CN207157539U - A kind of low flyer that can be manned - Google Patents
A kind of low flyer that can be manned Download PDFInfo
- Publication number
- CN207157539U CN207157539U CN201721178325.4U CN201721178325U CN207157539U CN 207157539 U CN207157539 U CN 207157539U CN 201721178325 U CN201721178325 U CN 201721178325U CN 207157539 U CN207157539 U CN 207157539U
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- Prior art keywords
- controller
- electrically connected
- circuit
- bottom plate
- battery
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Abstract
The utility model discloses a kind of low flyer that can be manned.The utility model on front side of bottom plate by setting rangefinder and buzzer alarm,And the coulometric detector of base plate interior link battery,Distance apart from barrier on front side of bottom plate is less than arranges value,Then rangefinder communicates information to controller,Controller control buzzer alarm sends alarm,When accumulator electric-quantity is less than setting electricity,Then communicate information to controller,Controller control buzzer alarm sends alarm,Can effectively avoid that accident occurs,Console is provided with the top of the bottom plate,Console both sides are provided with pedal,Pressure sensor is provided with before and after inside the pedal,After two pin step on,Body rocks the gravity tendency for changing pin,Controller calculates the incline direction of human body according to the information of each pressure sensor transmission,Generation flight directive is sent to flight controller,Flight controller controls each motor power (output) to realize the heading of equipment.
Description
Technical field
The utility model is specifically related to a kind of low flyer that can be manned, belongs to toy trip field of tool.
Background technology
Existing aircraft controls complexity in flight, therefore, it is proposed that a kind of low flyer that can be manned.
Utility model content
The technical problems to be solved in the utility model overcomes the defects of existing, there is provided a kind of low flyer that can be manned,
By setting rangefinder and buzzer alarm, and the coulometric detector of base plate interior link battery on front side of bottom plate, work as bottom
Distance on front side of plate apart from barrier is less than arranges value, then rangefinder communicates information to controller, controller control buzzing police
Report device sends alarm, and electricity is set when accumulator electric-quantity is less than, then communicates information to controller, controller control buzzing alarming
Device sends alarm, can effectively avoid that accident occurs, and console is provided with the top of the bottom plate, and console both sides are provided with pedal,
Pressure sensor is provided with before and after inside the pedal, after two pin step on, body rocks the gravity tendency for changing pin, control
Device processed calculates the incline direction of human body according to the information of each pressure sensor transmission, and generation flight directive is sent to flight control
Device processed, flight controller control each motor power (output) to realize the heading of equipment, effectively can solved in background technology
The problem of.
In order to solve the above-mentioned technical problem, the utility model provides following technical scheme：
The utility model provides a kind of low flyer that can be manned, including bottom plate, side plate, backplate and console, described
Side plate is arranged at bottom plate both sides, and the side plate front side and rear side are equipped with propeller, motor are provided with the propeller, described
Solar panel is provided with the middle part of side plate, the backplate is arranged at both sides at the top of bottom plate, and the console is arranged at plate top surface
Middle part, the console both sides are equipped with pedal, are sequentially provided with two pressure sensors inside the pedal from front to back, described
Charge port, rangefinder and buzzer alarm are sequentially provided with from left to right on front side of bottom plate, and the base plate interior is provided with battery, described
Battery side is provided with controller for solar, and the battery opposite side is provided with charging chip, and the battery top is past from a left side
The right side is sequentially provided with controller, flight controller and coulometric detector.
Preferably, the four groups of pressure sensors set on the pedal of the console both sides pass through circuit and controller electricity
Property connection, be respectively equipped with stop key and start key, the stop key and startup at the top of two side plates set at the top of the bottom plate
Key is electrically connected with by circuit and controller.
Preferably, the solar panel is electrically connected with by circuit and controller for solar, the solar control
Device is electrically connected with by circuit and battery, and the charge port is electrically connected with by circuit and charging chip, the charging chip
It is electrically connected with by circuit and battery, the charging chip is electrically connected with controller and flight controller respectively by circuit
Connect, the battery is electrically connected with by circuit and coulometric detector, and the coulometric detector is electrical with controller by circuit
Connection.
Preferably, the rangefinder is electrically connected with by circuit and controller, and the buzzer alarm passes through circuit and control
Device processed is electrically connected with.
Preferably, the motor set in the propeller is electrically connected with by circuit and flight controller, the flight
Controller is electrically connected with by circuit and controller.
The beneficial effect that the utility model is reached is：By setting rangefinder and buzzer alarm on front side of bottom plate, with
And the coulometric detector of base plate interior link battery, the distance apart from barrier on front side of bottom plate are less than arranges value, then ranging
Instrument communicates information to controller, and controller control buzzer alarm sends alarm, sets electricity when accumulator electric-quantity is less than, then
Controller is communicated information to, controller control buzzer alarm sends alarm, can effectively avoid that accident occurs, at the top of the bottom plate
There is provided console, console both sides are provided with pedal, and the pedal is provided with pressure sensor before and after inside, and two pin are stepped on
After up, body rocks the gravity tendency for changing pin, and controller calculates people according to the information of each pressure sensor transmission
The incline direction of body, generation flight directive are sent to flight controller, and flight controller controls each motor power (output) to realize
The heading of equipment.
Brief description of the drawings
Accompanying drawing is used for providing further understanding to of the present utility model, and a part for constitution instruction, with this practicality
New embodiment is used to explain the utility model together, does not form to limitation of the present utility model.
In the accompanying drawings：
Fig. 1 is a kind of low flyer overall structure diagram that can be manned described in the utility model embodiment；
Fig. 2 is a kind of low flyer bottom plate cross section structure schematic diagram that can be manned described in the utility model embodiment；
Fig. 3 is a kind of low flyer top view that can be manned described in the utility model embodiment；
Label in figure：1st, bottom plate；2nd, side plate；3rd, backplate；4th, console；5th, solar panel；6th, propeller；7th, buzzing
Siren；8th, rangefinder；9th, coulometric detector；10th, charge port；11st, pressure sensor；12nd, battery；13rd, controller；14、
Flight controller；15th, charging chip；16th, controller for solar；17th, motor；18th, pedal；19th, start key；20th, stop key.
Embodiment
Preferred embodiment of the present utility model is illustrated below in conjunction with accompanying drawing, it will be appreciated that described herein excellent
Select embodiment to be merely to illustrate and explain the utility model, be not used to limit the utility model.
Embodiment：Refer to Fig. 1-3, a kind of low flyer that can be manned of the utility model, including bottom plate 1, side plate 2,
Backplate 3 and console 4, side plate 2 are arranged at the both sides of bottom plate 1, and the front side of side plate 2 and rear side are equipped with propeller 6, set in propeller 6
There is motor 17, the middle part of side plate 2 is provided with solar panel 5, and backplate 3 is arranged at the top both sides of bottom plate 1, and console 4 is arranged at
In the middle part of the top surface of bottom plate 1, the both sides of console 4 are equipped with pedal 18, are sequentially provided with two pressure sensings inside pedal 18 from front to back
Device 11, the front side of bottom plate 1 are sequentially provided with charge port 10, rangefinder 8 and buzzer alarm 7 from left to right, and the inside of bottom plate 1 is provided with electric power storage
Pond 12, the side of battery 12 are provided with controller for solar 16, and the opposite side of battery 12 is provided with charging chip 15, the top of battery 12
Controller 13, flight controller 14 and coulometric detector 9 are sequentially provided with from left to right.
Further, the four groups of pressure sensors 11 set on the pedal 18 of the both sides of console 4 are by circuit and controller
13 are electrically connected with, and the top of two side plates 2 that the top of bottom plate 1 is set is respectively equipped with stop key 20 and start key 19, the He of stop key 20
Start key 19 is electrically connected with by circuit and controller 13, and the control of the aircraft directly by pedal 18, stop key 20 and is opened
Dynamic key 19 controls, wherein, the pressure sensor set in pedal 18 can detect the pressure of human body sole in real time, and pressure value is passed
Controller 13 is sent to, controller 13 can go out incline direction and the inclination of human body according to the mathematic interpolation between each pressure sensor 11
Dynamics, send flight directive, the flight side of the inclination control aircraft of realization human body to flight controller 14 based on this
To.
Further, solar panel 5 is electrically connected with by circuit and controller for solar 16, and controller for solar 16 is logical
Oversampling circuit is electrically connected with battery 12, and charge port 10 is electrically connected with by circuit and charging chip 15, and charging chip 15 passes through
Circuit is electrically connected with battery 12, and charging chip 15 is electrically connected with controller 13 and flight controller 14 respectively by circuit
Connect, battery 12 is electrically connected with by circuit and coulometric detector 9, and coulometric detector 9 is electrically connected by circuit and controller 13
Connect, solar panel 5 continual can charge for battery 12, the endurance of extension device, the electricity in battery 12
When measuring insufficient, detection information can be sent to controller 13 by coulometric detector 9, control buzzer alarm 7 to send out by controller 13
Go out alarm.
Further, rangefinder 8 is electrically connected with by circuit and controller 13, and buzzer alarm 7 passes through circuit and controller
13 are electrically connected with, and when aircraft front side is apart from barrier certain distance, rangefinder 8 can send information, control to controller 13
Device 13 processed controls buzzer alarm 7 to send alarm at once, wherein, rangefinder 8 can be infrared ambulator or sound-ranging equipment.
Further, the motor 17 set in propeller 6 is electrically connected with by circuit and flight controller 14, flight control
Device 14 is electrically connected with by circuit and controller 13, wherein, four common rotor flying controllers can be selected in flight controller 14,
Controller 13 is CPU, built-in operation program, can calculate the difference between each pressure sensor 11, and calculate people with this
The angle of inclination of body.
During use：By setting rangefinder and buzzer alarm, and base plate interior to link battery on front side of bottom plate
Coulometric detector, the distance apart from barrier on front side of bottom plate are less than arranges value, then rangefinder communicates information to controller, control
Device control buzzer alarm processed sends alarm, sets electricity when accumulator electric-quantity is less than, then communicates information to controller, control
Device control buzzer alarm sends alarm, can effectively avoid that accident occurs, console, console both sides are provided with the top of the bottom plate
Pedal is provided with, the pedal is provided with pressure sensor before and after inside, and after two pin step on, body rocks change pin
Gravity tendency, controller calculates the incline direction of human body according to the information of each pressure sensor transmission, and generation flight refers to
Order is sent to flight controller, and flight controller controls each motor power (output) to realize the heading of equipment, passes through setting
Start key and stop key, the start and stop of controllable device, the manned vehicle, control is easy, suitably promotes the use of.
Finally it should be noted that：Preferred embodiment of the present utility model is the foregoing is only, is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it can still modify to the technical scheme described in foregoing embodiments, or to which part technical characteristic
Carry out equivalent substitution.All any modification, equivalent substitution and improvements within the spirit and principles of the utility model, made etc.,
It should be included within the scope of protection of the utility model.
Claims (5)
1. a kind of low flyer that can be manned, including bottom plate (1), side plate (2), backplate (3) and console (4), its feature exist
In：The side plate (2) is arranged at bottom plate (1) both sides, and side plate (2) front side and rear side are equipped with propeller (6), the spiral
Motor (17) is provided with oar (6), is provided with solar panel (5) in the middle part of the side plate (2), the backplate (3) is arranged at bottom
Both sides at the top of plate (1), the console (4) are arranged in the middle part of bottom plate (1) top surface, and console (4) both sides are equipped with pedal
(18) two pressure sensors (11), are sequentially provided with inside the pedal (18) from front to back, bottom plate (1) front side is past from a left side
The right side is sequentially provided with charge port (10), rangefinder (8) and buzzer alarm (7), and battery (12) is provided with inside the bottom plate (1),
Battery (12) side is provided with controller for solar (16), and battery (12) opposite side is provided with charging chip (15),
Controller (13), flight controller (14) and coulometric detector (9) are sequentially provided with from left to right at the top of the battery (12).
A kind of 2. low flyer that can be manned according to claim 1, it is characterised in that：Console (4) both sides
Pedal (18) on four groups of pressure sensors (11) setting be electrically connected with by circuit and controller (13), the bottom plate
(1) stop key (20) and start key (19) are respectively equipped with the top of two side plates (2) that top is set, the stop key (20) and opened
Dynamic key (19) is electrically connected with by circuit and controller (13).
A kind of 3. low flyer that can be manned according to claim 1, it is characterised in that：The solar panel
(5) it is electrically connected with by circuit and controller for solar (16), the controller for solar (16) passes through circuit and battery
(12) it is electrically connected with, the charge port (10) is electrically connected with by circuit and charging chip (15), and the charging chip (15) is logical
Oversampling circuit is electrically connected with battery (12), and the charging chip (15) is controlled with controller (13) and flight respectively by circuit
Device (14) is electrically connected with, and the battery (12) is electrically connected with by circuit and coulometric detector (9), the coulometric detector
(9) it is electrically connected with by circuit and controller (13).
A kind of 4. low flyer that can be manned according to claim 1, it is characterised in that：The rangefinder (8) passes through
Circuit is electrically connected with controller (13), and the buzzer alarm (7) is electrically connected with by circuit and controller (13).
A kind of 5. low flyer that can be manned according to claim 1, it is characterised in that：Set in the propeller (6)
The motor (17) put is electrically connected with by circuit and flight controller (14), and the flight controller (14) passes through circuit and control
Device (13) processed is electrically connected with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721178325.4U CN207157539U (en) | 2017-09-14 | 2017-09-14 | A kind of low flyer that can be manned |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721178325.4U CN207157539U (en) | 2017-09-14 | 2017-09-14 | A kind of low flyer that can be manned |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207157539U true CN207157539U (en) | 2018-03-30 |
Family
ID=61721896
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721178325.4U Expired - Fee Related CN207157539U (en) | 2017-09-14 | 2017-09-14 | A kind of low flyer that can be manned |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207157539U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115123495A (en) * | 2022-08-30 | 2022-09-30 | 南京开天眼无人机科技有限公司 | Flight life buoy carrying battery monitoring module |
-
2017
- 2017-09-14 CN CN201721178325.4U patent/CN207157539U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115123495A (en) * | 2022-08-30 | 2022-09-30 | 南京开天眼无人机科技有限公司 | Flight life buoy carrying battery monitoring module |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180330 Termination date: 20190914 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |