CN208641742U - A kind of fixed-wing model plane wing dress fleet-footed runner - Google Patents
A kind of fixed-wing model plane wing dress fleet-footed runner Download PDFInfo
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- CN208641742U CN208641742U CN201821129501.XU CN201821129501U CN208641742U CN 208641742 U CN208641742 U CN 208641742U CN 201821129501 U CN201821129501 U CN 201821129501U CN 208641742 U CN208641742 U CN 208641742U
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- model plane
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Abstract
The utility model relates to a kind of fixed-wing model plane wings to fill fleet-footed runner, it includes and puts on the identical integrated fuselage of people's monnolithic case when wing dress is in state of flight, it is installed on the headstock of integrated fore-body and is installed on the rudder and empennage of integrated fuselage afterbody, Power Component is installed on headstock, headstock is by the cabin that is located at below integrated fuselage and is fixed on above cabin and extend out to the support frame of integrated body upper upwards and forms, Power Component is by lithium battery, expelling plate, motor, protective cover and blade composition, lithium battery and expelling plate are installed in cabin, motor and protective cover are fixed on above support frame, the output end of motor is fixedly connected with blade, expelling plate is connect with a wireless remote control signal.Beneficial effect is: the utility model is effectively combined fixed-wing model plane with wing dress flight concept, devises out the fixed-wing model plane wing dress fleet-footed runner of good a flight effect, shape and unique structure, deep to be liked by airplane hobbyist.
Description
Technical field
The utility model belongs to model plane and aircraft field, and in particular to a kind of fixed-wing model plane wing dress fleet-footed runner.
Background technique
Wing dress is a kind of special jump wear, is called flying squirrel dress.Wing dress flight, is also named the gliding of short distance horizon, is
Refer to that aviator wears wing dress, under flying from high building, high tower, bridge, steep cliff, helicopter, be close to high aerial building or from
Right landscape carries out unpowered flight.Aeromodelling aerocraft is divided into three categories, and is that fixed-wing (aerodone), helicopter and multiaxis fly respectively
Row device, the model plane of fixed-wing are more in the prior art, but have no and set fixed-wing model plane with what wing dress flight concept combined
The aircraft of meter.
Utility model content
The utility model provides a kind of fixed-wing model plane wing dress fleet-footed runner, it is intended to which fixed-wing model plane and the wing are filled flight concept knot
The strong Novel model airplane of a kind of unique structure, interest is designed altogether.
The technical solution that the utility model solves above-mentioned technical problem is as follows: a kind of fixed-wing model plane wing dress fleet-footed runner, packet
Include that identical as people monnolithic case of the wing dress in state of flight when is put on (so-called monnolithic case is identical herein simply means to shape phase
With not limiting specific size) integrated fuselage, be installed on the headstock of the integrated fore-body and be installed on institute
The rudder and empennage of integrated fuselage afterbody are stated, Power Component is installed, the headstock is by being located at institute on the headstock
It states the cabin below integrated fuselage and is fixed on above cabin and extend out to upwards the support frame of the integrated body upper
Composition, the Power Component are made of lithium battery, expelling plate, motor, protective cover and blade, the lithium battery and expelling plate installation
In in the cabin, the motor and protective cover are fixed on above support frame as described above, the output end of the motor and the blade
It is fixedly connected, the expelling plate is connect with a wireless remote control signal.
Compared with prior art, the utility model has the beneficial effects that
The utility model is effectively combined fixed-wing model plane and the wing dress flight concept, devise out a flight effect it is good,
The fixed-wing model plane wing of shape and unique structure fills fleet-footed runner, provides for airplane hobbyist a in the prior art without novel boat
Mould, can steadily controllable flight and when flight posture especially, interest it is stronger, it is deep to be liked by airplane hobbyist.
Based on the above technical solution, the utility model can also do following improvement.
Further, the integrated fuselage is by being located at intermediate fuselage plate in the horizontal direction and being located at the fuselage plate
The acclivitous flank of two sides forms, and the angle between the flank and fuselage plate is 8-20 degree.
Further, the empennage is two long slabs for being symmetrically disposed on the integral machine body lower rear, the long slab
It is vertically arranged and stretches along the longitudinal direction.
Further, two long front edge of board have angle, and the angle of angle is 0-4 degree.
Beneficial effect using above-mentioned further scheme is preferably to promote lift in flight, is conducive to reduce power
The power of component.
Further, the angle for the central axis that the output shaft of the motor stretches along the longitudinal direction with the fuselage plate is
0-2 degree, the rear end of the output shaft of the motor are fixedly connected with the blade, and the output shaft is horizontally disposed with or the low rear end in front end
Height, the angle between the output shaft and horizontal plane are 0-5 degree.
Beneficial effect using above-mentioned further scheme is more stable when making flight.
Further, the rudder is by vertical tail, electromagnetic coil, magnet and rudder face board group at the vertical tail, is along vertical
Direction is fixed on the central axis of the top of the integrated fuselage afterbody, and the electromagnetic wire is fixed on the vertical tail,
Circle, the magnet are located in the electromagnetic coil, and the front of the rudder face plate is connect with the vertical tail, after the rudder face plate
Portion can swing relative to the front of the rudder face plate, the front end at the rear portion that the rudder face plate can swing and the magnet
Connection.
Beneficial effect using above-mentioned further scheme is to be conducive to easily control wing dress fleet-footed runner's turning.
Further, the Power Component further includes guard circle, and the guard circle is fixedly connected with the motor, the blade
In the guard circle.
Beneficial effect using above-mentioned further scheme is to protect motor and prevent cabin water inlet and dust.
Further, control stick and open-close on-off are provided on the Digiplex.
Detailed description of the invention
Fig. 1 is the overall structure diagram that a kind of fixed-wing model plane wing provided by the utility model fills fleet-footed runner；
Fig. 2 is the explosive view that a kind of fixed-wing model plane wing provided by the utility model fills fleet-footed runner；
Fig. 3 is the schematic diagram for the Digiplex that the fixed-wing model plane wing provided by the utility model fills fleet-footed runner.
In attached drawing, parts list represented by the reference numerals are as follows:
1. integrated fuselage；2. headstock；3. empennage；4. Power Component；5. rudder；6. Digiplex；7. flank；
8. lithium battery；9. expelling plate；10. motor；11. protective cover；12. blade；13. guard circle；14. vertical tail,；15. electromagnetic coil；
16. magnet；17. rudder face plate.
Specific embodiment
The principles of the present invention and feature are described below in conjunction with attached drawing, example is served only for explaining that this is practical
It is novel, it is not intended to limit the scope of the utility model.
As shown in Figures 1 to 3, the utility model provides a kind of fixed-wing model plane wing dress fleet-footed runner comprising with put at wing dress
The identical integrated fuselage 1 of people's monnolithic case when state of flight, the headstock 2 for being installed on 1 front of the integrated fuselage
And it is installed on the rudder 5 and empennage 3 at 1 rear portion of the integrated fuselage, Power Component 4, institute are installed on the headstock 2
Headstock 2 is stated by the cabin positioned at integrated 1 lower section of fuselage and is fixed on above cabin and extend out to the one upwards
Change the support frame composition of 1 top of fuselage, the Power Component 4 is by lithium battery 8, expelling plate 9, motor 10, protective cover 11 and blade
12 compositions, the lithium battery 8 and expelling plate 9 are installed in the cabin, and the motor 10 and protective cover 11 are fixed on the branch
Above support, the output end of the motor 10 is fixedly connected with the blade 12, and the expelling plate 9 and a Digiplex 6 are believed
Number connection.
Further, the integrated fuselage 1 is by being located at intermediate fuselage plate in the horizontal direction and putting down positioned at the fuselage
The acclivitous flank 7 of plate two sides forms, and the angle between the flank 7 and fuselage plate is 8-20 degree.
It should be noted that the connection of integration fuselage and headstock, empennage can be viscous to be removably clamped or fixing
It connects.Integrated fuselage, organ's seat, empennage etc. are made of foamed materials such as EPO or KT, the fuselage plate of integrated fuselage, two
The thickness of flank is about 4-8mm.
Further, the empennage 3 is two long slabs for being symmetrically disposed on 1 lower rear of the integrated fuselage, the length
Plate is vertically arranged and stretches along the longitudinal direction.
Further, two long front edge of board have angle, and the angle of angle is 0-4 degree.
Further, the angle for the central axis that the output shaft of the motor 10 and the fuselage plate stretch along the longitudinal direction
For 0-2 degree, the rear end of the output shaft of the motor 10 is fixedly connected with the blade 12, and the output shaft is horizontally disposed with or front end
Low rear end is high, and the angle between the output shaft and horizontal plane is 0-5 degree.
It should be noted that above is referred to 0 degree of two component parallels of expression when angle.
Further, the rudder 5 is made of vertical tail, 14, electromagnetic coil 15, magnet 16 and rudder face plate 17, described vertical
The wing 14 is fixed on along the vertical direction on the central axis of the top at 1 rear portion of the integrated fuselage, fixed on the vertical tail, 14
Have the electromagnetic coil 15, the magnet 16 is located in the electromagnetic coil 15, the front of the rudder face plate 17 with it is described vertical
The wing 14 connects, and the rear portion of the rudder face plate 17 can swing relative to the front of the rudder face plate 17, and the rudder face plate 17 can
The front end at the rear portion to swing is connect with the magnet 16.
It should be noted that generating magnetic force when electromagnetic coil is powered makes side-to-side movement (the electromagnetic coil electricity in it of magnet 16
Stream direction change changes magnetic force direction), so that the rear portion of rudder face plate be driven to swing.
Further, the Power Component 4 further includes guard circle 13, and the guard circle 13 is fixedly connected with the motor 10,
The blade 12 is located in the guard circle 13.
It should be noted that guard circle covers blade from front, blade is rearward blown, and the structure of guard circle is similar to
The fan guard for the half that electric fan rear portion is connect with head, it acts as blade is protected, blade when preventing from surprisingly landing
By collision behaviour's wound.
Further, control stick and open-close on-off are provided on the Digiplex 6.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (8)
1. a kind of fixed-wing model plane wing fills fleet-footed runner, which is characterized in that including with to put on people of the wing dress in state of flight when whole
The identical integrated fuselage (1) of shape is installed on the headstock (2) of described integrated fuselage (1) front and is installed on described
The rudder (5) and empennage (3) at integrated fuselage (1) rear portion are equipped with Power Component (4), the machine on the headstock (2)
Headstock (2) is by the cabin below the integrated fuselage (1) and is fixed on above cabin and extend out to the one upwards
Change the support frame composition above fuselage (1), the Power Component (4) is by lithium battery (8), expelling plate (9), motor (10), protection
(11) and blade (12) is covered to form, the lithium battery (8) and expelling plate (9) are installed in the cabin, the motor (10) and
Protective cover (11) is fixed on above support frame as described above, and the output end of the motor (10) is fixedly connected with the blade (12), institute
Expelling plate (9) is stated to connect with a Digiplex (6) signal.
2. a kind of fixed-wing model plane wing according to claim 1 fills fleet-footed runner, which is characterized in that the integration fuselage (1)
It is formed by being located at intermediate fuselage plate in the horizontal direction and the acclivitous flank (7) positioned at fuselage plate two sides,
Angle between the flank (7) and fuselage plate is 8-20 degree.
3. a kind of fixed-wing model plane wing according to claim 2 fills fleet-footed runner, which is characterized in that the empennage (3) is symmetrical
Two long slabs of described integrated fuselage (1) lower rear are set to, the long slab is vertically arranged and stretches along the longitudinal direction.
4. a kind of fixed-wing model plane wing according to claim 3 fills fleet-footed runner, which is characterized in that two long front edge of board at
One angle, the angle of angle are 0-4 degree.
5. a kind of fixed-wing model plane wing according to claim 2 fills fleet-footed runner, which is characterized in that the output of the motor (10)
The angle for the central axis that axis and the fuselage plate stretch along the longitudinal direction is 0-2 degree, the output shaft of the motor (10)
Rear end is fixedly connected with the blade (12), and the output shaft is horizontally disposed or the low rear end in front end is high, the output shaft and level
Angle between face is 0-5 degree.
6. a kind of fixed-wing model plane wing according to any one of claims 1 to 5 fills fleet-footed runner, which is characterized in that the direction
Rudder (5) is made of vertical tail, (14), electromagnetic coil (15), magnet (16) and rudder face plate (17), and the vertical tail, (14) is along vertical
Direction is fixed on the central axis of the top at described integrated fuselage (1) rear portion, is fixed on the vertical tail, (14) described
Electromagnetic coil (15), the magnet (16) are located in the electromagnetic coil (15), and the front of the rudder face plate (17) is hung down with described
The straight wing (14) connection, the rear portion of the rudder face plate (17) can swing relative to the front of the rudder face plate (17), the rudder
The front end at the rear portion that panel (17) can swing is connect with the magnet (16).
7. a kind of fixed-wing model plane wing according to any one of claims 1 to 5 fills fleet-footed runner, which is characterized in that the power
Component (4) further includes guard circle (13), and the guard circle (13) is fixedly connected with the motor (10), and the blade (12) is located at
In the guard circle (13).
8. a kind of fixed-wing model plane wing according to any one of claims 1 to 5 fills fleet-footed runner, which is characterized in that described wireless
Remote controler is provided with control stick and open-close on-off on (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821129501.XU CN208641742U (en) | 2018-07-17 | 2018-07-17 | A kind of fixed-wing model plane wing dress fleet-footed runner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821129501.XU CN208641742U (en) | 2018-07-17 | 2018-07-17 | A kind of fixed-wing model plane wing dress fleet-footed runner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208641742U true CN208641742U (en) | 2019-03-26 |
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ID=65785303
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821129501.XU Active CN208641742U (en) | 2018-07-17 | 2018-07-17 | A kind of fixed-wing model plane wing dress fleet-footed runner |
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| Country | Link |
|---|---|
| CN (1) | CN208641742U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112527004A (en) * | 2020-10-22 | 2021-03-19 | 泰州镭昇光电科技有限公司 | Speed and direction integrated regulation and control system |
-
2018
- 2018-07-17 CN CN201821129501.XU patent/CN208641742U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112527004A (en) * | 2020-10-22 | 2021-03-19 | 泰州镭昇光电科技有限公司 | Speed and direction integrated regulation and control system |
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