CN203663450U - Propeller vector control structure of remote-control model plane - Google Patents

Propeller vector control structure of remote-control model plane Download PDF

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Publication number
CN203663450U
CN203663450U CN201320799775.0U CN201320799775U CN203663450U CN 203663450 U CN203663450 U CN 203663450U CN 201320799775 U CN201320799775 U CN 201320799775U CN 203663450 U CN203663450 U CN 203663450U
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CN
China
Prior art keywords
screw
steering wheel
hole
holder
fixing seat
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201320799775.0U
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Chinese (zh)
Inventor
沈安平
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
SHENZHEN SHENSHI TONGCHUANG SPACEFLIGHT MODEL CO Ltd
Original Assignee
SHENZHEN SHENSHI TONGCHUANG SPACEFLIGHT MODEL CO Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by SHENZHEN SHENSHI TONGCHUANG SPACEFLIGHT MODEL CO Ltd filed Critical SHENZHEN SHENSHI TONGCHUANG SPACEFLIGHT MODEL CO Ltd
Priority to CN201320799775.0U priority Critical patent/CN203663450U/en
Application granted granted Critical
Publication of CN203663450U publication Critical patent/CN203663450U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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 comprises a vector mechanism fixing part, a vector motion control part and a power executing part. The vector mechanism fixing part comprises a main plane body, a tail pipe, a steering engine fixing seat, a vertical wing fixing seat and a vertical wing. The vector motion control part comprises a steering engine, a steering engine pull rod, a first ball head screw, a steering engine oscillating arm, a motor rotation fixing seat, a ball bearing, a motor fixing seat and a second ball head screw. The power executing part comprises a motor, a metal clamp head, a first propeller fixing seat, a propeller and a second propeller fixing seat. The steering engine is arranged on the steering engine fixing seat and connected with the motor fixing seat through the steering engine pull rod, and the motor is arranged on the motor fixing seat. The propeller vector control structure of the remote-control model plane has the advantages of being high in plane body strength, simple in structure, high in control precision, flexible, easy and convenient to operate and the like.

Description

The screw vector controlled structure of remote-controlled model aircraft
Technical field
The utility model relates to a kind of screw vector controlled structure of remote-controlled model aircraft.
Background technology
In present multi-rotor aerocraft, its structure is that screw position immobilizes mostly, completes the stable of aircraft by paired positive and negative rotor, to aircraft turn tail and End-Management completes by the speed discrepancy of positive and negative rotor.This structure control is slower, and go to action slowly and control hysteresis, differentiate not obvious, is easy to cause locality misjudgment by front and back.Meanwhile, because rotor must become logarithm that cost is increased.
Summary of the invention
The technical problems to be solved in the utility model is to provide a kind of screw vector controlled structure that reduces 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 comprises main frame body, tail pipe, steering wheel holder, vertical tail, holder and vertical tail; Described vector motion control section comprises steering wheel, steering wheel pull bar, the first bulb screw, steering wheel swing arm, electric machine rotation holder, ball bearing, motor fixing seat and the second bulb screw; Described power operating part comprises motor, metal collet, screw the first holder, screw and screw the second holder; Described steering wheel is located on steering wheel holder, and steering wheel connects motor fixing seat by steering wheel pull bar, and motor is located in motor fixing seat.
Steering wheel holder described in the utility model is inserted on tail pipe, vertical tail, holder is inserted on tail pipe, vertical tail, is assemblied on vertical tail, holder, steering wheel is assemblied on steering wheel holder, steering wheel swing arm is assemblied on steering wheel, the first bulb screw is locked in steering wheel swing arm, the two ends of steering wheel pull bar snap into respectively the first bulb screw and lock on the second bulb screw in motor fixing seat, ball bearing is bumped in electric machine rotation holder, electric machine rotation holder is inserted on tail pipe, motor fixing seat is assembled on electric machine rotation holder, motor is assembled in motor fixing seat, metal collet, screw the first holder, screw, screw the second holder is assemblied on motor shaft.
Steering wheel holder described in the utility model is provided with tail pipe fixing hole, the first screw hole and steering wheel fixed screw holes, steering wheel is provided with the first screw through-hole and swing arm screw hole, steering wheel swing arm is provided with the second screw through-hole and the second screw hole, steering wheel pull bar is provided with bulb hole, electric machine rotation holder is provided with ball bearing holddown groove and the 4th screw hole, ball bearing is provided with bearing bore diameter and bearing outside diameter, vertical tail, holder is provided with the 3rd screw hole and tail pipe fixing hole, vertical tail, is provided with the 3rd screw through-hole, motor fixing seat is provided with bulb screw hole, motor fixed screw through hole and the 4th screw through-hole, motor is provided with main shaft and the 5th screw hole, metal collet is provided with thread and circular hole, screw the first holder is provided with band oblique angle through hole, screw is provided with through hole, screw the second holder is provided with tooth hole.
Steering wheel holder described in the utility model uses steering wheel holder screw to lock in the first screw hole to be nested on tail pipe, vertical tail, holder uses vertical tail, fixed screw to be locked in the 3rd screw hole to be nested on tail pipe through the 3rd screw through-hole, steering wheel uses steering wheel fixed screw to be locked in steering wheel fixed screw holes to be assemblied on steering wheel holder through the first screw through-hole, steering wheel swing arm is used steering wheel swing arm fixed screw to be locked in swing arm screw hole to be assemblied on steering wheel through the second screw through-hole, the first bulb screw is locked on the second screw hole of steering wheel swing arm, steering wheel pull bar snaps on the first bulb screw and the second bulb screw, ball bearing is bumped in the ball bearing holddown groove of electric machine rotation holder, the bearing bore diameter of electric machine rotation holder is nested on tail pipe, motor fixing seat is used motor fixing seat screw to be locked in the 4th screw hole to be assembled on electric machine rotation holder through the 4th screw through-hole, motor uses motor fixing screw to be locked in the 5th screw hole to be assembled in motor fixing seat through motor fixed screw through hole, metal collet is nested on main shaft, the through hole with oblique angle through hole and screw of screw the first holder is through metal collet, the tooth hole that re-uses screw the second holder screws in thread and fixes.
The utility model compared with prior art, has the advantages such as fuselage intensity is high, simple in structure, control accuracy is high, flexible operation is easy.
Accompanying drawing explanation
Fig. 1 is schematic perspective view of the present utility model.
Fig. 2 is sectional perspective schematic diagram of the present utility model.
Fig. 3 is one of perspective exploded view of the present utility model.
Fig. 4 is two of perspective exploded view of the present utility model.
Fig. 5 is power operating part decomposing schematic representation of the present utility model.
Fig. 6 is control principle schematic diagram of the present utility model.
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
Below in conjunction with accompanying drawing, the utility model will be further described.
As shown in Figures 3 to 6, the screw vector controlled structure of the utility model remote-controlled model aircraft, comprise vector mechanism standing part, vector motion control section and power operating part, vector mechanism standing part comprises main frame body 1, tail pipe 2, steering wheel holder 3, steering wheel holder screw 4, vertical tail, holder 5, vertical tail, 6 and vertical tail, fixed screw 7; Vector motion control section comprises steering wheel 8, steering wheel fixed screw 9, steering wheel pull bar 10, steering wheel swing arm fixed screw 11, the first bulb screw 12, steering wheel swing arm 13, electric machine rotation holder 14, ball bearing 15, motor fixing screw 16, motor fixing seat 17, motor fixing seat screw 18 and the second bulb screw 19; Power operating part comprises motor 20, metal collet 21, screw the first holder 22, screw 23, screw the second holder 24.Wherein: steering wheel holder 3 is provided with tail pipe fixing hole 25, the first screw hole 26 and steering wheel fixed screw holes 27, steering wheel 8 is provided with the first screw through-hole 28 and swing arm screw hole 29, steering wheel swing arm 13 is provided with the second screw through-hole 30 and the second screw hole 31, steering wheel pull bar 10 is provided with bulb hole 32, electric machine rotation holder 14 is provided with ball bearing holddown groove 35 and the 4th screw hole 38, ball bearing 15 is provided with bearing bore diameter 36 and bearing outside diameter 37, vertical tail, holder 5 is provided with the 3rd screw hole 33 and tail pipe fixing hole 34, vertical tail, 6 is provided with the 3rd screw through-hole 40, motor fixing seat 17 is provided with bulb screw hole 39, motor fixed screw through hole 41 and the 4th screw through-hole 42, motor 20 is provided with main shaft 43 and the 5th screw hole 49, metal collet 21 is provided with thread 44 and circular hole 48, screw the first holder 22 is provided with band oblique angle through hole 45, screw 23 is provided with through hole 46, screw the second holder 24 is provided with tooth hole 47, the central axis of steering wheel swing arm 13 is A1, the central axis of electric machine rotation holder 14 is A2.
When the utility model assembling, holder 3 is nested on tail pipe 2, vertical tail, holder 5 is nested on tail pipe 2, vertical tail, 6 is assemblied on vertical tail, holder 5, steering wheel 8 is assemblied on steering wheel holder 3, steering wheel swing arm 13 is assemblied on steering wheel 8, the first bulb screw 12 is locked in steering wheel swing arm 13, the two ends of steering wheel pull bar 10 snap into respectively the first bulb screw 12 and lock on the second bulb screw 19 in motor fixing seat 17, ball bearing 15 is bumped in electric machine rotation holder 14, electric machine rotation holder 14 is nested on tail pipe 2, motor fixing seat 17 is assembled on electric machine rotation holder 14, motor 20 is assembled in motor fixing seat 17, metal collet 21, screw the first holder 22, screw 23, screw the second holder 24 is assemblied on motor 20 axles.
Concrete assembling mode is: steering wheel holder 3 uses steering wheel holder screw 4 to lock in the first screw hole 26 to be nested on tail pipe 2, vertical tail, holder 5 uses vertical tail, fixed screw 7 to be locked in the 3rd screw hole 33 to be nested on tail pipe 2 through the 3rd screw through-hole 40, steering wheel 8 uses steering wheel fixed screw 9 to be locked in steering wheel fixed screw holes 27 to be assemblied on steering wheel holder 3 through the first screw through-hole 28, steering wheel swing arm 13 is used steering wheel swing arm fixed screw 11 to be locked in swing arm screw hole 29 to be assemblied on steering wheel 8 through the second screw through-hole 30, the first bulb screw 12 is locked on the second screw hole 31 of steering wheel swing arm 13, steering wheel pull bar 10 snaps on the first bulb screw 12 and the second bulb screw 19, ball bearing 15 is bumped in the ball bearing holddown groove 35 of electric machine rotation holder 14, the bearing bore diameter 36 of electric machine rotation holder 14 is nested on tail pipe 2, motor fixing seat 17 is used motor fixing seat screw 18 to be locked in the 4th screw hole 38 to be assembled to electric machine rotation holder 14 through the 4th screw through-hole 42, motor 20 uses motor fixing screw 16 to be locked on the 5th screw hole 49 to be assembled in motor fixing seat 17 through motor fixed screw through hole 41, metal collet 21 is nested on main shaft 43, the through hole with oblique angle through hole 45 and screw 23 46 of screw the first holder 22 is through metal collet 21, the tooth hole 47 that re-uses screw the second holder 24 is screwed into thread 44 and fixes.
From illustrating and above-mentioned explanation, in the utility model, the operation principle of the screw vector controlled structure of remote-controlled model aircraft is: in the time need to changing the heading of the model of an airplane, send adjustment signal by emitter to steering wheel 8, make steering wheel swing arm 13 around its A1 direction of principal axis rotation, again by the second bulb screw 19 in steering wheel pull bar 10 push-and-pull motor fixing seat 17, make motor fixing seat 17 around its A2 direction of principal axis left rotation and right rotation, drive motor 20 and screw 23 left rotation and right rotation, the rotation of implementation model aircraft, realize the vector controlled to screw 23 action directions, sensitivity is higher, the operability of aircraft is stronger.
As can be seen here, 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, reduce 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 (4)

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 comprises main frame body (1), tail pipe (2), steering wheel holder (3), vertical tail, holder (5) and vertical tail, (6); Described vector motion control section comprises steering wheel (8), steering wheel pull bar (10), the first bulb screw (12), steering wheel swing arm (13), electric machine rotation holder (14), ball bearing (15), motor fixing seat (17) and the second bulb screw (19); Described power operating part comprises motor (20), metal collet (21), screw the first holder (22), screw (23) and screw the second holder (24); It is upper that described steering wheel (8) is located at steering wheel holder (3), and steering wheel (8) connects motor fixing seat (17) by steering wheel pull bar (10), and motor (20) is located in motor fixing seat (17).
2. the screw vector controlled structure of remote-controlled model aircraft according to claim 1, it is characterized in that: described steering wheel holder (3) is nested on tail pipe (2), vertical tail, holder (5) is nested on tail pipe (2), vertical tail, (6) is assemblied on vertical tail, holder (5), steering wheel (8) is assemblied on steering wheel holder (3), steering wheel swing arm (13) is assemblied on steering wheel (8), the first bulb screw (12) is locked in steering wheel swing arm (13), the two ends of steering wheel pull bar (10) snap into respectively the first bulb screw (12) and lock on the second bulb screw (19) in motor fixing seat (17), ball bearing (15) is bumped in electric machine rotation holder (14), electric machine rotation holder (14) is nested on tail pipe (2), motor fixing seat (17) is assembled on electric machine rotation holder (14), motor (20) is assembled in motor fixing seat (17), metal collet (21), screw the first holder (22), screw (23), screw the second holder (24) is assemblied on motor (20) axle.
3. the screw vector controlled structure of remote-controlled model aircraft according to claim 2, it is characterized in that: described steering wheel holder (3) is provided with tail pipe fixing hole (25), the first screw hole (26) and steering wheel fixed screw holes (27), steering wheel (8) is provided with the first screw through-hole (28) and swing arm screw hole (29), steering wheel swing arm (13) is provided with the second screw through-hole (30) and the second screw hole (31), steering wheel pull bar (10) is provided with bulb hole (32), electric machine rotation holder (14) is provided with ball bearing holddown groove (35) and the 4th screw hole (38), ball bearing (15) is provided with bearing bore diameter (36) and bearing outside diameter (37), vertical tail, holder (5) is provided with the 3rd screw hole (33) and tail pipe fixing hole (34), vertical tail, (6) is provided with the 3rd screw through-hole (40), motor fixing seat (17) is provided with bulb screw hole (39), motor fixed screw through hole (41) and the 4th screw through-hole (42), motor (20) is provided with main shaft (43) and the 5th screw hole (49), metal collet (21) is provided with thread (44) and circular hole (48), screw the first holder (22) is provided with band oblique angle through hole (45), screw (23) is provided with through hole (46), screw the second holder (24) is provided with tooth hole (47).
4. the screw vector controlled structure of remote-controlled model aircraft according to claim 3, it is characterized in that: described steering wheel holder (3) uses steering wheel holder screw (4) to lock in the first screw hole (26) to be nested on tail pipe (2), vertical tail, holder (5) uses vertical tail, fixed screw (7) to be locked in the 3rd screw hole (33) to be nested on tail pipe (2) through the 3rd screw through-hole (40), steering wheel (8) uses steering wheel fixed screw (9) to be locked in steering wheel fixed screw holes (27) to be assemblied on steering wheel holder (3) through the first screw through-hole (28), steering wheel swing arm (13) is used steering wheel swing arm fixed screw (11) to be locked in swing arm screw hole (29) to be assemblied on steering wheel (8) through the second screw through-hole (30), the first bulb screw (12) is locked on second screw hole (31) of steering wheel swing arm (13), steering wheel pull bar (10) snaps on the first bulb screw (12) and the second bulb screw (19), ball bearing (15) is bumped in the ball bearing holddown groove (35) of electric machine rotation holder (14), the bearing bore diameter (36) of electric machine rotation holder (14) is nested on tail pipe (2), motor fixing seat (17) is used motor fixing seat screw (18) to be locked in the 4th screw hole (38) to be assembled on electric machine rotation holder (14) through the 4th screw through-hole (42), motor (20) uses motor fixing screw (16) to be locked in the 5th screw hole (49) to be assembled in motor fixing seat (17) through motor fixed screw through hole (41), metal collet (21) is nested on main shaft (43), the band oblique angle through hole (45) of screw the first holder (22) and the through hole (46) of screw (23) are through metal collet (21), the tooth hole (47) that re-uses screw the second holder (24) screws in thread (44) and fixes.
CN201320799775.0U 2013-12-06 2013-12-06 Propeller vector control structure of remote-control model plane Expired - Fee Related CN203663450U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320799775.0U CN203663450U (en) 2013-12-06 2013-12-06 Propeller vector control structure of remote-control model plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320799775.0U CN203663450U (en) 2013-12-06 2013-12-06 Propeller vector control structure of remote-control model plane

Publications (1)

Publication Number Publication Date
CN203663450U true CN203663450U (en) 2014-06-25

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320799775.0U Expired - Fee Related CN203663450U (en) 2013-12-06 2013-12-06 Propeller vector control structure of remote-control model plane

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Country Link
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107970622A (en) * 2017-12-29 2018-05-01 王子铭 Remote-controlled model aircraft vector motor cabinet

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107970622A (en) * 2017-12-29 2018-05-01 王子铭 Remote-controlled model aircraft vector motor cabinet
CN107970622B (en) * 2017-12-29 2024-03-15 王子铭 Remote control model plane vector motor base

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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: 20140625

Termination date: 20191206

CF01 Termination of patent right due to non-payment of annual fee