CN207715274U - A kind of novel unmanned vehicle engine igniter - Google Patents
A kind of novel unmanned vehicle engine igniter Download PDFInfo
- Publication number
- CN207715274U CN207715274U CN201721739943.1U CN201721739943U CN207715274U CN 207715274 U CN207715274 U CN 207715274U CN 201721739943 U CN201721739943 U CN 201721739943U CN 207715274 U CN207715274 U CN 207715274U
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- shell
- wall
- ignition
- unmanned vehicle
- vehicle engine
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Abstract
The utility model discloses a kind of novel unmanned vehicle engine igniters, including shell, the upper end of the shell is provided with input interface, the side of the input interface is provided with the accumulator mounted on shell upper end, the other side of input interface is provided with the upper fixed seat for being fixed on shell upper end simultaneously, and the lower end of shell is fixed with lower fixed seat, the lower end of shell is also symmetrical arranged there are two output interface in the both sides of lower fixed seat simultaneously, the outer wall of the shell is equipped with revolution counter, while the inside of shell is equipped with ignition switch by the inner wall of upper end.Shell, accumulator, revolution counter, ignition switch, ignition coil, distributor, crankshaft position sensor, ignition controller, processor and spark plug is arranged in the utility model, solves the problems, such as unmanned vehicle engine igniter and revolution counter separation down to inconvenient for use, risk factor is high and flight difficulty is big.
Description
Technical field
The utility model is related to engine apparatus technical field, specially a kind of novel unmanned vehicle engine igniter.
Background technology
Currently, with the progress of scientific and technological level, unmanned plane is applied in more and more fields, now nobody
Machine is mainly used in agricultural and scientific research field, will also play increasingly important role in people's lives.Wherein nobody
Machine engine is the capital equipment of unmanned plane, and the quality of engine quality directly affects the using effect of unmanned plane, present
Unmanned vehicle engine can deal with basic use demand, but also be faced with certain technological deficiency and deficiency simultaneously：
1. in the prior art engine ignition and revolution counter be separation, with when to look for a connector to be connected
It connects, uses very inconvenient；
2. igniter and revolution counter are perishable when in use, there are certain hidden danger when engine overall startup, nothing is increased
Man-machine risk factor；
3. engine is easy to stop working when in use, operation has some setbacks, jitter, and the flight for increasing unmanned plane is difficult
Degree.
Utility model content
(1) the technical issues of solving
The purpose of this utility model is to provide a kind of novel unmanned vehicle engine igniters, solve unmanned plane and start
Machine igniter and revolution counter detach the problem so that inconvenient for use, risk factor is high and flight difficulty is big.
(2) technical solution
To achieve the above object, the utility model provides the following technical solutions：A kind of novel unmanned vehicle engine igniting dress
It sets, including shell, the upper end of the shell is provided with input interface, and the side of the input interface is provided on shell
The accumulator at end, while the other side of input interface is provided with the upper fixed seat for being fixed on shell upper end, and the lower end of shell
It is fixed with lower fixed seat, while the lower end of shell is also symmetrical arranged that there are two output interface, the shells in the both sides of lower fixed seat
The outer wall of body is equipped with revolution counter, while the inside of shell is equipped with ignition switch, the ignition switch by the inner wall of upper end
The output end of lower section is connected with the ignition coil mounted on inner walls, and the output end below the ignition coil is connected with installation
It is connected with the spark plug mounted on inner walls, and point in the output end of the distributor of inner walls, the distributor side
The output end of the firewire circle other side is connected with the ignition controller for being fixed on inner walls, while the inner wall of shell and the igniting
The corresponding position of coil is provided with crankshaft position sensor.
Preferably, the ventilation hole positioned at revolution counter side is provided on the outer wall of the shell.
Preferably, it is connected by electric wire between the accumulator and ignition switch, and be provided with can supply lines for enclosure interior
The through-hole passed through.
Preferably, the mounting base that the ignition coil is arranged by one end respectively with the distributor is fixed in shell
On wall.
Preferably, the output end below the crankshaft position sensor is connected with the processor mounted on inner walls, and
The output end of processor is connected with the input terminal of ignition controller.
Preferably, the output end of the ignition controller is connected with the input terminal of the revolution counter.
(3) advantageous effect
The utility model provides a kind of novel unmanned vehicle engine igniter, has following advantageous effect：
1, the utility model is connected to shell by the way that shell, ignition coil, ignition controller and revolution counter, revolution counter is arranged
The outer surface of body, while revolution counter is connected with the ignition controller of enclosure interior, when equipment is started to work, ignition coil passes through
The effect of ignition controller makes revolution counter operate, so that revolution counter is arranged in the outer surface of igniter, integral type group
Dress so that equipment is more convenient to use.
2, the utility model passes through a fire control by the way that shell, revolution counter, ignition controller and processor, processor is arranged
The effect of device processed makes revolution counter work so that equipment reasonable design, and revolution counter is arranged on the outer wall of shell, avoids and turns
The separation of fast table and igniter so that the safety coefficient of equipment improves, and when use is hardly damaged.
3, for the utility model by the way that revolution counter and shell is arranged, shell and revolution counter are integral type assembling design, are avoided
It is easy when unmanned plane during flying flame-out so that the operation of unmanned plane is more smooth, and signal is more stablized, and reduces flying for unmanned plane
Row difficulty.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the structural schematic diagram of the utility model enclosure interior；
Fig. 3 is the flow chart of the utility model.
In figure：Under 1 shell, 2 accumulators, 3 input interfaces, 4 upper fixed seats, 5 revolution counters, 6 ventilation holes, 7 output interfaces, 8
Fixed seat, 9 ignition switches, 10 ignition coils, 11 distributors, 12 crankshaft position sensors, 13 ignition controllers, 14 processors,
15 spark plugs.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
As shown in Figs. 1-3, a kind of embodiment provided by the utility model：A kind of novel unmanned vehicle engine igniter,
Including shell 1, the upper end of shell 1 is provided with input interface 3, and the side of input interface 3 is provided with the storage mounted on 1 upper end of shell
Battery 2, while the other side of input interface 3 is provided with the upper fixed seat 4 for being fixed on 1 upper end of shell, and the lower end of shell 1 is same
When be fixed with lower fixed seat 8, the lower end of shell 1 is also symmetrical arranged that there are two output interface 7, shells 1 in the both sides of lower fixed seat 8
Outer wall revolution counter 5 is installed, the ventilation hole 6 positioned at 5 side of revolution counter is provided on the outer wall of shell 1, while shell 1 is interior
Portion is equipped with ignition switch 9 by the inner wall of upper end, is connected by electric wire between accumulator 2 and ignition switch 9, and in shell 1
Portion be provided with can the through-hole that passes through of supply lines, the output end of 9 lower section of ignition switch is connected with the ignition lead mounted on 1 inner wall of shell
The output end of circle 10,10 lower section of ignition coil is connected with the distributor 11 mounted on 1 inner wall of shell, ignition coil 10 and distributor
11 mounting bases being arranged respectively by one end are fixed on the inner wall of shell 1, and the output end of 11 side of distributor is connected with installation
It is connected with the igniting for being fixed on 1 inner wall of shell in the output end of the spark plug 15 of 1 inner wall of shell, and 10 other side of ignition coil
Controller 13, the output end of ignition controller 13 are connected with the input terminal of the revolution counter 5, at the same the inner wall of shell 1 with it is described
10 corresponding position of ignition coil is provided with crankshaft position sensor 12, and crankshaft position sensor 12 can record song when in use
Shaft position information, and the output end of 12 lower section of crankshaft position sensor is connected with the processor 14 mounted on 1 inner wall of shell, and
The output end of processor 14 is connected with the input terminal of ignition controller 13.
When in use, accumulator 2 controls the working condition of ignition coil 10 by ignition switch 9, and ignition coil 10 exists
Under the action of distributor 11 spark plug 15 can work normally, complete the ignition operation of equipment, and ignition coil 10 simultaneously can
To influence the working condition of ignition controller 13, while the also processor 14 of ignition controller 13 is influenced, works as ignition controller
13 can make 5 normal operation of revolution counter when running well so that and the rationalization in igniter surface particles 1 is arranged in revolution counter 5,
Crankshaft position information can be passed to processor 14 by crankshaft position sensor 12 simultaneously so that and the accuracy of device improves, this
Utility model makes revolution counter 5 and ignition housings 1 be designed for integral type, reduces intermediate connector part, uses new energy
It is improved.
It can to sum up obtain, the utility model is by being arranged shell 1, accumulator 2, revolution counter 5, ignition switch 9, ignition coil
10, distributor 11, crankshaft position sensor 12, ignition controller 13, processor 14 and spark plug 15, solve unmanned plane hair
Motivation igniter and revolution counter detach the problem so that inconvenient for use, risk factor is high and flight difficulty is big.
It should be noted that herein, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also include other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of novel unmanned vehicle engine igniter, including shell (1), it is characterised in that：The upper end of the shell (1) is set
It is equipped with input interface (3), the side of the input interface (3) is provided with the accumulator (2) mounted on shell (1) upper end, simultaneously
The other side of input interface (3) is provided with the upper fixed seat (4) for being fixed on shell (1) upper end, and the lower end of shell (1) is fixed
There is a lower fixed seat (8), while the lower end of shell (1) is also symmetrical arranged that there are two output interfaces in the both sides of lower fixed seat (8)
(7), the outer wall of the shell (1) is equipped with revolution counter (5), while the inside of shell (1) is installed a little by the inner wall of upper end
Fire switchs (9), and the output end below the ignition switch (9) is connected with the ignition coil (10) mounted on shell (1) inner wall, institute
It states the output end below ignition coil (10) and is connected with the distributor (11) mounted on shell (1) inner wall, the distributor (11)
The output end of side is connected with the spark plug (15) mounted on shell (1) inner wall, and the output of ignition coil (10) other side
End is connected with the ignition controller (13) for being fixed on shell (1) inner wall, while the inner wall of shell (1) and the ignition coil (10)
Corresponding position is provided with crankshaft position sensor (12).
2. a kind of novel unmanned vehicle engine igniter according to claim 1, it is characterised in that：The shell (1)
Outer wall on be provided with the ventilation hole (6) positioned at revolution counter (5) side.
3. a kind of novel unmanned vehicle engine igniter according to claim 1, it is characterised in that：The accumulator
(2) it is connect by electric wire between ignition switch (9), and be internally provided with can the through-hole that passes through of supply lines for shell (1).
4. a kind of novel unmanned vehicle engine igniter according to claim 1, it is characterised in that：The ignition coil
(10) mounting base being arranged respectively by one end with the distributor (11) is fixed on the inner wall of shell (1).
5. a kind of novel unmanned vehicle engine igniter according to claim 1, it is characterised in that：The crank position
Output end below sensor (12) is connected with the processor (14) mounted on shell (1) inner wall, and the output of processor (14)
End is connected with the input terminal of ignition controller (13).
6. a kind of novel unmanned vehicle engine igniter according to claim 1, it is characterised in that：The ignition control
The output end of device (13) is connected with the input terminal of the revolution counter (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721739943.1U CN207715274U (en) | 2017-12-14 | 2017-12-14 | A kind of novel unmanned vehicle engine igniter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721739943.1U CN207715274U (en) | 2017-12-14 | 2017-12-14 | A kind of novel unmanned vehicle engine igniter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207715274U true CN207715274U (en) | 2018-08-10 |
Family
ID=63055598
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721739943.1U Active CN207715274U (en) | 2017-12-14 | 2017-12-14 | A kind of novel unmanned vehicle engine igniter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207715274U (en) |
-
2017
- 2017-12-14 CN CN201721739943.1U patent/CN207715274U/en active Active
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