CN204916173U - Multiaxis aircraft with horn swing function - Google Patents
Multiaxis aircraft with horn swing function Download PDFInfo
- Publication number
- CN204916173U CN204916173U CN201520438336.6U CN201520438336U CN204916173U CN 204916173 U CN204916173 U CN 204916173U CN 201520438336 U CN201520438336 U CN 201520438336U CN 204916173 U CN204916173 U CN 204916173U
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- Prior art keywords
- horn
- axle bed
- axle
- gear
- swing
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Abstract
The utility model discloses an installed simple structure, processing convenience, low cost, had self -locking function's swing mechanism's multiaxis aircraft with horn swing function, support among the swing mechanism comprises last bottom plate, axle bed, worm gear transmission mechanism, bevel gear, support arm, and this swing mechanism installs in the multiaxis aircraft in pairs, also can install according to the needs of horn quantity, and this swing mechanism makes horn luffing motion angle big, swings reliable and stablely. The swing of one or many horns can be done to the swing mechanism of installation motor made multiaxis aircraft with horn swing function on the worm horn, and the swing is synchronal or criss -cross or goes on in proper order, has increased the interest of flight like this, has tempered people's the ability of controlling.
Description
Technical field
The utility model relates to Multi-axis aircraft field, the Multi-axis aircraft of particularly horn swing.
Background technology
The horn of remote control Multi-axis aircraft was all can not make vertical direction upper in the past, lower swing, some remote control Multi-axis aircrafts have all installed the The Cloud Terrace with shooting equipment now, the interference of any object is not subject in order to make the camera lens of the shooting equipment in The Cloud Terrace, so horn is made the swing making vertical direction, make horn or foot rest not check rail before the camera lens of shooting equipment, affect the effect of photographic images, will horn be connected on a swinging gear like this, this swinging gear connects fuselage, the work of operation swinging gear makes horn swing to not in the scope of angle lens.Existingly be arranged in Multi-axis aircraft that the mechanism structure that horn can be made to swing is complicated, processing trouble, Multi-axis aircraft is that installation two horns are done to swing simultaneously, produce the swinging gear that installation two horns are done to swing, install four, six, eight ... wait horn work to swing, produce four, six, eight ... horn etc. make the swinging gear swung, such productive costs is just high, the swinging gear of this corresponding horn quantity lacks the alerting ability of assembling, thus too increases this cost having the remote control Multi-axis aircraft of swinging gear of production.The simultaneously existing horn remote control Multi-axis aircraft that can swing, can not carry out a horn and swing or the swing of many horn intersections or the action such as swing successively gradually.
Summary of the invention
The utility model provides that a kind of swinging gear structure of installation is simple, easy to process, cost is low, use is reliable, swinging gear has auto-lock function, make any bar horn make the Multi-axis aircraft with horn oscillating function of wobbling action.
For solving the problems of the technologies described above, the technical scheme that the utility model adopts is: the Multi-axis aircraft with horn oscillating function, comprise Multi-axis aircraft 100, described Multi-axis aircraft 100 installs swinging gear 50, support 1 in described swinging gear 50 comprises, bottom plate 1-1, 1-2, first axle bed 1-3, second axle bed 1-4, 3rd axle bed 1-5, 4th axle bed 1-6, Worm wheel transmission mechanism 2, Worm wheel transmission mechanism 2 is provided with in described support 1, described first axle bed axle bed 1-3, the first through hole 1-31 set by second axle bed 1-4, second through hole 1-41 connects the bearing set by axle 2-11 of the worm gear 2-1 of Worm wheel transmission mechanism 2, described worm gear 2-1 engages worm 2-2, bearing set by described worm screw 2-2 both sides connects the 3rd axle bed 1-5, third through-hole 1-51 set by 4th axle bed 1-6, fourth hole 1-61, the top position Connectable umbrella gear 2-22 of described worm screw 2-2 in the outside of the 4th axle bed 1-6 or motor 2-22, described worm gear 2-1 side is provided with support arm 3, described support arm 3 connects horn 4 side, described horn 4 opposite side connects attaching parts 5, axle 6-1 set in swing arm 6 set by described attaching parts 5 is flexibly connected the side of connecting rod 7, the opposite side of described connecting rod 7 is flexibly connected axle 8-1 set in Connection Block 8, on described, bottom plate 1-1, 1-2 side is provided with open slot 1-0, the opposite side of described bottom plate 1-2 is provided with at least two screw 1-20.
Further, described bevel gear 2-22 meshing bevel gear 9, the bearing set by axle 9-1 side of described bevel gear 9 is connected and fixed the fifth hole 10-0 set by plate 10 center, described adapter plate 10 is provided with permanent seat 11, the 6th through hole 11-0 set by described permanent seat 11 connects the bearing set by described axle 9-1 opposite side, and the shaped position of the quantity that the edge of described adapter plate 10 is installed according to swinging gear 50 and installation is provided with the 7th through hole 10-1 of the screw 1-20 set by corresponding bottom plate 1-2.
The beneficial effects of the utility model are: use Worm wheel transmission mechanism as swing element in the horn swinging gear installed in Multi-axis aircraft, swinging gear is made to have self-locking property, can not produce after horn swings to position and loosen dislocation, the propulsive effort swung is large, and the swinging gear of horn is set according to the horn quantity that remote control Multi-axis aircraft will configure, configuration two swinging gear of two horns, the configuration swinging gear of four horns, is configured swinging gear by that analogy.Swinging gear can also configure motor one to one simultaneously, and the wobbling action of swinging gear is by electric machine control.Make Multi-axis aircraft can realize one or more horn to swing simultaneously or intersect and swing or the action such as swing successively gradually, which adds the interest of various change of the in-flight flare maneuver of remote control Multi-axis aircraft, also temper the manipulation ability of people.Multi-axis aircraft mechanism structure of the present invention is simple, easy to process, low production cost, thus reduces the productive costs of remote control Multi-axis aircraft.
Accompanying drawing explanation
Fig. 1 is the schematic diagram that the utility model has the swinging gear of the Multi-axis aircraft Install and configure bevel gear of horn oscillating function.
Fig. 2 is the schematic diagram that the utility model has the swinging gear of the multiaxis flight Install and configure motor of horn oscillating function.
Detailed description of the invention
As shown in Figure 1 to Figure 2, the utility model has the detailed description of the invention of the Multi-axis aircraft of horn oscillating function, there is the Multi-axis aircraft of horn oscillating function, comprise Multi-axis aircraft 100, described Multi-axis aircraft 100 installs swinging gear 50 makes horn 4 swing, and the support 1 in described swinging gear 50 comprises upper and lower fixing plate 1-1,1-2, the first axle bed 1-3, the second axle bed 1-4, the 3rd axle bed 1-5, the 4th axle bed 1-6, Worm wheel transmission mechanism 2.
Be provided with Worm wheel transmission mechanism 2 in described support 1, described first axle bed 1-3, the first through hole 1-31 set by the second axle bed 1-4, the second through hole 1-41 connect the bearing set by worm gear 2-1 axle 2-11, described worm gear 2-1 engages worm 2-2.
Bearing set by described worm screw 2-2 side connects the 3rd axle bed 1-5, the third through-hole 1-51 set by the 4th axle bed 1-6, fourth hole 1-61, the top position Connectable umbrella gear 2-22 of described worm screw 2-2 in the outside of the 4th axle bed 1-6 or motor 2-22.
Described worm gear 2-1 side is provided with support arm 3, described support arm 3 connects horn 4 side, described horn 4 opposite side connects attaching parts 5, and axle 6-1 set in the swing arm 6 set by described attaching parts 5 is flexibly connected the side of connecting rod 7, and the opposite side of described connecting rod 7 is flexibly connected the axle 8-1 set by Connection Block 8.The motor driving screw propeller is installed at position, swing arm top.
Described upper and lower fixing plate 1-1,1-2 side is provided with open slot 1-0, and the opposite side of described bottom plate 1-2 is provided with at least two screw 1-20.The both sides of the open slot 1-0 that the first axle bed 1-3, the second axle bed 1-4 that are mounted with worm gear are arranged on set by upper and lower fixing plate 1-1,1-2 are screwed.Worm screw side is connected in the 3rd axle bed 1-5, the 4th axle bed 1-6, and the 3rd axle bed 1-5, the 4th axle bed 1-6 are arranged on the middle side of the first axle bed 1-3, the second axle bed 1-4, at position, worm screw top Connectable umbrella gear 2-22 or the motor 2-22 of this side.
Described bevel gear 2-22 meshing bevel gear 9, the bearing set by axle 9-1 side of described bevel gear 9 is connected and fixed the fifth hole 10-0 set by plate 10 center, described adapter plate 10 is provided with permanent seat 11, the 6th through hole 11-1 set by described permanent seat 11 connects the bearing set by axle 9-1 opposite side of described bevel gear 9, and this side of described axle 9-1 connects motor 30.
The quantity that the edge of described adapter plate 10 is installed according to swinging gear 50 and shaped position are provided with the 7th through hole 10-1 of the screw 1-20 set by corresponding bottom plate 1-2.When a frame remote control Multi-axis aircraft arranges symmetrical placement two horns, with the swinging gear of two configuration bevel gears, by four horn symmetrical placement, with the swinging gear of four configuration bevel gears, these swinging gear are fixedly connected on adapter plate 10, then horn is fixedly connected on support arm, Connection Block 8 is screwed with the lower surface being arranged on body plate (body plate does not mark at this) perpendicular to the axis of worm-wheel shaft.Axle in Connection Block 8 is flexibly connected connecting rod side, and the opposite side of connecting rod is flexibly connected the axle in swing arm, installs at the position, top of swing arm the motor that screw propeller is housed.This swinging gear is installed neatly according to the quantity of Multi-axis aircraft configuration horn, can two to, three to, four to, five successively swinging gear is installed over the ground.
Operating electrical machines 30 works, and when bevel gear drives two (or the worm gear in multiple swinging gear) worm gears to make reciprocating rotary, makes it horn and swings up and down.
The Multi-axis aircraft 100 that the utility model has a horn oscillating function also can install the swinging gear 50 configuring motor 2-22 one to one makes horn 4 swing, the horn so just making the Multi-axis aircraft with horn oscillating function install no matter paired quantity how, installs this swinging gear all neatly.Operating electrical machines 2-22 works, and makes horn one or more do wobbling action, and the wobbling action of horn is simultaneously or intersects or swing successively.Which adds the interest of various change of the in-flight flare maneuver of Multi-axis aircraft.Also the manipulation ability of people has been tempered.The Multi-axis aircraft with horn oscillating function does these wobbling actions, is that the swinging gear of configuration bevel gear of the present utility model is not accomplished yet.That swinging gear that existing remote control Multi-axis aircraft is installed simultaneously is not accomplished yet.The Multi-axis aircraft that the utility model has horn oscillating function can be selected to install swinging gear according to the needs of horn wobbling action.(some the prior art features in the utility model are not shown).
Claims (2)
1. there is the Multi-axis aircraft of horn oscillating function, comprise Multi-axis aircraft (100), in described Multi-axis aircraft (100), swinging gear (50) is installed, it is characterized in that: the support (1) in described swinging gear (50) comprises, bottom plate (1-1, 1-2), first axle bed (1-3), second axle bed (1-4), 3rd axle bed (1-5), 4th axle bed (1-6), Worm wheel transmission mechanism (2), Worm wheel transmission mechanism (2) is provided with in described support (1), described first axle bed axle bed (1-3), the first through hole (1-31) set by second axle bed (1-4), second through hole (1-41) connects the bearing set by axle (2-11) of the worm gear (2-1) of Worm wheel transmission mechanism (2), described worm gear (2-1) engages worm (2-2), bearing set by described worm screw (2-2) side connects the 3rd axle bed (1-5), third through-hole through hole (1-51) set by 4th axle bed (1-6), fourth hole (1-61), described worm screw (2-2) is at the 4th axle bed (1-6) outer tip end position Connectable umbrella gear (2-22) or motor (2-22), described worm gear (2-1) side is provided with support arm (3), described support arm (3) connects horn (4) side, described horn (4) opposite side connects attaching parts (5), axle (6-1) set in swing arm (6) set by described attaching parts (5) is flexibly connected the side of connecting rod (7), the opposite side of described connecting rod (7) is flexibly connected axle (8-1) set in Connection Block (8), on described, bottom plate (1-1), (1-2) side is provided with open slot (1-0), the opposite side of described bottom plate (1-2) is provided with at least two screws (1-20).
2. the Multi-axis aircraft with horn oscillating function according to claim 1, it is characterized in that: described bevel gear (2-22) meshing bevel gear (9), the bearing set by axle (9-1) side of described bevel gear (9) is connected and fixed the fifth hole (10-0) set by plate (10) center, described adapter plate (10) is provided with permanent seat (11), the 6th through hole (11-0) set by described permanent seat (11) connects the bearing set by described axle (9-1) opposite side, this side of described axle (9-1) connects motor (30), the shaped position of the quantity that the edge of described adapter plate (10) is installed according to swinging gear (50) and installation is provided with the 7th through hole (10-1) of the screw (1-20) set by corresponding bottom plate (1-2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520438336.6U CN204916173U (en) | 2015-06-19 | 2015-06-19 | Multiaxis aircraft with horn swing function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520438336.6U CN204916173U (en) | 2015-06-19 | 2015-06-19 | Multiaxis aircraft with horn swing function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204916173U true CN204916173U (en) | 2015-12-30 |
Family
ID=54965327
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520438336.6U Expired - Fee Related CN204916173U (en) | 2015-06-19 | 2015-06-19 | Multiaxis aircraft with horn swing function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204916173U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109592024A (en) * | 2016-07-05 | 2019-04-09 | 金福珍 | A kind of Intelligent unattended machine |
-
2015
- 2015-06-19 CN CN201520438336.6U patent/CN204916173U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109592024A (en) * | 2016-07-05 | 2019-04-09 | 金福珍 | A kind of Intelligent unattended machine |
| CN109592024B (en) * | 2016-07-05 | 2022-02-11 | 武汉慧农无人机科技有限公司 | Intelligent unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151230 Termination date: 20170619 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |