CN209051588U - A kind of novel unmanned plane - Google Patents
A kind of novel unmanned plane Download PDFInfo
- Publication number
- CN209051588U CN209051588U CN201821643054.XU CN201821643054U CN209051588U CN 209051588 U CN209051588 U CN 209051588U CN 201821643054 U CN201821643054 U CN 201821643054U CN 209051588 U CN209051588 U CN 209051588U
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- China
- Prior art keywords
- fixed frame
- unmanned plane
- shaft
- sleeve
- steering engine
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Abstract
The utility model relates to air vehicle technique fields, and disclose a kind of novel unmanned plane, including fixed frame, support leg is fixedly installed at the top of the fixed frame, the side of the fixed frame is fixedly mounted there are three equally distributed mounting bracket, and the mounting bracket is fixedly installed with fixed plate far from one end of fixed frame, and the inner wall movable sleeve of the fixed plate is connected to installing mechanism, the inside fixing sleeve of the installing mechanism is connected to motor cabinet, and fixing sleeve is connected to propeller on the output shaft of the motor cabinet.The novel unmanned plane, pass through the mutual cooperation of steering engine and connecting shaft, connecting rod, pull rod, it realizes through rotation connection axis and adjusts the angles and positions of connecting rod, to pull pull rod to be moved forward and backward, it drives installation sleeve to be rotated using pull rod, the angle of motor cabinet is adjusted to realize, convenient for controlling the heading of unmanned plane, the load for reducing steering engine improves the service life of steering engine.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of novel unmanned plane.
Background technique
Unmanned plane refers to the not manned vehicle using radio robot and the presetting apparatus provided for oneself manipulation, city
What general prevalence was more on field is four axis unmanned planes, and two axis rotate forward two axis reversions, and anti-twisted power each other can be offset,
And three axis cannot cancel out each other, so it is unbalanced anti-twisted to offset to tilt generation horizontal component by paddle by steering engine
Power, and product in the market is essentially all by steering engine direct-driving motor seat, the load of such steering engine is just very big, the steering engine longevity
Life is very short, influences safe flight.
Utility model content
In view of the deficiencies of the prior art, the utility model provides a kind of novel unmanned plane, has and reduces steering engine load, mentions
The advantages of high steering engine service life, solves the problems, such as that steering engine direct-driving motor seat causes steering engine load serious.
The utility model provides the following technical solutions: a kind of novel unmanned plane, including fixed frame, the top of the fixed frame
It is fixedly installed with support leg, there are three equally distributed mounting bracket, the installation branch for the side fixed installation of the fixed frame
Frame is fixedly installed with fixed plate far from one end of fixed frame, and the inner wall movable sleeve of the fixed plate is connected to installing mechanism, the peace
The inside fixing sleeve of mounting mechanism is connected to motor cabinet, and fixing sleeve is connected to propeller, the fixed frame on the output shaft of the motor cabinet
The bottom of inner cavity is fixedly installed with steering engine, and fixing sleeve is connected to link mechanism on the output shaft of the steering engine, the link mechanism
The connection of the lower rotation of one end and installing mechanism.
Preferably, the link mechanism includes connecting shaft, and the output shaft of the connecting shaft and steering engine is fixedly attached, the company
One end of spindle is fixedly installed with connecting column, and the bottom movable sleeve of the connecting column is connected to connecting rod, one end of the connecting rod
Movable sleeve is connected to shaft II, and the bottom of the shaft II is fixedly connected with pull rod, and the external activity of the pull rod is socketed with guiding
Block, the top of the guide pad are fixedly connected with the bottom of fixed frame.
Preferably, the installing mechanism includes installation sleeve, and the two sides of the installation sleeve are fixedly installed with shaft I,
The bottom of the installation sleeve is fixedly installed with transfer block, and the front of the installation sleeve is connected with gripping block, the folder
The tight positive two sides of block offer counter sink, and the internal activity of counter sink is socketed with screw, the gripping block and installation sleeve
It is fixed by screws.
Preferably, the transfer block inner wall is fixedly installed with round bar, and the external activity of round bar is socketed with pull rod, the drawing
Bar is rotatablely connected by round bar and connecting rod.
Preferably, the quantity of the connecting shaft is three, and the angle between three connecting shafts is 120 degree.
Be compared with the prior art, the utility model have it is following the utility model has the advantages that
1, the novel unmanned plane realizes by the mutual cooperation of steering engine and connecting shaft, connecting rod, pull rod and passes through rotation
Connecting shaft adjusts the angles and positions of connecting rod, so that pull rod be pulled to be moved forward and backward, utilizes pull rod that installation sleeve is driven to carry out
Rotation, is adjusted the angle of motor cabinet to realize, and convenient for controlling the heading of unmanned plane, reduces the negative of steering engine
Lotus improves the service life of steering engine.
2, novel unmanned plane, by the mutual cooperation of installation sleeve and shaft I, gripping block, convenient for being carried out to motor cabinet
Installation clamps, and ensure that the stability of motor cabinet, and motor cabinet can be rotated by shaft I, fixed plate, realizes pair
The angle of motor cabinet is adjusted.
Detailed description of the invention
Fig. 1 is the utility model overall structure diagram；
Fig. 2 is the utility model linkage arrangement schematic diagram；
Fig. 3 is the utility model installing mechanism structural schematic diagram.
In figure: 1, fixed frame；2, support leg；3, mounting bracket；4, fixed plate；5, installing mechanism；51, installation sleeve；52,
Shaft I；53, transfer block；54, gripping block；6, motor cabinet；7, propeller；8, steering engine；9, link mechanism；91, connecting shaft；92, even
Connect column；93, connecting rod；94, shaft II；95, pull rod；96, guide pad.
Specific embodiment
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
Every other embodiment obtained, fall within the protection scope of the utility model.
Referring to Fig. 1, a kind of novel unmanned plane, including fixed frame 1, the top of fixed frame 1 are fixedly installed with support leg 2,
The side of fixed frame 1 is fixedly mounted there are three equally distributed mounting bracket 3, and mounting bracket 3 is fixed far from one end of fixed frame 1
Fixed plate 4 is installed, the inner wall movable sleeve of fixed plate 4 is connected to installing mechanism 5, and the inside fixing sleeve of installing mechanism 5 is connected to motor
Seat 6, fixing sleeve is connected to propeller 7 on the output shaft of motor cabinet 6, and the bottom of 1 inner cavity of fixed frame is fixedly installed with steering engine 8, steering engine 8
Output shaft on fixing sleeve be connected to link mechanism 9, one end of link mechanism 9 is connect with the lower rotation of installing mechanism 5；
As shown in Fig. 2, link mechanism 9 includes connecting shaft 91, connecting shaft 91 and the output shaft of steering engine 8 are fixedly attached, and are connected
One end of axis 91 is fixedly installed with connecting column 92, and the bottom movable sleeve of connecting column 92 is connected to connecting rod 93, one end of connecting rod 93
Movable sleeve is connected to shaft II 94, and the bottom of shaft II 94 is fixedly connected with pull rod 95, and the external activity of pull rod 95 is socketed with guiding
The top of block 96, guide pad 96 is fixedly connected with the bottom of fixed frame 1, and connecting column 92 is also synchronous when being rotatablely connected axis 91 turns
Dynamic, so that connecting rod 93 be driven, 93 one end of connecting rod is rotated with connecting column 92, and the other end is rotated with shaft II 94,
Connecting rod 93 can also haul shaft II 94 and be translated at the same time, to drive pull rod 95 to advance or retreat, convenient for pulling
Installation sleeve 51 rotates, and realizes and is adjusted to the angle of motor cabinet 6；
As shown in figure 3, installing mechanism 5 includes installation sleeve 51, the two sides of installation sleeve 51 are fixedly installed with shaft I
52, the bottom of installation sleeve 51 is fixedly installed with transfer block 53, and the front of installation sleeve 51 is connected with gripping block 54, installation
The top of sleeve 51 and gripping block 54 offers semi-circular groove, and installation sleeve 51 and gripping block 54 are combined latter two semicircle
Shape slot is merged into a blind round hole, and the inside of blind round hole is placed with motor cabinet 6, then by screw by gripping block 54 with
Installation sleeve 51 is locked, and convenient for motor cabinet 6 is fixed, is also able to drive 6 turns of motor cabinet while being rotatablely installed sleeve 51
It is dynamic, convenient for adjusting the angle of motor cabinet 6, in order to which the direction to unmanned plane during flying regulates and controls, the positive two sides of gripping block 54
Counter sink is offered, and the internal activity of counter sink is socketed with screw, gripping block 54 and 51 company of being screwed of installation sleeve
It connects；
53 inner wall of transfer block is fixedly installed with round bar, and the external activity of round bar is socketed with pull rod 95, and pull rod 95 passes through circle
Bar and connecting rod 93 are rotatablely connected, and installation sleeve 51 rotates along shaft I 52 when pulling pull rod 95, while transfer block
53 also rotate with pull rod 95, convenient for adjusting the angle of installation sleeve 51；
The quantity of connecting shaft 91 is three, and the angle between three connecting shafts 91 is 120 degree, passes through 8 band of steering engine
Dynamic three connecting shafts 91 rotate synchronously, while can also adjust the angle of three motor cabinets 6 simultaneously, convenient for carrying out to unmanned plane
The control in direction.
When starting, motor cabinet 6 is placed on to the inside of installation sleeve 51, then covers gripping block 54 and lock screw, then
Start steering engine 8, steering engine 8 drives connecting shaft 91 to rotate, and connecting shaft 91 also will drive connecting column 92 and occur to turn when rotation
Dynamic, so that connecting rod 93 be driven, 93 one end of connecting rod is with the rotation of connecting column 92 at this time, and the other end is with II 94 turns of shaft
Dynamic, connecting rod 93 can also haul shaft II 94 and be translated at the same time, to drive pull rod 95 to advance or retreat, convenient for drawing
Dynamic installation sleeve 51 rotates, and realizes and is adjusted to the angle of motor cabinet 6.
It should be noted that, in this document, 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 including 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 understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of novel unmanned plane, including fixed frame (1), it is characterised in that: be fixedly installed with branch at the top of the fixed frame (1)
Support foot (2), there are three equally distributed mounting bracket (3), the mounting brackets for the side fixed installation of the fixed frame (1)
(3) one end far from fixed frame (1) is fixedly installed with fixed plate (4), and the inner wall movable sleeve of the fixed plate (4) is connected to fitting machine
The inside fixing sleeve of structure (5), the installing mechanism (5) is connected to motor cabinet (6), fixing sleeve on the output shaft of the motor cabinet (6)
It is connected to propeller (7), the bottom of fixed frame (1) inner cavity is fixedly installed with steering engine (8), on the output shaft of the steering engine (8)
Fixing sleeve is connected to link mechanism (9), and one end of the link mechanism (9) is connect with the lower rotation of installing mechanism (5).
2. a kind of novel unmanned plane according to claim 1, it is characterised in that: the link mechanism (9) includes connecting shaft
(91), the connecting shaft (91) and the output shaft of steering engine (8) are fixedly attached, and one end of the connecting shaft (91) is fixedly installed with company
It connects column (92), the bottom movable sleeve of the connecting column (92) is connected to connecting rod (93), one end movable sleeve of the connecting rod (93)
It is connected to shaft II (94), the bottom of the shaft II (94) is fixedly connected with pull rod (95), the external activity of the pull rod (95)
It is socketed with guide pad (96), the top of the guide pad (96) is fixedly connected with the bottom of fixed frame (1).
3. a kind of novel unmanned plane according to claim 1, it is characterised in that: the installing mechanism (5) includes installation set
Cylinder (51), the two sides of the installation sleeve (51) are fixedly installed with shaft I (52), and the bottom of the installation sleeve (51) is fixed
It is equipped with transfer block (53), the front of the installation sleeve (51) is connected with gripping block (54), and the gripping block (54) is just
The two sides in face offer counter sink, and the internal activity of counter sink is socketed with screw, the gripping block (54) and installation sleeve
(51) it is fixed by screws.
4. a kind of novel unmanned plane according to claim 3, it is characterised in that: transfer block (53) inner wall is fixedly mounted
There is round bar, and the external activity of round bar is socketed with pull rod (95), the pull rod (95) is connected by round bar and connecting rod (93) rotation
It connects.
5. a kind of novel unmanned plane according to claim 2, it is characterised in that: the quantity of the connecting shaft (91) is three
It is a, and the angle between three connecting shafts (91) is 120 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821643054.XU CN209051588U (en) | 2018-10-10 | 2018-10-10 | A kind of novel unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821643054.XU CN209051588U (en) | 2018-10-10 | 2018-10-10 | A kind of novel unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209051588U true CN209051588U (en) | 2019-07-02 |
Family
ID=67050217
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821643054.XU Expired - Fee Related CN209051588U (en) | 2018-10-10 | 2018-10-10 | A kind of novel unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209051588U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110861769A (en) * | 2019-12-03 | 2020-03-06 | 江西清科九扬智能装备有限公司 | Unmanned aerial vehicle prevents falling system |
-
2018
- 2018-10-10 CN CN201821643054.XU patent/CN209051588U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110861769A (en) * | 2019-12-03 | 2020-03-06 | 江西清科九扬智能装备有限公司 | Unmanned aerial vehicle prevents falling system |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190702 Termination date: 20201010 |