CN216752346U - Model airplane flight control device with cable bundling function - Google Patents

Abstract

The utility model discloses a model aeroplane and model ship flight control device with cable is received and is restrainted function, including sliding plate, connecting seat and controller subassembly, the equal sliding connection in both sides of controller subassembly has the sliding plate, the both sides threaded connection of controller subassembly has the connecting seat, a set of rotation seat is installed to the sliding plate, the surface of rotation seat has cup jointed the swivel becket, the surface of swivel becket passes through the swivel becket from last to having connected gradually first deflector and second deflector down. The utility model discloses a setting of sliding plate, limiting plate, rotation seat and swivel becket, the rotation nature through the swivel becket to add the rotation nature of first deflector and second deflector, through the setting of limiting plate, linkage plate, control bolt and holding piece, cooperation holding piece plays good spacing clamping action to circuit assembly under the complementary action of linkage plate, then adds its holistic stability of circuit assembly when the device uses, alleviates the influence of rocking then.

Description

Model airplane flight control device with cable bundling function

Technical Field

The utility model relates to a flight control technical field specifically is a model aeroplane and model ship flight control device with cable function of binding up.

Background

With the appearance of the model airplane, more and more schools also develop the interest class of the relevant model airplane, and the model airplane is popular with more and more people, but the use of the existing model airplane device still has certain defects, so that the usability of the device is influenced.

The model airplane flight control device with the cable bundling function in the prior art has the defects that:

the patent document CN211987082U discloses an automatic control device for model airplane flying, which comprises a model airplane body, wherein the front part of the model airplane body is provided with a square cavity, an automatic control module shell is arranged inside the square cavity, the outer side wall of the automatic control module shell is provided with a locking device, the inside of a groove is hinged with a wedge block, the left side wall and the right side wall of the square cavity are provided with locking grooves matched with the wedge block, and the modules cooperate to complete the intelligent control function; the wedge blocks connected with the automatic control module shell are matched with the locking grooves to realize locking of the automatic control module shell in the square grooves, the automatic control module shell can be integrally disassembled by pressing down the sliding rod, and the damping spring arranged at the bottom of the automatic control module shell well realizes the effect of damping vibration, so that the electronic elements in the automatic control module shell are prevented from being damaged due to impact when the model airplane descends, the defects of the traditional technology are overcome, the device has a simple integral structure, is reliable and convenient to use and is convenient to popularize;

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a model aeroplane and model ship flight control device with cable is received and is restrainted function to solve the problem that provides among the above-mentioned background art.

In order to achieve the purpose, the utility model provides the following technical scheme, a model airplane flight control device with cable bundling function, comprising a sliding plate, a connecting seat and a controller component, wherein the sliding plate is connected with both sides of the controller component in a sliding way, and the connecting seat is connected with both sides of the controller component in a threaded way;

the sliding plate is provided with a group of rotating seats, the outer surface of each rotating seat is sleeved with a rotating ring, and the outer surface of each rotating ring is sequentially connected with a first steering plate and a second steering plate from top to bottom through the rotating ring;

the limiting plate is installed to the inboard of first deflector, the inboard of second deflector is installed and is linked up the fishplate bar.

Preferably, a protection plate is installed on one side of the connecting seat, and an insulating pad is connected to the outer side of the protection plate in an embedded mode.

Preferably, the two sides of the controller assembly are both provided with limiting sliding grooves, the bottom of the sliding plate is slidably connected inside the limiting sliding grooves, and the front end and the tail end of the controller assembly are both provided with circuit assemblies.

Preferably, the two sides of the top of the limiting plate are both provided with limiting sleeves in a penetrating mode, the middle of the top of the limiting plate is connected with a control bolt in a penetrating mode through threads, and the bottom of the control bolt is connected with a clamping piece in a embedding mode.

Preferably, the top of the connecting plate is embedded with a rubber pad, two sides of the bottom of the connecting plate are both in threaded through connection with positioning bolts, and the front ends of the positioning bolts are in threaded connection with the inner part of the limiting sleeve.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses a setting of sliding plate, limiting plate, rotation seat and swivel becket, the rotation nature through the swivel becket to add the rotation nature of first deflector and second deflector, through the setting of limiting plate, linkage plate, control bolt and holding piece, cooperation holding piece plays good spacing clamping action to circuit assembly under the complementary action of linkage plate, then adds its holistic stability of circuit assembly when the device uses, alleviates the influence of rocking then.

2. The utility model discloses a setting of connecting seat, guard plate, insulating pad and rubber pad, the guard plate passes through to carry out the threaded connection between connecting seat and the controller subassembly, consequently, it has good just, and the guard plate surface passes through insulating pad to and the setting of rubber pad on the linkage plate, thereby when addding the device use, the insulating protectiveness of its auxiliary structure improves the usability of device then.

Drawings

FIG. 1 is a perspective view of the present invention;

fig. 2 is a schematic cross-sectional view of the limiting plate structure of the present invention;

FIG. 3 is a schematic sectional view of the sliding plate structure of the present invention;

fig. 4 is a schematic sectional view of the protection plate structure of the present invention.

In the figure: 1. a sliding plate; 2. a connecting seat; 3. a controller assembly; 4. a rotating seat; 5. a rotating ring; 6. a first steer plate; 7. a second steer plate; 8. a limiting plate; 9. a connector tile; 10. a protection plate; 11. an insulating pad; 12. a line component; 13. a limiting sleeve; 14. a control bolt; 15. a clamping piece; 16. a rubber pad; 17. and (6) positioning the bolt.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

The first embodiment is as follows:

referring to fig. 1, 2 and 3, an embodiment of the present invention provides a model airplane flight control device with cable bundling function, including a sliding plate 1, a limiting plate 8 and a rotating seat 4, wherein both sides of a controller assembly 3 are respectively provided with a limiting chute, the bottom of the sliding plate 1 is slidably connected inside the limiting chute, both the front end and the tail end of the controller assembly 3 are respectively provided with a circuit assembly 12, both sides of the controller assembly 3 are respectively slidably connected with the sliding plate 1, both sides of the controller assembly 3 are respectively connected with a connecting seat 2 by screw threads, the sliding plate 1 is provided with a set of rotating seat 4, the outer surface of the rotating seat 4 is sleeved with a rotating ring 5, the outer surface of the rotating ring 5 is sequentially connected with a first steering plate 6 and a second steering plate 7 from top to bottom by the rotating ring 5, the limiting plate 8 is installed on the inner side of the first steering plate 6, both sides of the top side of the limiting plate 8 are respectively provided with a limiting sleeve 13, the middle part of the top of the limiting plate 8 is in threaded connection with a control bolt 14, the bottom of the control bolt 14 is in embedded connection with a clamping piece 15, and the inner side of the second steering plate 7 is provided with a connecting plate 9;

through the sliding plate 1, the limiting plate 8, the setting of rotating seat 4 and swivel becket 5, the rotatability through swivel becket 5, thereby add the rotatability of first deflector 6 and second deflector 7, through the limiting plate 8, the joint board 9, the setting of control bolt 14 and clamping piece 15, cooperation clamping piece 15 plays good spacing clamping action to line set 12 under the auxiliary action of joint board 9, then add its line set 12 holistic stability when the device uses, then alleviate the influence of rocking.

Example two:

referring to fig. 1, 2 and 4, in an embodiment of the present invention, a model airplane flight control device with a cable winding function includes a protection plate 10 installed on one side of a connection seat 2, an insulation pad 11 is embedded and connected on the outer side of the protection plate 10, a rubber pad 16 is embedded and installed on the top of a connection plate 9, positioning bolts 17 are threaded and connected on both sides of the bottom of the connection plate 9, and the front ends of the positioning bolts 17 are threaded and connected inside a limit sleeve 13;

through the setting of connecting seat 2, guard plate 10, insulating pad 11 and rubber pad 16, carry out threaded connection between guard plate 10 passes through connecting seat 2 and controller subassembly 3, consequently, it has good just dismantlement nature, and the guard plate 10 surface is through insulating pad 11 to and the setting of rubber pad 16 on the connection board 9, thereby when adding the device use, the insulating protectiveness of its auxiliary structure improves the usability of device then

The utility model discloses in, the device's working procedure as follows:

through the arrangement of the sliding plate 1 and the limiting plate 8, the sliding plate 1 can be provided with the rotating seat 4 and the rotating ring 5, and through the rotation of the rotating ring 5, the rotation of the first steering plate 6 and the second steering plate 7 is added, through the arrangement of the limiting plate 8 and the connecting plate 9, the limiting plate 8 and the connecting plate 9 are matched through the limiting sleeve 13 and the positioning bolt 17, so that the connection and fixation effect is achieved, after the limiting plate 8 and the connecting plate 9 are limited, the clamping piece 15 can be pushed through the rotation of the control bolt 14, then the clamping piece 15 is matched under the auxiliary effect of the connecting plate 9, so that the circuit component 12 can be well limited and clamped, the integral stability of the circuit component 12 when the device is used is added, then the shaking influence is reduced, through the arrangement of the connecting seat 2 and the protection plate 10, the protection plate 10 is in threaded connection with the controller component 3 through the connecting seat 2, therefore, the device has good convenience for disassembly, and the surface of the protection plate 10 is provided with the insulating pad 11 and the rubber pads 16 on the connecting joint plates 9, so that the insulating protection performance of the auxiliary structure is added when the device is used, and the usability of the device is improved.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Claims (5)

1. The utility model provides a model aeroplane and model ship flight control device with cable function of restrainting, includes sliding plate (1), connecting seat (2) and controller subassembly (3), its characterized in that: sliding plates (1) are connected to two sides of the controller component (3) in a sliding mode, and connecting seats (2) are connected to two sides of the controller component (3) in a threaded mode;

the sliding plate (1) is provided with a group of rotating seats (4), the outer surface of each rotating seat (4) is sleeved with a rotating ring (5), and the outer surface of each rotating ring (5) is sequentially connected with a first steering plate (6) and a second steering plate (7) from top to bottom through the rotating ring (5);

limiting plates (8) are installed on the inner sides of the first steering plates (6), and connecting plates (9) are installed on the inner sides of the second steering plates (7).

2. The model airplane flight control device with the cable bundling function according to claim 1, characterized in that: a protection plate (10) is installed on one side of the connecting seat (2), and an insulation pad (11) is connected to the outer side of the protection plate (10) in an embedded mode.

3. The model airplane flight control device with the cable bundling function according to claim 1, characterized in that: the limiting sliding grooves are formed in the two sides of the controller assembly (3), the bottom of the sliding plate (1) is connected to the inside of the limiting sliding grooves in a sliding mode, and the front end and the tail end of the controller assembly (3) are provided with line assemblies (12).

4. The model airplane flight control device with the cable bundling function according to claim 1, characterized in that: limiting sleeve pipes (13) are installed on two sides of the top of the limiting plate (8) in a penetrating mode, a control bolt (14) is connected to the middle of the top of the limiting plate (8) in a penetrating mode through threads, and clamping pieces (15) are connected to the bottom of the control bolt (14) in an embedded mode.

5. The model airplane flight control device with the cable bundling function according to claim 1, characterized in that: the top of the connecting plate (9) is embedded with a rubber pad (16), two sides of the bottom of the connecting plate (9) are in threaded through connection with positioning bolts (17), and the front ends of the positioning bolts (17) are in threaded connection with the inner part of the limiting sleeve (13).

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