CN206107561U - Long flight time aircraft - Google Patents
Long flight time aircraft Download PDFInfo
- Publication number
- CN206107561U CN206107561U CN201621167335.3U CN201621167335U CN206107561U CN 206107561 U CN206107561 U CN 206107561U CN 201621167335 U CN201621167335 U CN 201621167335U CN 206107561 U CN206107561 U CN 206107561U
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- China
- Prior art keywords
- aileron
- motor
- central plate
- connecting rod
- aircraft
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- 239000007787 solid Substances 0.000 claims description 3
- 238000010276 construction Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
Abstract
The utility model belongs to unmanned aerial vehicle prepares the field, especially relates to a long flight time aircraft. This aircraft includes: regular hexagon's well core plate, during core plate includes in should core plate with down in core plate, be provided with the position that six angles of regular hexagon between core plate and the lower well core plate are connected in last to six ailerons, have 3 between aileron and the well core plate 5 the last angle of inclination of degree, aileron tip are furnished with the screw, and the screw is after the rotation, and the promotion air current of production is to the well core plate outside. The utility model discloses does the aileron carry on 3 simultaneously 5 the upper counterangle of degree is connected, and the screw is after the rotation, and the promotion air current of production is to outside the well core plate, and at this moment, the lift of aircraft is to the inboard to the efficiency of having saved the motor has improved the time of flying.
Description
Technical field
The utility model belongs to unmanned machine preparation field, more particularly to aircraft during a kind of long boat.
Background technology
Due to being to use battery to be powered, flight always researcher wishes what is solved to unmanned plane during long boat
Problem, in addition to increasing the capacity of battery, also having reach flying for long time by mitigating weight and reach the light purpose of bearing a heavy burden, but
All there is a problem of it is certain, aircraft kick the beam can cause flight it is unstable, the capacity increase of battery can increase the weight of battery
Amount.
Utility model content
Technical problem to be solved in the utility model is aircraft when providing a kind of long boat, is increased by the change of structure
Plus the flight time.
A kind of aircraft when the utility model is achieved in that long boat, the aircraft includes：Orthohexagonal center
Plate, the central plate includes upper central plate and lower central plate, is provided with six ailerons and is connected between central plate and lower central plate
The position at orthohexagonal six angles, the tilt angle with 3-5 degree between aileron and central plate, aileron end is furnished with spiral
Oar, after rotation, the promotion air-flow of generation is to central plate outside for screw.
Further, the aileron is connected to orthohexagonal central plate by aileron folded piece, and the folded piece includes
Two parallel fixed seats, are connected between upper central plate and lower central plate by fixed seat, are set in two parallel fixed seats
Bolt sliding bar is set in the guide chute of horizontalization row, two guide chutes, in the guide chute of two parallel fixed seats
Rear side is connected two fixed seats by a connecting rod with holes, position centered on the hole, vertical on the bolt sliding bar
Connection jackscrew, is inserted in after limit spring the hole through connecting rod on the jackscrew, arrange aileron horn connecting seat by rotating shaft with it is solid
Reservation connects, and in connecting seat both sides semicircle limit fastener is arranged, and when aileron horn launches, bolt sliding bar blocks buckle, and
Carry out spacing.
Further, the outer side-lower in two fixed seats arranges connection otic placode, also including aileron horn connecting seat, aileron horn
Connecting seat is set to cylindrical structure, and the lower section both sides of cylinder have a connection otic placode of triangle, the connection otic placode of triangle with it is solid
The connection otic placode of reservation is formed connecting seat and is connected with fixed seat axle after spiral shell axle connection, and the axis of connecting seat cylinder is with
Core place plane has the tilt angle of 3-5 degree.
Further, the connection otic placode downside of the triangle arranges spacing preiection, on the inside of the connection otic placode of fixed seat
It is raised spacing in groove when connecting seat is folded when rotating with 90 degree of groove.
Further, bolt hole is set on cylinder, is connected with aileron connecting rod by bolt.
Further, the aileron connects screw by aileron connecting rod, motor is connected in the aileron connecting rod and is connected
Female connector, motor connection set is nested into the end of aileron connecting rod, and motor connection set is integrally formed with motor base, and motor cover is inserted in
Is tightly connected in motor base and then by motor cover, motor is fixed in motor base, the stator axis base of motor and motor
Base connects, and screw is fixed on the outer rotor of motor by fixed lower sheeting with fixed upper compressing tablet.
Further, motor connection set inner side arranges a spacing preiection bar, and in aileron connecting rod limited impression is arranged, and leads to
Cross spacing preiection bar and limited impression cause plane that the motor base of aileron motor is located and central plate planar offset 2.7～
2.9 degree.
Further, skew includes that left avertence is moved and right avertence shifting, wherein, two adjacent motor bases are contrary deviation angle
Degree.
Compared with prior art, beneficial effect is the utility model：The utility model aileron carries out the upper of 3-5 degree simultaneously
Dihedral connects, screw after rotation, the promotion air-flow of generation to central plate outside, now, the lift of aircraft to inner side, from
And the efficiency of motor is saved, improve the time of flight.Aileron folded piece, aileron are connected to by orthohexagonal central plate
On the central plate, in flight course, central plate entire area stress passes to shaking for central plate so as to reduce motor for connection
It is dynamic so that structure connection is more firm.Central plate is the design of hermetically sealed waterproof construction.
In flight course, motor can produce torsion, in order to offset this torsion, coaxial motor be it is clockwise with it is counterclockwise
Rotation, in order to more stable, and improves efficiency, and the deviation angle of motor is set to into 2.7 degree, because aircraft during long boat, electricity
The rotating speed of machine is relatively low, and the diameter of screw is larger with pitch, and response speed is slower, and its reaction torque effect is poor, 2.7 degree of setting
Deviation angle increases reaction torque power.
Description of the drawings
Fig. 1 is the Flight Vehicle Structure schematic diagram that the utility model embodiment is provided；
Fig. 2 is the detonation configuration figure of aileron in the aircraft that the utility model embodiment is provided；
Fig. 3 is to connect top surface structure figure in folded piece in the aircraft that the utility model embodiment is provided.
Specific embodiment
In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and enforcement
Example, is further elaborated to the utility model.It should be appreciated that specific embodiment described herein is only to explain
The utility model, is not used to limit the utility model.
Referring to Fig. 1, the aircraft includes：Orthohexagonal central plate 1, the central plate 1 include upper central plate 101 with it is lower in
Core 102, is provided with the position that six ailerons 2 are connected to orthohexagonal six angles between central plate 101 and lower central plate 102
Put, the tilt angle with 3-5 degree between aileron 2 and central plate 1, six ailerons 2 carry out the upper counterangle connection of 3-5 degree simultaneously,
Screw after rotation, the promotion air-flow of generation to central plate outside, now, the lift of aircraft to inner side, so as to save
The efficiency of motor, improves the time of flight.Aileron folded piece is connected to by orthohexagonal central plate, during aileron is connected to
On core, in flight course, the entire area stress of central plate 1, so as to reduce the vibration that motor passes to central plate so that knot
Structure connection is more firm.Central plate 1 is the design of hermetically sealed waterproof construction.
Fig. 3 is combined referring to Fig. 2, the connection folded piece between central plate 1 and aileron 2, including two parallel fixed seats
501, it is connected between upper central plate 101 and lower central plate 102 by fixed seat 501, arrange in two parallel fixed seats 501
Bolt sliding bar 502 is set in parallel guide chute 507, two guide chutes 507, in two parallel fixed seats 501
The rear side of guide chute 507 is connected two fixed seats 501 by one with holes 510 connecting rod 508 (referring to Fig. 3), and hole is arranged
Vertical connection jackscrew 511 (referring to Fig. 3), is inserted in after limit spring through connection on jackscrew on center, bolt sliding bar
The hole 510 of bar 508.
Connection otic placode 509 is set in the outer side-lower of two fixed seats 501, aileron horn connecting seat 504 is cylindrical structure, round
The lower section both sides of cylinder have the connection otic placode 506 of triangle, the connection otic placode 506 of triangle and the connection otic placode 509 of fixed seat
By a spiral shell axle connect 503 connect after, form connecting seat 504 and be connected with the axle of fixed seat 501, the setting of the connection otic placode of triangle downside is limited
Position raised 512, the groove 513 on the inside of the connection otic placode of fixed seat with 90 degree is raised when connecting seat is folded when rotating
It is spacing in groove so that, 90 degree can only be folded between connecting seat and fixed seat, prevent from stretching disconnected by connecting line and touch it
His equipment.Semicircle limit fastener 505 is set in connecting seat both sides, when aileron connecting rod 203 is launched, bolt sliding bar 502 will
Buckle card 505 is lived, and carry out it is spacing, need fold when, by slide bolt sliding bar backward, buckle depart from bolt sliding bar,
After connecting seat is rotated with fixed seat axle, spacing in groove, 90 degree of foldings of central plate and aileron are snapped in by projection.
The cylinder of aileron horn connecting seat 504 has the upper counterangle of 3-5 degree with the place plane of central plate 1.Spiral shell is set on cylinder
Keyhole, is connected by bolt with aileron connecting rod 203.
Referring to Fig. 2, aileron connecting rod connection motor connection set 204, motor connection set 204 is nested into aileron connecting rod 203
End, motor connection set 204 inner side arrange a spacing preiection bars, limited impression, motor connection are set in aileron connecting rod
Set is connected on motor assembly 202, and motor assembly 202 includes the motor base 205 being formed in one with motor connection set, motor
Machine governor is set in base 205, motor cover 206 is inserted in motor base 205 and then is tightly connected by motor cover 207, electricity
Machine is fixed in motor base, and the stator axis base of motor is connected with motor base, and screw 201 is by fixed lower sheeting 208
It is fixed on the outer rotor of motor with fixed upper compressing tablet 209.
Can produce after connection between draw runner that six ailerons are set in aileron connecting rod and motor cabinet and groove structure
(groove that the draw runner that sets in motor cabinet is arranged with aileron horn have between the two relative to the horizontal line skew of aileron horn 2.7 degree),
Here skew includes that left avertence is moved and right avertence shifting, wherein, two adjacent aileron motors are contrary deviation angle.Including relative
Central plate plane inclines clockwise the plane that 2.7 degree of ailerons are formed, and the plane that another aileron motor is formed is with respect to central plate plane
2.7 degree are inclined counterclockwise.
In flight course, aileron motor can produce torsion, in order to offset this torsion, coaxial motor be it is clockwise with it is inverse
Hour hands rotate, and in order to more stable, and improve efficiency, the deviation angle of motor are set to into 2.7 degree, because flying during long boat
Device, the rotating speed of motor is relatively low, and the diameter of screw is larger with pitch, and response speed is slower, and its reaction torque effect is poor, setting
2.7 degree of deviation angles increase reaction torque power.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
Any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (8)
1. aircraft when a kind of length is navigated, it is characterised in that the aircraft includes：Orthohexagonal central plate, the central plate includes
Upper central plate and lower central plate, are provided with six ailerons and are connected to orthohexagonal six angles between central plate and lower central plate
Position, the tilt angle with 3-5 degree between aileron and central plate, aileron end is furnished with screw, screw after rotation,
The promotion air-flow of generation is to central plate outside.
2. according to aircraft during the long boat described in claim 1, it is characterised in that the aileron is connected to by aileron folded piece
Orthohexagonal central plate, the folded piece includes two parallel fixed seats, and upper central plate is connected to under by fixed seat
Between central plate, parallel guide chute is set in two parallel fixed seats, bolt sliding bar is set in two guide chutes,
In the rear side of the guide chute of two parallel fixed seats two fixed seats are connected by a connecting rod with holes, the hole is
Center, vertical connection jackscrew, is inserted in after limit spring the hole through connecting rod on the bolt sliding bar on the jackscrew,
Arrange aileron horn connecting seat to be connected with fixed seat by rotating shaft, semicircle limit fastener is set in connecting seat both sides, aileron launches
When, bolt sliding bar blocks buckle, and carries out spacing.
3. according to aircraft during the long boat described in claim 2, it is characterised in that arrange in the outer side-lower of two fixed seats and connect
Ear connecting plate, also including aileron horn connecting seat, aileron horn connecting seat is set to cylindrical structure, and the lower section both sides of cylinder have triangle
Connection otic placode, after the connection otic placode of triangle is connected with the connection otic placode of fixed seat by a spiral shell axle, form connecting seat and solid
Reservation axle connects, and axis and the central plate place plane of connecting seat cylinder have the tilt angle of 3-5 degree.
4. according to aircraft during the long boat described in claim 3, it is characterised in that the connection otic placode downside of the triangle is arranged
Spacing preiection, the groove on the inside of the connection otic placode of fixed seat with 90 degree is raised spacing when connecting seat is folded when rotating
In groove.
5. according to aircraft during the long boat described in claim 3, it is characterised in that arrange bolt hole on cylinder, by bolt with
Aileron connecting rod connects.
6. according to aircraft during the long boat described in claim 3, it is characterised in that the aileron connects spiral shell by aileron connecting rod
Rotation oar, connects motor connection set in the aileron connecting rod, motor connection set is nested into the end of aileron connecting rod, motor connection
Set is integrally formed with motor base, and machine governor is set in motor base, and motor cover is inserted in motor base and then by motor
Cover seal connects, and motor is fixed in motor base, and the stator axis base of motor is connected with motor base, and screw is by fixing
Lower sheeting is fixed on the outer rotor of motor with fixed upper compressing tablet.
7. according to aircraft during the long boat described in claim 6, it is characterised in that motor connection set inner side arranges a spacing preiection
Bar, in aileron connecting rod limited impression is arranged, and by spacing preiection bar and limited impression the motor base of aileron motor is caused
2.7～2.9 degree of the plane at place and central plate planar offset.
8. according to aircraft during the long boat described in claim 7, it is characterised in that skew includes that left avertence is moved and right avertence is moved, wherein,
Two adjacent motor bases are contrary deviation angle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621167335.3U CN206107561U (en) | 2016-10-26 | 2016-10-26 | Long flight time aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621167335.3U CN206107561U (en) | 2016-10-26 | 2016-10-26 | Long flight time aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206107561U true CN206107561U (en) | 2017-04-19 |
Family
ID=58524958
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621167335.3U Expired - Fee Related CN206107561U (en) | 2016-10-26 | 2016-10-26 | Long flight time aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206107561U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379522A (en) * | 2016-10-26 | 2017-02-08 | 辽宁电力建设监理有限公司 | Long-endurance aircraft |
-
2016
- 2016-10-26 CN CN201621167335.3U patent/CN206107561U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106379522A (en) * | 2016-10-26 | 2017-02-08 | 辽宁电力建设监理有限公司 | Long-endurance aircraft |
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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 |
Granted publication date: 20170419 Termination date: 20181026 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |