CN203235257U - Propeller vector control structure of remote-control model plane - Google Patents
Propeller vector control structure of remote-control model plane Download PDFInfo
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- CN203235257U CN203235257U CN 201320216820 CN201320216820U CN203235257U CN 203235257 U CN203235257 U CN 203235257U CN 201320216820 CN201320216820 CN 201320216820 CN 201320216820 U CN201320216820 U CN 201320216820U CN 203235257 U CN203235257 U CN 203235257U
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Abstract
The utility model discloses a propeller vector control structure of a remote-control model plane. The propeller vector control structure of the remote-control model plane comprises a vector mechanism fixing part, a vector motion control part and a power execution part, wherein the vector mechanism fixing part comprises a main engine body, a fixing pull rod, a hexagonal fixing rod, a fixing round bar, a steering engine fixing base and a fixing hanging ring, the vector motion control part comprises a steering engine, a steering engine pull rod, a control outer disc, a cross inner disc, a ball screw, a metal lining and a fixing screw, and the power execution part is composed of a motor, a metal adapter, a Kimi screw, a propeller, a gasket and a fixing screw. The propeller vector control structure of the remote-control model plane has the advantages that the body is high in strength, the structure is simple, the control accuracy is high, and operation is flexible, easy and convenient.
Description
Technical field
The utility model relates to a kind of screw vector controlled structure of remote-controlled model aircraft.
Background technology
In common remote-controlled model aircraft, its structure is that the screw position immobilizes mostly, afterbody has a pair of wing flap that can swing up and down and the empennage that can swing, and the change of implementation model aircraft flight direction then is the flow direction that changes air-flow by the wing flap of steering wheel pulling afterbody and empennage.This structure is very high to structural strength, the manufacture process requirement of fuselage, head turn to flexibility ratio relatively poor.
Summary of the invention
The technical problems to be solved in the utility model provides a kind of screw vector controlled structure that reduces the fuselage manufacturing cost, improves the remote-controlled model aircraft of steering flexibility.
For solving the problems of the technologies described above, the utility model adopts following technical scheme: a kind of screw vector controlled structure of remote-controlled model aircraft, comprise vector mechanism standing part, vector motion control section and power operating part, described vector mechanism standing part refers to the fuselage, steady brace, hexagonal fixed bar of the model of an airplane, fixedly round bar, steering wheel holder and fixing suspension ring; Described vector motion control section comprises steering wheel, steering wheel pull bar, control outer disk, cross inner disc, two bulb screws, metal lining and fixed screws; Described power operating part is made of motor, metal adapter, base rice screw, screw, pad and fixed screw.Wherein, fixedly round bar, hexagonal fixed bar, the first steering wheel holder and the second steering wheel holder are assemblied in respectively with it the main frame, the first steering wheel is assemblied on the first steering wheel holder, and the second steering wheel is assemblied on the second steering wheel holder, and adapter is fixedly connected with the main shaft of motor by base rice screw.
Main frame described in the utility model is provided with fixedly fixedly square hole and round bar fixing hole of square hole, the second steering wheel of hexagonal bar fixing hole, the first steering wheel with it, the two ends of steady brace have hexagon ring and pull bar circular hole, fixedly suspension ring are provided with suspension ring circular hole and semicircle orifice, the first steering wheel holder is provided with the first steering wheel holddown groove, the first steering wheel fixed screw holes and the first steering wheel holder pole, and the second steering wheel holder is provided with the second steering wheel holddown groove, the second steering wheel fixed screw holes and the second steering wheel holder pole; Described the first steering wheel is provided with the first bulb, the second steering wheel is provided with the second bulb, the first steering wheel pull bar is respectively equipped with the first bulb hole and the second bulb hole, the second steering wheel pull bar is respectively equipped with the 3rd bulb hole and the 4th bulb hole, control outer disk long axis direction has the outer disk screw hole, and short-axis direction has the outer disk circular hole, and the oblique angle direction has the oblique angle screw hole, cross inner disc long axis direction has the major axis screw hole, and short-axis direction has minor axis screw hole and positive inner disc circular hole; Described adapter side has base rice screw hole and screw hole, and motor bottom is provided with the motor screw hole.
Four the first steering wheels that four the first steering wheel holder poles of the first steering wheel holder described in the utility model are assemblied in the main frame body are fixedly in the square hole, four the second steering wheels that four the second steering wheel holder poles of the second steering wheel holder are assemblied in the main frame body are fixedly in the square hole, the hexagonal fixed bar is assemblied in two hexagonal bar fixing holes of main frame body, fixedly round bar is assemblied in two round bar fixing holes of main frame body, the hexagon ring of steady brace rear end is assemblied on the hexagonal fixed bar, fixedly the top suspension ring circular hole of suspension ring is assemblied in fixedly on the round bar, the below semicircle orifice is assemblied on the steady brace, and the steady brace position is fixed.
The first steering wheel described in the utility model is assemblied in the first steering wheel holddown groove on the first steering wheel holder, and lock in the first steering wheel fixed screw holes with two lock screws, the second steering wheel is assemblied in the second steering wheel holddown groove on the second steering wheel holder, and locks in the second steering wheel fixed screw holes with two lock screws.
Be fitted into metal lining in the outer disk circular hole of control outer disk described in the utility model, the long axis direction of cross inner disc is coaxial with the short-axis direction of control outer disk, the endoporus that fixed screw passes metal lining is locked the major axis screw hole of the long axis direction of cross inner disc, the first bulb screw is locked in the oblique angle screw hole at control outer disk oblique angle, the second bulb screw is locked in the minor axis screw hole of short-axis direction of cross inner disc, and fixed screw passes the pull bar circular hole of steady brace front end and locks in the outer disk screw hole of control outer disk long axis direction.
The first bulb hole of the first steering wheel pull bar one end described in the utility model is assemblied on the first bulb of the first steering wheel, the second bulb hole of the other end is assemblied on the bulb of the second bulb screw, the 3rd bulb hole of the second steering wheel pull bar one end is assemblied on the second bulb of the second steering wheel, and the 4th bulb hole of the other end is assemblied on the bulb of the first bulb screw.
Adapter described in the utility model is assemblied on the main shaft of motor, locking base rice screw hole with base rice screw fixes, screw is assemblied on the adapter, lock with screw and pad in the screw hole of adapter, fixed screw is locked in the motor screw hole of motor bottom by the inner disc circular hole on the cross inner disc.
The utility model compared with prior art has that airframe structure is simple, aircraft rotates flexibly, high, a recreational advantage such as strong of control accuracy.
Description of drawings
Fig. 1 is three-dimensional assembling schematic diagram of the present utility model.
Fig. 2 is internal structure assembling schematic diagram of the present utility model.
Fig. 3 is perspective exploded view of the present utility model.
Fig. 4 is control outer disk structural representation of the present utility model.
Fig. 5 is cross inner disc structural representation of the present utility model.
Fig. 6 is the assembling schematic diagram of the utility model control outer disk and cross inner disc.
Fig. 7 is adapter structure schematic diagram of the present utility model.
Fig. 8 is motor bottom structural representation of the present utility model.
The specific embodiment
The utility model will be further described below in conjunction with accompanying drawing.
To shown in Figure 8, the screw vector controlled structure of the utility model remote-controlled model aircraft comprises main frame body 1 such as Fig. 3, steady brace 2, fixedly suspension ring 3, fixedly round bar 4, hexagonal fixed bar 5, fixed screw 6, the first steering wheel holder 7, the first steering wheel 8, lock screw 9, the first steering wheel pull bar 10, the second steering wheel holder 11, the second steering wheel 12, the second steering wheel pull bar 13, control outer disk 14, metal lining 15, the first bulb screw 16, cross inner disc 17, the second bulb screw 18, motor 19, base rice screw 20, adapter 21, screw 22, pad 23 and screw 24.Wherein: main frame body 1 is provided with fixedly fixedly square hole 27, round bar fixing hole 28 of square hole 26, the second steering wheel of hexagonal bar fixing hole 25, the first steering wheel; Steady brace 2 is provided with hexagon ring 29 and pull bar circular hole 32; Fixedly suspension ring 3 are provided with suspension ring circular hole 30 and semicircle orifice 31; The first steering wheel holder 7 is provided with the first steering wheel holddown groove 33, the first steering wheel fixed screw holes 34 and the first steering wheel holder pole 35; The first steering wheel 8 is provided with the first bulb 36, the second steering wheel 12 is provided with the second bulb 42, the first steering wheel pull bar 10 is respectively equipped with the first bulb hole 37 and the second bulb hole 38, the second steering wheel pull bar 13 is respectively equipped with the 3rd bulb hole 43 and the 4th bulb hole 44, the second steering wheel holders 11 are provided with the second steering wheel holddown groove 39, the second steering wheel fixed screw holes 40 and the second steering wheel holder pole 41; Control outer disk 14 long axis direction A1 are provided with outer disk screw hole 45, and short-axis direction A2 is provided with outer disk circular hole 46, and the oblique angle direction is provided with oblique angle screw hole 47; Cross inner disc 17 long axis direction B1 are provided with major axis screw hole 50, and short-axis direction B2 is provided with minor axis screw hole 49, and the front is provided with inner disc circular hole 48; Motor 19 bottoms are provided with motor screw hole 53; The adapter 21 side faces of cylinder are provided with base rice screw hole 51, and end face is provided with screw hole 52.
Fixedly round bar 4 is fitted into the round bar fixing hole 28 of main frame body 1, hexagonal fixed bar 5 is fitted into the hexagonal bar fixing hole 25 of main frame body 1, the first steering wheel that the first steering wheel holder 7 is fitted into main frame body 1 by the first steering wheel holder pole 35 is square hole 26 fixedly, the second steering wheel that the second steering wheel holder 11 is fitted into main frame body 1 by the second steering wheel holder pole 41 is square hole 27 fixedly, the hexagon ring 29 of steady brace 2 back is assemblied on the hexagonal fixed bar 5, fixedly the suspension ring circular hole 30 of suspension ring 3 tops is assemblied in fixedly on the round bar 4, and the semicircle orifice 31 of below is assemblied on the steady brace 2.
The first steering wheel 8 is assemblied in the first steering wheel holddown groove 33 on the first steering wheel holder 7, and fix with the first steering wheel fixed screw holes 34 that lock screw 9 is locked the first steering wheel holder 7, the second steering wheel 12 is assemblied in the second steering wheel holddown groove 39 on the second steering wheel holder 11, and fixes with the second steering wheel fixed screw holes 40 that lock screw 9 is locked the second steering wheel holder 11.
The first bulb hole 37 of the first steering wheel pull bar 10 is assemblied on the first bulb 36 of the first steering wheel 8, the second bulb hole 38 is assemblied on the second bulb screw 18, control cross inner disc 17 is around short-axis direction A2 left-right rotation, the 3rd bulb hole 43 of the second steering wheel pull bar 13 is assemblied on the second bulb 42 of the second steering wheel 12, the 4th bulb hole 44 is assemblied on the first bulb screw 16, and pulling control outer disk 14 is rotated up and down around long axis direction A1.
By the diagram and above-mentioned explanation as can be known, the operation principle of the screw vector controlled structure of remote-controlled model aircraft is in the utility model: when needs change the heading of the model of an airplane, send the adjustment signal for respectively the first steering wheel 8 and the second steering wheel 12 by emitter, the first steering wheel 8 is by the second bulb screw 18 on the first steering wheel pull bar 10 push-and-pull cross inner discs 17, make cross inner disc 17 around A2/B1 direction of principal axis left-right rotation, drive motor 19 and screw 22 swing, implementation model aircraft left/right rotation to; The second steering wheel 12 makes control outer disk 14 rotate up and down around the A2/B1 direction of principal axis by the first bulb screw 16 on the second steering wheel pull bar 13 push-and-pulls control outer disk 14, and drive motor 19 and screw 22 swing up and down, the rising of implementation model aircraft and decline.The first steering wheel 8 control model of an airplane left/right rotations to, the lifting of the second steering wheel 12 control model of an airplanes, two steering wheel actings in conjunction, control outer disk 14 and cross inner disc 17 rotate synchronously, can realize that sensitivity is higher to the vector controlled of screw 22 action directions, the operability of aircraft is stronger.
This shows that the application of the screw vector controlled structure of the remote-controlled model aircraft in the utility model had both increased the fuselage intensity of the model of an airplane, reduced the manufacturing cost of fuselage, realized again the target that the model of an airplane can turn to flexibly, and control accuracy is higher, recreational stronger.
Claims (7)
1. the screw vector controlled structure of a remote-controlled model aircraft, comprise vector mechanism standing part, vector motion control section and power operating part, it is characterized in that: described vector mechanism standing part by main frame body (1), steady brace (2), fixedly suspension ring (3), fixedly round bar (4), hexagonal fixed bar (5), the first steering wheel holder (7) and the second steering wheel holder (11) form; Described vector motion control section is comprised of the first steering wheel (8), the first steering wheel pull bar (10), the second steering wheel (12), the second steering wheel pull bar (13), the first bulb screw (16), the second bulb screw (18), control outer disk (14), cross inner disc (17), metal lining (15) and fixed screw (6); Described power operating part comprises motor (19), base rice screw (20), adapter (21), screw (22), pad (23) and screw (24); Described fixedly round bar (4), hexagonal fixed bar (5), the first steering wheel holder (7) and the second steering wheel holder (11) are assemblied in respectively on the main frame body (1), the first steering wheel (8) is assemblied on the first steering wheel holder (7), the second steering wheel (12) is assemblied on the second steering wheel holder (11), and adapter (21) is fixedly connected with the main shaft of motor (19) by base rice screw (20).
2. the screw vector controlled structure of remote-controlled model aircraft according to claim 1, it is characterized in that: be provided with hexagonal bar fixing hole (25) on the described main frame body (1), the first steering wheel is square hole (26) fixedly, the second steering wheel is square hole (27) and round bar fixing hole (28) fixedly, the two ends of steady brace (2) have hexagon ring (29) and pull bar circular hole (32), fixedly suspension ring (3) are provided with suspension ring circular hole (30) and semicircle orifice (31), the first steering wheel holder (7) is provided with the first steering wheel holddown groove (33), the first steering wheel fixed screw holes (34) and the first steering wheel holder pole (35), the second steering wheel holder (11) is provided with the second steering wheel holddown groove (39), the second steering wheel fixed screw holes (40) and the second steering wheel holder pole (41); Described the first steering wheel (8) is provided with the first bulb (36), the second steering wheel (12) is provided with the second bulb (42), the first steering wheel pull bar (10) is respectively equipped with the first bulb hole (37) and the second bulb hole (38), the second steering wheel pull bar (13) is respectively equipped with the 3rd bulb hole (43) and the 4th bulb hole (44), control outer disk (14) long axis direction (A1) has outer disk screw hole (45), short-axis direction (A2) has outer disk circular hole (46), the oblique angle direction has oblique angle screw hole (47), cross inner disc (17) long axis direction (B1) has major axis screw hole (50), and short-axis direction (B2) has minor axis screw hole (49) and positive inner disc circular hole (48); Described adapter (21) side has base rice screw hole (51) and screw hole (52), and motor (19) bottom is provided with motor screw hole (53).
3. the screw vector controlled structure of remote-controlled model aircraft according to claim 2, it is characterized in that: four the first steering wheels that four the first steering wheel holder poles (35) of described the first steering wheel holder (7) are assemblied in main frame body (1) are fixedly in the square hole (26), four the second steering wheels that four the second steering wheel holder poles (41) of the second steering wheel holder (11) are assemblied in main frame body (1) are fixedly in the square hole (27), hexagonal fixed bar (5) is assemblied in two hexagonal bar fixing holes (25) of main frame body (1), fixedly round bar (4) is assemblied in two round bar fixing holes (28) of main frame body (1), the hexagon ring (29) of steady brace (2) rear end is assemblied on the hexagonal fixed bar (5), fixedly the top suspension ring circular hole (30) of suspension ring (3) is assemblied in fixedly on the round bar (4), below semicircle orifice (31) is assemblied on the steady brace (2), and steady brace (2) position is fixed.
4. the screw vector controlled structure of remote-controlled model aircraft according to claim 3, it is characterized in that: described the first steering wheel (8) is assemblied in the first steering wheel holddown groove (33) on the first steering wheel holder (7), and lock in the first steering wheel fixed screw holes (34) with two lock screws (9), the second steering wheel (12) is assemblied in the second steering wheel holddown groove (39) on the second steering wheel holder (11), and locks in the second steering wheel fixed screw holes (40) with two lock screws (9).
5. the screw vector controlled structure of remote-controlled model aircraft according to claim 4, it is characterized in that: be fitted into metal lining (15) in the outer disk circular hole (46) of described control outer disk (14), the long axis direction (B1) of cross inner disc (17) is coaxial with the short-axis direction (A2) of control outer disk (14), the endoporus that fixed screw (6) passes metal lining (15) is locked the major axis screw hole (50) of the long axis direction (B1) of cross inner disc (17), the first bulb screw (16) is locked in the oblique angle screw hole (47) at control outer disk (14) oblique angle, the second bulb screw (18) is locked in the minor axis screw hole (49) of short-axis direction (B2) of cross inner disc (17), and fixed screw (6) passes the pull bar circular hole (32) of steady brace (2) front end and locks in the outer disk screw hole (45) of control outer disk (14) long axis direction (A1).
6. the screw vector controlled structure of remote-controlled model aircraft according to claim 5, it is characterized in that: the first bulb hole (37) of described the first steering wheel pull bar (10) is assemblied on first bulb (36) of the first steering wheel (8), the second bulb hole (38) is assemblied on the bulb of the second bulb screw (18), the 3rd bulb hole (43) of the second steering wheel pull bar (13) is assemblied on second bulb (42) of the second steering wheel (12), and the 4th bulb hole (44) is assemblied on the bulb of the first bulb screw (16).
7. the screw vector controlled structure of remote-controlled model aircraft according to claim 6, it is characterized in that: described adapter (21) is assemblied on the main shaft of motor (19), it is fixing to lock base rice screw hole (51) with base rice screw (20), screw (22) is assemblied on the adapter (21), lock with screw (24) and pad (23) in the screw hole (52) of adapter (21), fixed screw (6) is locked in the motor screw hole (53) of motor (19) bottom by the inner disc circular hole (48) on the cross inner disc (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320216820 CN203235257U (en) | 2013-04-26 | 2013-04-26 | Propeller vector control structure of remote-control model plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320216820 CN203235257U (en) | 2013-04-26 | 2013-04-26 | Propeller vector control structure of remote-control model plane |
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| CN203235257U true CN203235257U (en) | 2013-10-16 |
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| CN 201320216820 Expired - Fee Related CN203235257U (en) | 2013-04-26 | 2013-04-26 | Propeller vector control structure of remote-control model plane |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104554706A (en) * | 2014-11-24 | 2015-04-29 | 北京航空航天大学 | Novel control method for high aspect-ratio flying wing solar-powered airplane |
| CN106927039A (en) * | 2016-12-09 | 2017-07-07 | 河北工业大学 | Vector puller system and VUAV vector tensile strength control method |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN107628231A (en) * | 2017-10-24 | 2018-01-26 | 红河学院 | The foldable unmanned plane of water surface landing vector fixed-wing |
| CN114949878A (en) * | 2022-05-24 | 2022-08-30 | 张晓勇 | Vector kite with control function |
-
2013
- 2013-04-26 CN CN 201320216820 patent/CN203235257U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104554706A (en) * | 2014-11-24 | 2015-04-29 | 北京航空航天大学 | Novel control method for high aspect-ratio flying wing solar-powered airplane |
| CN106927039A (en) * | 2016-12-09 | 2017-07-07 | 河北工业大学 | Vector puller system and VUAV vector tensile strength control method |
| CN107364572A (en) * | 2017-08-11 | 2017-11-21 | 红河学院 | Fixed-wing vector unmanned plane |
| CN107364572B (en) * | 2017-08-11 | 2024-01-30 | 昆明学院 | Fixed wing vector unmanned plane |
| CN107628231A (en) * | 2017-10-24 | 2018-01-26 | 红河学院 | The foldable unmanned plane of water surface landing vector fixed-wing |
| CN114949878A (en) * | 2022-05-24 | 2022-08-30 | 张晓勇 | Vector kite with control function |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131016 Termination date: 20200426 |