CN207346076U - A kind of constant fixed-wing of center of gravity verts system - Google Patents
A kind of constant fixed-wing of center of gravity verts system Download PDFInfo
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- CN207346076U CN207346076U CN201721348025.6U CN201721348025U CN207346076U CN 207346076 U CN207346076 U CN 207346076U CN 201721348025 U CN201721348025 U CN 201721348025U CN 207346076 U CN207346076 U CN 207346076U
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- empennage
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- 230000005484 gravity Effects 0.000 title claims abstract description 15
- 238000003466 welding Methods 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims 1
- 230000005611 electricity Effects 0.000 description 5
- 230000005540 biological transmission Effects 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
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Abstract
Vert system the utility model discloses a kind of constant fixed-wing of center of gravity, its structure includes the first wing, first empennage, main body, second empennage, fixing bolt, second wing, hypsokinesis switch block, propeller, micromachine, lean forward switch block, fixed block, preceding contact wheel, movable pulley afterwards, connecting wire, the micromachine is equipped with machine shaft, fixing terminal, motor body, binding post, rear end cap, the fixing terminal is vertically welded in the center on motor body surface and uses and is welded to connect, the machine shaft is connected through fixing terminal in motor body internal mechanical, the utility model by equipped with micromachine, the weight of aircraft can be mitigated, due to reducing weight, power consumption is less, improve the cruising ability of aircraft, aircraft is set to work the longer time, improve the efficiency of work.
Description
Technical field
The utility model is that a kind of constant fixed-wing of center of gravity verts system, belongs to fixed-wing and verts system regions.
Background technology
Fixed wing aircraft is referred to as aircraft, refers to produce the thrust advanced or pulling force by power set, by the fixation of fuselage
Wing produces lift, in the aircraft for overweighting air of endoatmosphere flight.
Prior art discloses Application No.：201520681912.X a kind of VTOL Fixed Wing AirVehicle, including
Fuselage, empennage and the power set with inclining rotary mechanism, it is spiral that the power set with inclining rotary mechanism include fixedpiston
Paddle, engine, enging cabin, slip-stream rudder, wing, tilting wing and steering engine, engine are installed in enging cabin, fixedpiston
The output axis connection of propeller and engine, tilting wing one end are fixedly connected on enging cabin, and the other end rotatably connects
It is connected on wing, slip-stream rudder is movably connected on tilting wing, slip-stream rudder described in servo driving, described dynamic with inclining rotary mechanism
Power apparatus is symmetrically disposed on fuselage both sides, and is horizontally disposed with for wing, and the fuselage head is equipped with through hole, and exhausting wind is set in through hole
Fan, prior art people are energized using engine, and engine weight is overweight, and electricity consumption speed is fast, reduces the cruising time of aircraft, work
It is low to make efficiency.
Utility model content
Vert in view of the deficienciess of the prior art, the utility model aim is to provide a kind of constant fixed-wing of center of gravity and be
System, is energized, engine weight is overweight, and electricity consumption speed is fast, reduces the continuation of the journey of aircraft with solving prior art people using engine
The problem of time, work efficiency is low.
To achieve these goals, the utility model is to realize by the following technical solutions：A kind of center of gravity is constant
Fixed-wing verts system, its structure include the first wing, the first empennage, main body, the second empennage, fixing bolt, the second wing,
Hypsokinesis switch block, propeller, micromachine, the switch block that leans forward, fixed block, preceding contact wheel, rear movable pulley, connecting wire, described first
Wing vertical is welded on the right end at main body rear, and second wing vertical is welded on the left end at main body rear, and described
One empennage is vertically fixed on the top of the first wing and the second wing and uses and is welded to connect with the second empennage, first tail
The wing is in same level and parallel to each other with the second empennage, and the fixing bolt is equipped with and two and is threadably secured
In the lower section of the first wing and the second wing, the hypsokinesis switch block is equipped with two and is fixed on the first wing and the by bearing
The lower section in two wing stage casings, the switch block that leans forward are fixed on left and right ends in front of main body, the micro electric by supporting block
Machine is equipped with two and is vertically fixed on hypsokinesis switch block and the top of switch block of leaning forward, and the micromachine passes through hypsokinesis switch block, preceding
The circuit board electrical connection verted inside block and main body, the propeller is fixed on the top of micromachine by bearing, described
Fixed block is fixed on the front of main body lower surface by rivet, and the preceding contact wheel is connected by rotation axis and the activity of preceding contact wheel
Connect, the rear movable pulley is installed on the rear of preceding contact wheel and using mechanically connecting, and the main body passes through conducting wire and hypsokinesis
Circuit board electrical connection inside switch block, the micromachine are equipped with machine shaft, fixing terminal, motor body, binding post, rear end
Lid, the fixing terminal are vertically welded in the center on motor body surface and using being welded to connect, and the machine shaft runs through
Fixing terminal is connected in motor body internal mechanical, the motor body embedded in hypsokinesis switch block in switch block surface of leaning forward, after described
End cap is welded on the bottom of motor body, and the binding post is vertically fixed on the outer surface of rear end cap and with hypsokinesis switch block in preceding
The circuit board electrical connection verted inside block.
Further, the propeller is equipped with two or more and is yi word pattern structure.
Further, the hypsokinesis switch block and the switch block that leans forward are parallel to each other.
Further, the preceding contact wheel, rear movable pulley are in same level.
Further, first wing is mutually symmetrical with by main body and the second wing.
Further, the micromachine is brshless DC motor, transmission efficiency higher.
Further, the propeller is stainless steel material, and long-time service will not be by corrosion.
Beneficial effect
A kind of constant fixed-wing of center of gravity of the utility model verts system, by equipped with micromachine, can mitigate and fly
The weight of machine, due to reducing weight, power consumption is less, improves the cruising ability of aircraft, when the aircraft is worked longer
Between, improve the efficiency of work.
Brief description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon：
Fig. 1 is that a kind of constant fixed-wing of center of gravity of the utility model verts the structure diagram of system.
Fig. 2 is the structure diagram of the utility model micromachine.
In figure：First wing -1, the first empennage -2, main body -3, the second empennage -4, fixing bolt -5, the second wing -6,
Hypsokinesis switch block -7, propeller -8, micromachine -9, the switch block -10 that leans forward, fixed block -11, preceding contact wheel -12, rear movable pulley -13,
Connecting wire -14, machine shaft -901, fixing terminal -902, motor body -903, binding post -904, rear end cap -905.
Embodiment
To make the technical means, creative features, achievable purpose and effectiveness that the utility model is realized easy to understand, below
With reference to embodiment, the utility model is expanded on further.
Please refer to Fig.1, Fig. 2, the utility model provides a kind of constant fixed-wing of center of gravity and verts system：Its structure includes the
It is one wing 1, the first empennage 2, main body 3, the second empennage 4, fixing bolt 5, the second wing 6, hypsokinesis switch block 7, propeller 8, micro-
Type motor 9, the switch block 10 that leans forward, fixed block 11, preceding contact wheel 12, rear movable pulley 13, connecting wire 14, first wing 1 hang down
The straight right end for being welded on 3 rear of main body, second wing 6 are vertically welded in the left end at 3 rear of main body, first tail
The wing 2 is vertically fixed on the top of the first wing 1 and the second wing 6 and uses and is welded to connect with the second empennage 4, first tail
The wing 2 is in same level and parallel to each other with the second empennage 4, and the fixing bolt 5 is equipped with two and passes through screw thread
The lower section of the first wing 1 and the second wing 6 is fixed on, the hypsokinesis switch block 7 is equipped with two and is fixed on first by bearing
The lower section in 1 and second wing of wing, 6 stage casing, the switch block 10 that leans forward are fixed on the left and right two in the front of main body 3 by supporting block
End, the micromachine 9 are equipped with two and are vertically fixed on the top of hypsokinesis switch block 7 and the switch block 10 that leans forward, the micro electric
Machine 9 is consolidated by hypsokinesis switch block 7, the switch block 10 that leans forward with the circuit board electrical connection inside main body 3, the propeller 8 by bearing
The top of micromachine 9 is scheduled on, the fixed block 11 is fixed on the front of 3 lower surface of main body by rivet, is contacted before described
Wheel 12 is flexibly connected by rotation axis with preceding contact wheel 12, and the rear movable pulley 13 is installed on the rear of preceding contact wheel 12 and adopts
With mechanical connection, the main body 3 is equipped with by the circuit board electrical connection inside conducting wire and hypsokinesis switch block 7, the micromachine 9
Machine shaft 901, fixing terminal 902, motor body 903, binding post 904, rear end cap 905,902 vertical welding of fixing terminal
It is connected on the center on 903 surface of motor body and using being welded to connect, the machine shaft 901 is through fixing terminal 902 in electricity
903 internal mechanical of owner's body connects, and the motor body 903 is embedded in hypsokinesis switch block 7 in 10 surface of switch block of leaning forward, the rear end cap
905 are welded on the bottom of motor body 903, and the binding post 904 is vertically fixed on the outer surface of rear end cap 905 and and hypsokinesis
Circuit board electrical connection of the switch block 7 inside the switch block 10 that leans forward, the propeller 8 are equipped with two or more and are yi word pattern structure,
The hypsokinesis switch block 7 and the switch block 10 that leans forward are parallel to each other, and the preceding contact wheel 12, rear movable pulley 13 are in same level,
First wing 1 is mutually symmetrical with by main body 3 and the second wing 6, and the micromachine 9 is brshless DC motor, transmission
More, the propeller 8 is stainless steel material to efficiency, and long-time service will not be by corrosion.
When in use, people are by with establishing wireless connection inside main body 3, passing through preceding contact wheel 12, rear movable pulley 13
Slip run in advance, preceding 12 lifting of contact wheel, main body 3, which soars, to take off, by the first wing 1, the first empennage 2, the second empennage 4,
The balance of second wing 6 makes aircraft balanced in the air, when needing conversion direction, can pass through hypsokinesis switch block 7 and the switch block 1 that leans forward
Make 6 sidesway of the first 1 second wing of wing, and since 3 heavier-weight of main body, the center of gravity of equipment will not change, the first wing 1
Second wing 6 only shifts, and does not interfere with device inclined, makes the object of main body 3 will not be jolted, when verting,
Binding post 904 receives electric signal, obtains motor body 903 electric, drives the rotation of machine shaft 901 to produce moment of torsion, drives spiral
Paddle 8 rotates, and 1 second wing 6 of the first wing is verted, makes equipment more flexible.
Fixing bolt 5 described in the utility model is by a kind of fastening dimerous of hexagon-head and ring flange and screw rod
Part, need to coordinate with nut, for being fastenedly connected two components for carrying through hole.
Its structure and principle are all that this technology personnel can be learnt by technical manual or be known by normal experiment method,
The utility model solves the problems, such as it is that prior art people are energized using engine, and engine weight is overweight, and electricity consumption speed is fast, subtracts
In the cruising time of few aircraft, work efficiency is low, and the utility model is combined with each other by above-mentioned component, can mitigate the weight of aircraft
Amount, due to reducing weight, power consumption is less, improves the cruising ability of aircraft, aircraft is worked the longer time, improves
The efficiency of work, it is described in detail below：
The fixing terminal 902 is vertically welded in the center on 903 surface of motor body and uses and is welded to connect, the electricity
Machine shaft 901 is connected through fixing terminal 902 in 903 internal mechanical of motor body, and the motor body 903 is embedded in hypsokinesis switch block
7 in 10 surface of switch block of leaning forward, and the rear end cap 905 is welded on the bottom of motor body 903, and the binding post 904 is vertically fixed
In the outer surface of rear end cap 905 and circuit board electrical connection with hypsokinesis switch block 7 inside the switch block 10 that leans forward.
The advantages of basic principle and main feature and the utility model of the utility model has been shown and described above, for
For those skilled in the art, it is clear that the utility model is not limited to the details of above-mentioned one exemplary embodiment, and without departing substantially from this
In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than described above limit, it is intended that will fall in the implication and scope of the equivalency of claim
All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation
It is required that.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical solution, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (5)
- The system 1. a kind of constant fixed-wing of center of gravity verts, it is characterised in that：Its structure includes the first wing (1), the first empennage (2), main body (3), the second empennage (4), fixing bolt (5), the second wing (6), hypsokinesis switch block (7), propeller (8), miniature Motor (9), the switch block that leans forward (10), fixed block (11), preceding contact wheel (12), rear movable pulley (13), connecting wire (14), described One wing (1) is vertically welded in the right end at main body (3) rear, and second wing (6) is vertically welded in main body (3) rear Left end, it is characterised in that：First empennage (2) and the second empennage (4) are vertically fixed on the top of the first wing (1) and the second wing (6) simultaneously Using being welded to connect, first empennage (2) be in the second empennage (4) it is in same level and parallel to each other, it is described solid Bolt (5) is determined equipped with two and is threadedly secured to the lower section of the first wing (1) and the second wing (6), is verted after described Block (7) is equipped with two and the lower section of the first wing (1) and the second wing (6) stage casing is fixed on by bearing, verts before described Block (10) is fixed on the left and right ends in front of main body (3) by supporting block, and the micromachine (9) is equipped with two and vertical The top of hypsokinesis switch block (7) and switch block (10) of leaning forward is fixed on, the micromachine (9) is by hypsokinesis switch block (7), lean forward switch block (10) circuit board electrical connection internal with main body (3), the propeller (8) are fixed on the upper of micromachine (9) by bearing Side, the fixed block (11) are fixed on the front of main body (3) lower surface by rivet, and the preceding contact wheel (12) passes through rotation Axis is flexibly connected with preceding contact wheel (12), and the rear movable pulley (13) is installed on the rear of preceding contact wheel (12) and using machinery Connection, the main body (3) pass through the internal circuit board electrical connection of conducting wire and hypsokinesis switch block (7)；The micromachine (9) be equipped with machine shaft (901), fixing terminal (902), motor body (903), binding post (904), Rear end cap (905), the fixing terminal (902) are vertically welded in the center on motor body (903) surface and are connected using welding Connect, the machine shaft (901) connects through fixing terminal (902) in motor body (903) internal mechanical, the motor body (903) embedded in hypsokinesis switch block (7) bottom of motor body (903) is welded in the switch block that leans forward (10) surface, the rear end cap (905) Portion, the binding post (904) are vertically fixed on the outer surface of rear end cap (905) and with hypsokinesis switch block (7) in the switch block that leans forward (10) internal circuit board electrical connection.
- The system 2. a kind of constant fixed-wing of center of gravity according to claim 1 verts, it is characterised in that：The propeller (8) it is equipped with two or more and be yi word pattern structure.
- The system 3. a kind of constant fixed-wing of center of gravity according to claim 1 verts, it is characterised in that：The hypsokinesis switch block (7) it is parallel to each other with the switch block that leans forward (10).
- The system 4. a kind of constant fixed-wing of center of gravity according to claim 1 verts, it is characterised in that：The preceding contact wheel (12), rear movable pulley (13) is in same level.
- The system 5. a kind of constant fixed-wing of center of gravity according to claim 1 verts, it is characterised in that：First wing (1) it is mutually symmetrical with by main body (3) and the second wing (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721348025.6U CN207346076U (en) | 2017-10-18 | 2017-10-18 | A kind of constant fixed-wing of center of gravity verts system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721348025.6U CN207346076U (en) | 2017-10-18 | 2017-10-18 | A kind of constant fixed-wing of center of gravity verts system |
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| CN207346076U true CN207346076U (en) | 2018-05-11 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111490639A (en) * | 2020-05-25 | 2020-08-04 | 贵州雅光电子科技股份有限公司 | Power electronic equipment output end fixing structure of motor |
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2017
- 2017-10-18 CN CN201721348025.6U patent/CN207346076U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111490639A (en) * | 2020-05-25 | 2020-08-04 | 贵州雅光电子科技股份有限公司 | Power electronic equipment output end fixing structure of motor |
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