gas cylinder is discharged high pressure gas by triggering corkage means of deflation and inflate the air cushion that can bubble through the water column of formation in air bag, can be climbed the mountain life saving gas cushion by rescue personnel.
Description
Technical field
The utility model relates to a kind of unmanned plane, especially a kind of unmanned plane of taking photo by plane with high stability.
Background technique
Existing water life-saving equipment mainly has lifebuoy, lifeboat etc., since large vessel is not easy close drowning man, because
This general use adds throwing device on ship and rescue aid is jettisoninged to drowning man, and adjust the distance closer drowning man
It is rescued.But the travel speed of ship is slower, and rescue response is not in time.
Due to the complexity of sea environment, rescue at sea activity generally has high difficulty, and unmanned plane is because having height
The features such as mobility, high security, can at sea play great role in pick-up operation.
Summary of the invention
The purpose of this utility model is exactly to provide a kind of with high stability in order to avoid the shortcoming in background technique
Unmanned plane of taking photo by plane.
In order to achieve the above objectives, the utility model adopts the following technical solution: a kind of to take photo by plane nobody with high stability
Machine, including fuselage, control mainboard, motor, screw blade, spiral rowlock, battery, the two sides of fuselage are connected with flight branch
Frame, a point front and back side for two sides flight bracket, which is separately connected, is provided with spiral rowlock, and each spiral rowlock longitudinally offers spiral shell respectively
Mounting hole is revolved, motor is connected with by bracket respectively in spiral mounting hole, the power output end of each motor is connected separately with spiral shell
Blade is revolved, the inside of the fuselage is equipped with battery, and the battery is through control mainboard respectively for being electrically connected to each motor, fuselage
Upper end be equipped with accommodate storehouse, accommodate storehouse be built-in with life saving gas cushion, the life saving gas cushion includes several air bags, is respectively set on air bag
There is gas nozzle；Orlop portion is accommodated in fuselage and is equipped with several high pressure gas cylinders, and high pressure gas cylinder is equipped with corkage means of deflation, and each height
Air bottle is connected to connection with the gas nozzle of each air bag through each safety corkage means of deflation respectively.
A kind of optimization for the utility model, the corkage means of deflation include valve body, are equipped with chamber, chamber in valve body
Interior to be equipped with piston, valve body inner piston upper chambers seal to form closed combustion chamber, and burning medicament is equipped in combustion chamber；In valve body
The chamber inner wall of piston underside is equipped with bottleneck connection screw thread, and the valve interior wall of piston underside chamber side is equipped with gas outlet, gas
Connection is connected to gas outlet by gas nozzle on capsule, the lower end of the piston is equipped with striker, and striker axially offers outlet gap, institute
The bottleneck for stating high pressure gas cylinder is screwed into through bottleneck connection screw thread is connected to valve body, bottleneck of the striker axially with respect to high pressure gas cylinder.
A kind of optimization for the utility model, the unmanned plane of taking photo by plane further include the point being electrically connected with control mainboard
Fiery trigger, igniting trigger are set to fuselage inner valve body side, are respectively equipped with igniter in each combustion chamber, trigger of respectively lighting a fire
It respectively corresponds and is electrically connected with igniter.
The side of a kind of optimization for the utility model, fuselage is controlled by storage battery power supply through control mainboard equipped with several
Rescue indicator light.
A kind of optimization for the utility model, the bottom outside of fuselage are connected with by storage battery power supply through control mainboard
Control infrared imaging ball machine
A kind of optimization for the utility model, fuselage upper end accommodate storehouse upper cover and are equipped with cover board.
A kind of optimization for the utility model, the life saving gas cushion side are connect with accommodating chamber bottom.
The utility model compared with the background art, have it is structurally reasonable, it is easy to make, in the initial state, the unmanned plane
The rotation of motor driven screw blade is remotely controlled through operator to take off；It is reached by controlling the different output power revolving speed of motor
To control heading；Motor speed is gradually decreased when flight to rescue region and fuselage is landed in the water surface, fuselage
Upper end offers accommodating chamber, and the interior life saving gas cushion for setting several air bags is provided in accommodating chamber, and height is provided on the downside of it
Air bottle makes high pressure gas cylinder discharge high pressure gas and inflates in air bag by triggering corkage means of deflation, at this point, cover board is flicked,
Life saving gas cushion expands into the air cushion that can be bubbled through the water column after air bag is fully aerated, can climb up life saving gas cushion by rescue personnel；
Life saving gas cushion tail end after expansion is connect with fuselage, and the motor, screw blade, spiral rowlock of fuselage side are as water surface row at this time
Into driving device, the screw blade by approximately level side as water paddle, start motor then fuselage with life saving gas cushion forward
It promotes, and the control of each motor different dynamic power enables control over the direction of travel of buoyancy fuselage；Infrared imaging ball machine
Setting on the one hand take photo by plane monitoring as flight.
Detailed description of the invention
Fig. 1 is the schematic perspective view with the unmanned plane of taking photo by plane of high stability.
Fig. 2 is the side elevational cross-section structural schematic diagram with the unmanned plane of taking photo by plane of high stability.
Fig. 3 is A enlarged drawing.
Fig. 4 is that there is the unmanned plane life saving gas cushion air bag inflation of taking photo by plane of high stability to flick rear schematic diagram.
Specific embodiment
Embodiment 1: referring to Fig.1-4.A kind of unmanned plane of taking photo by plane with high stability, including fuselage 1, control mainboard 2, electricity
Machine 3, screw blade 4, spiral rowlock 5, battery 6, the two sides of fuselage 1 are connected with flight bracket 7, two sides flight bracket 7
A point front and back side be separately connected and be provided with spiral rowlock 5, and each spiral rowlock 5 is longitudinal offers spiral mounting hole 51 respectively,
Motor 3 is connected with by bracket 52 respectively in spiral mounting hole 51, the power output end of each motor 3 is connected separately with screw blade
4, the inside of the fuselage 1 is equipped with battery 6, and the battery 6 is through control mainboard 2 respectively for being electrically connected to each motor 3, fuselage
1 upper end, which is equipped with, accommodates storehouse 11, accommodates storehouse 11 and is built-in with life saving gas cushion 8, the life saving gas cushion 8 includes several air bags 81, air bag
Gas nozzle 82 is respectively arranged on 81；11 bottom of storehouse is accommodated in fuselage 1 and is equipped with several high pressure gas cylinders 10, is divided on high pressure gas cylinder 10
Means of deflation 9 She You not be opened, and gas nozzle 82 of each high pressure gas cylinder 10 respectively through each safety corkage means of deflation 9 and each air bag connects
Lead to and connects.
The corkage means of deflation 9 includes valve body 91, and chamber 92 is equipped in valve body 91, is equipped with piston 93, valve in chamber 92
91 inner piston of body, 93 side and chamber end seal to form closed combustion chamber 94, and burning medicament 95 is equipped in combustion chamber 94；Valve
92 inner wall of chamber of 91 inner piston of body, 93 downside is equipped with bottleneck connection screw thread 96,91 inner wall of valve body of another side cavity 92 of piston 93
It is equipped with gas outlet 97, passes through gas nozzle 82 on air bag 81 and is connected to connection with gas outlet 97, the lower end of the piston 93 is equipped with striker
98, the bottleneck 101 of the high pressure gas cylinder 10 is screwed into through bottleneck connection screw thread 96 is connected to valve body 91, and striker 98 is axially with respect to height
The bottleneck 101 of air bottle 10.
The unmanned plane of taking photo by plane further includes the igniting trigger 90 being electrically connected with control mainboard 2, and igniting trigger 90 is set
It is placed in 1 inner valve body of fuselage, 91 side, is respectively equipped with igniter 99 in each combustion chamber 94, each trigger 90 of lighting a fire respectively corresponds and point
Firearm 99 is electrically connected.The side of fuselage 1 is equipped with several rescue indicator lights 12 controlled by the power supply of battery 6 through control mainboard 2.
It is to be understood that: although the present embodiment contrasts detailed description to the utility model, these are said
It is bright, only to the simple declaration of the utility model, rather than limitations of the present invention, it is any without departing from the utility model reality
Innovation and creation in matter spirit, each fall in the protection scope of the utility model.
Claims (5)
1. a kind of unmanned plane of taking photo by plane with high stability, it is characterised in that including fuselage (1), control mainboard (2), motor (3),
Screw blade (4), spiral rowlock (5), battery (6), the two sides of fuselage (1) are connected with flight bracket (7), two sides flight
A point front and back side for bracket (7), which is separately connected, to be provided with spiral rowlock (5), and each spiral rowlock (5) longitudinally offers spiral respectively
Mounting hole (51) is connected with motor (3) by bracket (52) respectively in spiral mounting hole (51), and the power of each motor (3) is defeated
Outlet is connected separately with screw blade (4), and the inside of the fuselage (1) is equipped with battery (6), and the battery (6) is through controlling
For mainboard (2) respectively for being electrically connected to each motor (3), the upper end of fuselage (1), which is equipped with, accommodates storehouse (11), accommodates and can be saved built in storehouse (11)
Anger pad (8), the life saving gas cushion (8) includes several air bags (81), and gas nozzle (82) are respectively arranged on air bag (81)；Fuselage
(1) storehouse (11) bottom is accommodated in and is equipped with several high pressure gas cylinders (10), is respectively equipped on high pressure gas cylinder (10) and is opened dress of deflating
It sets (9), and each high pressure gas cylinder (10) is connected to connection with the gas nozzle (82) of each air bag through each safety corkage means of deflation (9) respectively,
The bottom outside of fuselage (1), which is connected with, controls infrared imaging ball machine (13) through control mainboard (2) by battery (6) power supply.
2. the unmanned plane of taking photo by plane according to claim 1 with high stability, it is characterized in that: the corkage means of deflation
(9) include valve body (91), be equipped with chamber (92) in valve body (91), be equipped with piston (93) in chamber (92), valve body (91) inner piston
(93) side and chamber end seal to be formed closed combustion chamber (94), and burning medicament (95) is equipped in combustion chamber (94)；Valve body
(91) chamber (92) inner wall on the downside of inner piston (93) is equipped with bottleneck connection screw thread (96), piston (93) another side cavity (92)
Valve body (91) inner wall is equipped with gas outlet (97), is connected to connection with gas outlet (97) by gas nozzle (82) on air bag (81), described
The lower end of piston (93) is equipped with striker (98), and the bottleneck (101) of the high pressure gas cylinder (10) is screwed into through bottleneck connection screw thread (96)
It is connected to valve body (91), bottleneck (101) of the striker (98) axially with respect to high pressure gas cylinder (10).
3. the unmanned plane of taking photo by plane according to claim 2 with high stability, it is characterised in that further include and control mainboard
(2) the igniting trigger (90) being electrically connected, igniting trigger (90) are set to fuselage (1) inner valve body (91) side, each to burn
Igniter (99) are respectively equipped in room (94), respectively igniting trigger (90) is respectively corresponded is electrically connected with igniter (99).
4. the unmanned plane of taking photo by plane according to claim 1 with high stability, it is characterized in that: the side of fuselage (1) is equipped with
Several rescue indicator lights (12) controlled by battery (6) power supply through control mainboard (2).
5. the unmanned plane of taking photo by plane according to claim 1 with high stability, it is characterized in that: fuselage (1) upper end accommodates storehouse
(11) upper cover is equipped with cover board (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820925641.1U CN208377064U (en) | 2018-06-14 | 2018-06-14 | A kind of unmanned plane of taking photo by plane with high stability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820925641.1U CN208377064U (en) | 2018-06-14 | 2018-06-14 | A kind of unmanned plane of taking photo by plane with high stability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208377064U true CN208377064U (en) | 2019-01-15 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820925641.1U Active CN208377064U (en) | 2018-06-14 | 2018-06-14 | A kind of unmanned plane of taking photo by plane with high stability |
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| Country | Link |
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| CN (1) | CN208377064U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110435849A (en) * | 2019-08-21 | 2019-11-12 | 泰州市柯普尼通讯设备有限公司 | Small rescue unmanned plane |
-
2018
- 2018-06-14 CN CN201820925641.1U patent/CN208377064U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110435849A (en) * | 2019-08-21 | 2019-11-12 | 泰州市柯普尼通讯设备有限公司 | Small rescue unmanned plane |
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