CN207631484U - A kind of course of new aircraft - Google Patents
A kind of course of new aircraft Download PDFInfo
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- CN207631484U CN207631484U CN201721804457.3U CN201721804457U CN207631484U CN 207631484 U CN207631484 U CN 207631484U CN 201721804457 U CN201721804457 U CN 201721804457U CN 207631484 U CN207631484 U CN 207631484U
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- arm
- fixed arm
- course
- fixed
- mounting groove
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Abstract
The utility model discloses a kind of course of new aircraft, including body and remote controler, multiple grooves are symmetrically offered on the body, it is rotatably connected to the first fixed arm in each groove, the second fixed arm is inserted in first fixed arm, the described one end of second fixed arm far from the first fixed arm is fixedly connected with actuating arm, propeller module is rotatably connected on the actuating arm, mounting groove is offered on the body, and battery module is equipped in the mounting groove.The utility model is simple in structure, easy to use, can change the size of unmanned plane according to actual needs, has a variety of state of flights, and applicability is wide, and remote controler is put into mounting groove after when not in use taking out battery module, and easy to carry and storage is worthy to be popularized.
Description
Technical field
The utility model is related to vehicle technology field more particularly to a kind of course of new aircraft.
Background technology
Aircraft is by mankind's manufacture, can fly away from ground, controls in endoatmosphere or big in space flight and by people
The instrument flying object of the gas-bearing formation external space (space) flight, aircraft are divided into aircraft, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also one kind of aircraft, and unmanned plane is manipulated not using radio robot and the presetting apparatus provided for oneself
Manned aircraft, from technical standpoint definition can be divided into unmanned helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, nobody
Dirigible and unmanned parasol etc.；By application field can be divided into it is military with it is civilian, military aspect unmanned plane is divided into reconnaissance plane and target drone；
Currently, unmanned plane can be widely applied to national ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitoring,
Traffic patrolling, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, the monitoring of protection zone wild animal, air sampling, sea
Thing scouting, border tour, prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water money
It is source exploitation, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, gloomy
Woods pest and disease damage protects and the fields such as monitoring, digital city.Aircraft is with compact-sized, build is less than normal, popular relatively strong, movement
Flexibly and the advantages that flight stability by extensively in civil and military, and quite it is popular；However existing unmanned plane is big
Small fixation cannot change the size of unmanned plane as needed to use, while remote controler and unmanned plane are separately carried and stored, pole
It is easy to be lost.
Utility model content
Purpose of the utility model is to solve unmanned plane sizes in the prior art to fix, and cannot change nothing as needed
Man-machine size uses, while remote controler and unmanned plane separately carry and store, the problem of easily loss, and the one kind proposed
Course of new aircraft.
To achieve the goals above, the utility model uses following technical solution：
A kind of course of new aircraft, including body and remote controler symmetrically offer multiple grooves on the body, each described
It is rotatably connected to the first fixed arm in groove, the second fixed arm, second fixed arm are inserted in first fixed arm
One end far from the first fixed arm is fixedly connected with actuating arm, and propeller module, the machine are rotatably connected on the actuating arm
Mounting groove is offered on body, and battery module is equipped in the mounting groove.
Preferably, the first mounting hole and the second mounting hole are offered on each first fixed arm, each described the
It opens up fluted on two fixed arms, is fixedly connected with fixed block by multiple springs in the groove, and fixed block is located at the
In one mounting hole.
Preferably, each propeller module is made of two moving blocks and two propellers, each driving
Rotation connection is there are two moving block on arm, and symmetrically there are two propellers for rotation connection on two moving blocks.
Preferably, each actuating arm is electrically connected between battery module by conducting wire.
Preferably, battery protection shell is equipped at the notch of the mounting groove.
Preferably, the size of the remote controler is adapted to the size of mounting groove.
In the utility model, fixed block is pressed down on, the spring-compressed being attached thereto pushes up drive to close to body side
Swing arm, the upper arm of fixed block and the inner wall of the first fixed arm offset, and when being pushed to the first mounting hole, spring restores former long, band
Dynamic fixed block moves upwards, and is fastened in the first mounting hole, then passes through remote control control aircraft；It presses down on and fixes
Block, the spring-compressed being attached thereto pull up actuating arm to far from body side, and the upper arm of fixed block is interior with the first fixed arm
Wall offsets, and when being pushed to the second mounting hole, spring restores former long, drives fixed block to move upwards, is fastened on the second mounting hole
It is interior, then pass through remote control control aircraft；When carrying, downward push fixed block, the spring-compressed being attached thereto, to
Actuating arm is pulled up far from body side, the upper arm of fixed block and the inner wall of the first fixed arm offset, when being pushed to the second fixation
Kong Shi, spring restore former long, drive fixed block to move upwards, be fastened in the second mounting hole, then rotate the first fixed arm, make
The rotation close to each other of corresponding two the first fixed arms in position, then rotates moving block so that propeller and the first fixed arm
It is parallel, then corresponding four propellers in turned position, the state for keeping it parallel each other while vertical with the first fixed arm,
Then battery protection shell and battery module are dismantled, remote controler is placed in mounting groove；Remote controler, battery module and driving
The relevant concrete structure of arm and the technology that Principle of Communication is existing maturation, not described here any more.The utility model is simple in structure, makes
With convenient, the size of unmanned plane can be changed according to actual needs, there are a variety of state of flights, applicability is wide, without using
When battery module is taken out after remote controler is put into mounting groove, it is easy to carry and storage, be worthy to be popularized.
Description of the drawings
Fig. 1 be the utility model proposes a kind of course of new aircraft structural schematic diagram；
Fig. 2 be the utility model proposes a kind of course of new aircraft fixed block be located at the second mounting hole status architecture illustrate
Figure；
Fig. 3 be the utility model proposes a kind of course of new aircraft folded state structural schematic diagram.
In figure：1 body, 2 battery modules, 3 first fixed arms, 4 propellers, 5 actuating arms, 6 second fixed arms, 7 remote controlers,
8 first mounting holes, 9 second mounting holes, 10 fixed blocks, 11 moving blocks.
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.
In the description of the present invention, it should be understood that term "upper", "lower", "front", "rear", "left", "right",
The orientation or positional relationship of the instructions such as "top", "bottom", "inner", "outside" is to be based on the orientation or positional relationship shown in the drawings, and is only
The utility model and simplifying describes for ease of description, do not indicate or imply the indicated device or element must have it is specific
Orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.
Referring to Fig.1-3, a kind of course of new aircraft, including body 1 and remote controler 7 symmetrically offer on body 1 multiple recessed
Slot is rotatably connected to the first fixed arm 3 in each groove, is inserted with the second fixed arm 6 in the first fixed arm 3, and each first
The first mounting hole 8 and the second mounting hole 9 are offered on fixed arm 3, and fluted, groove is opened up on each second fixed arm 6
It is interior to be fixedly connected with fixed block 10 by multiple springs, and fixed block 10 is located in the first mounting hole 8, the second fixed arm 6 is separate
One end of first fixed arm 3 is fixedly connected with actuating arm 5, and propeller module, each propeller mould are rotatably connected on actuating arm 5
Block is made of two moving blocks 11 and two propellers 4, moving block 11 there are two rotation connections on each actuating arm 5, two
Symmetrically rotation connection offers mounting groove, battery module is equipped in mounting groove there are two propeller 4 on body 1 on moving block 11
2, battery protection shell is equipped at the notch of mounting groove, each actuating arm 5 is electrically connected between battery module 2 by conducting wire, distant
The size of control device 7 is adapted to the size of mounting groove.
When the utility model is used, fixed block 10 is pressed down on, the spring-compressed being attached thereto, to close to 1 side of body
Actuating arm 5 is pushed up, the upper arm of fixed block 10 and the inner wall of the first fixed arm 3 offset, when being pushed to the first mounting hole 8,
Spring restores former long, drives fixed block 10 to move upwards, is fastened in the first mounting hole 8, is then controlled and is flown by remote controler 7
Device；Fixed block 10 is pressed down on, the spring-compressed being attached thereto pulls up actuating arm 5 to far from 1 side of body, fixed
The upper arm of block 10 and the inner wall of the first fixed arm 3 offset, and when being pushed to the second mounting hole 9, spring restores former long, drives and fixes
Block 10 moves upwards, and is fastened in the second mounting hole 9, then controls aircraft by remote controler 7；When carrying, downwards
Press fixed block 10, the spring-compressed being attached thereto pulls up actuating arm 5 to far from 1 side of body, the upper arm of fixed block 10 with
The inner wall of first fixed arm 3 offsets, and when being pushed to the second mounting hole 9, spring restores former long, and fixed block 10 is driven to transport upwards
It is dynamic, it is fastened in the second mounting hole 9, then rotates the first fixed arm 3, make corresponding two the first fixed arms 3 in position mutually
Close to rotation, moving block 11 is then rotated so that propeller 4 is parallel with the first fixed arm 3, then turned position corresponding four
A propeller 4, the state for keeping it parallel each other while vertical with the first fixed arm 3, then dismantles battery protection shell and battery
Remote controler 7 is placed in mounting groove by module 2；Remote controler 7, battery module 2 and 5 relevant concrete structure of actuating arm and
Principle of Communication is the technology of existing maturation, not described here any more.
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.
The preferable specific implementation mode of the above, only the utility model, but the scope of protection of the utility model is not
Be confined to this, any one skilled in the art within the technical scope disclosed by the utility model, according to this practicality
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. a kind of course of new aircraft, including body (1) and remote controler (7), which is characterized in that symmetrically opened up on the body (1)
There are multiple grooves, the first fixed arm (3) is rotatably connected in each groove, is inserted in first fixed arm (3)
Second fixed arm (6), the one end of second fixed arm (6) far from the first fixed arm (3) are fixedly connected with actuating arm (5), institute
It states and is rotatably connected to propeller module on actuating arm (5), offer mounting groove on the body (1), be equipped in the mounting groove
Battery module (2).
2. a kind of course of new aircraft according to claim 1, which is characterized in that on each first fixed arm (3)
Offer the first mounting hole (8) and the second mounting hole (9), opened up on each second fixed arm (6) it is fluted, it is described recessed
It is fixedly connected with fixed block (10) by multiple springs in slot, and fixed block (10) is located in the first mounting hole (8).
3. a kind of course of new aircraft according to claim 1, which is characterized in that each propeller module is by two
Moving block (11) and two propellers (4) form, moving block (11) there are two rotation connections on each actuating arm (5), and two
Symmetrically there are two propellers (4) for rotation connection on a moving block (11).
4. a kind of course of new aircraft according to claim 1, which is characterized in that each actuating arm (5) is and battery
Module is electrically connected between (2) by conducting wire.
5. a kind of course of new aircraft according to claim 1, which is characterized in that be equipped with battery at the notch of the mounting groove
Protective shell.
6. a kind of course of new aircraft according to claim 1, which is characterized in that the size of the remote controler (7) with
The size of mounting groove is adapted to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721804457.3U CN207631484U (en) | 2017-12-21 | 2017-12-21 | A kind of course of new aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721804457.3U CN207631484U (en) | 2017-12-21 | 2017-12-21 | A kind of course of new aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207631484U true CN207631484U (en) | 2018-07-20 |
Family
ID=62853703
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721804457.3U Active CN207631484U (en) | 2017-12-21 | 2017-12-21 | A kind of course of new aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207631484U (en) |
-
2017
- 2017-12-21 CN CN201721804457.3U patent/CN207631484U/en active Active
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