CN113273855A

CN113273855A - Model display mechanism for aerospace aircraft based on self-balancing

Info

Publication number: CN113273855A
Application number: CN202110664718.0A
Authority: CN
Inventors: 曾彦淇; 姚旭敏; 殷凤南
Original assignee: Hongdi Chongqing Information Technology Co ltd
Current assignee: Hongdi Chongqing Information Technology Co ltd
Priority date: 2021-06-16
Filing date: 2021-06-16
Publication date: 2021-08-20

Abstract

The invention discloses a self-balancing-based model display mechanism for an aerospace aircraft, and relates to the technical field of display equipment. This model show mechanism for space flight and aviation aircraft based on self-balancing, including the unable adjustment base, the top of unable adjustment base is rotated and is installed and support the pillar, and the top fixed mounting who supports the pillar has the rotation stand, and the bottom fixed mounting who rotates the stand has the support landing leg, and the top fixed mounting who rotates the stand has the support column. This model show mechanism for space flight and aviation aircraft based on self-balancing can be at the in-process convenient to detach and the installation of show by the aircraft model to setting up like this and can reducing the installation time of aircraft model when the show, increasing the efficiency of installation, can also make its effect that reaches the self-balancing at the in-process of aircraft model show, not only avoided the condition that the aircraft model dropped, can also demonstrate the in-process that removes at the aircraft simultaneously, guarantee the stability of aircraft.

Description

Model display mechanism for aerospace aircraft based on self-balancing

Technical Field

The invention relates to the technical field of display equipment, in particular to a self-balancing-based model display mechanism for an aerospace aircraft.

Background

The aircraft model need be used at display device at the in-process of show, but present partial display device structure and function are all more single, can not be effectual all the angle with the aircraft model present spectator, thereby can reduce the bandwagon effect of aircraft, and most aircraft models all fix the aircraft when the show, can lead to the aircraft model can't remove at the in-process of show like this, can reduce the bandwagon effect of aircraft model, for example, the patent that publication number is CN112869486A, fix when can showing the aircraft model, avoid the aircraft model to drop, but can't make the aircraft remove during the show, produce single visual effect like this at the in-process that spectator watched, thereby reduce the experience that spectator watched.

Disclosure of Invention

The invention aims to solve at least one of technical problems in the prior art, provides a self-balancing-based model display mechanism for an aerospace aircraft, and can solve the problems that an aircraft model cannot move in the display process and the display effect of the aircraft model is reduced.

In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a model show mechanism for space flight and aviation aircraft based on self-balancing, including the unable adjustment base, the top of unable adjustment base is rotated and is installed and support the pillar, the top fixed mounting who supports the pillar has the rotation stand, the bottom fixed mounting who rotates the stand has the support traveller, the top fixed mounting who rotates the stand has the support column, the top fixed mounting of support column has the roof, the bottom fixed mounting of roof has the dead lever, the bottom fixed mounting of dead lever has the light filling lamp fixed station, the bottom fixed mounting of light filling lamp fixed station has the light filling lamp, be provided with stand slewing mechanism on the unable adjustment base, sliding mechanism, installation mechanism and balanced fixed establishment.

Preferably, the top of the stabilizing base is provided with an annular chute, the bottom of the supporting sliding leg is fixedly provided with a sliding block, the sliding block is slidably arranged in the annular chute, and the supporting sliding leg and the stabilizing base are slidably arranged.

Preferably, stand slewing mechanism is including rotating the motor, U type guard box, the guard plate, the rotating gear, pivot and fixed tooth plate, the outer wall fixed mounting who rotates the stand has fixed tooth plate, the top fixed mounting who stabilizes the base has rotation motor and U type guard box, the top of U type guard box is rotated and is installed the pivot, the outer wall fixed mounting of pivot has rotating gear, epaxial rotating gear meshes with the fixed tooth plate that rotates on the stand mutually, the output shaft that rotates the motor passes through the shaft coupling and the one end fixed mounting of pivot, one side fixed mounting of U type guard box has the guard plate, set up like this and to increase viewer's the experience of watching.

Preferably, slide mechanism includes electronic slide rail, electronic slide, slide fixed block, fixed station and mounting box, rotates the top of stand and has seted up electronic slide rail, and the inside slidable mounting of electronic slide rail has electronic slide, and the top fixed mounting of electronic slide has the slide fixed block, and the top fixed mounting of slide fixed block has the fixed station, and the top fixed mounting of fixed station has the mounting box, sets up like this and can carry out the light filling with the aircraft when the show and handle to increase the viewing experience of viewer.

Preferably, the mounting mechanism comprises a tension spring, a lifting ring, an open lifting ring support rod, a pressing handle, a hinged lever, a lever support block, a spring fixing rod, a spring limit plate, a fixing box, a connecting cylinder, a pulling spring and a connecting pulling plate, wherein the lever support block is fixedly mounted on one side of the mounting box, the hinged lever is fixedly mounted on the top of the lever support block, the pressing handle is hinged to the hinged lever, the spring fixing rod is fixedly mounted on one side of the pressing handle, the spring is fixedly mounted on the top of the spring fixing rod, the spring limit plate is fixedly mounted on the inner wall of one side of the mounting box, the bottom of the spring limit plate is fixedly mounted on the top of the spring, the open lifting ring support rod is fixedly mounted on the top of the pressing handle, the open lifting ring is fixedly mounted on the top of the open lifting ring support rod, the open lifting ring is in lap joint with the lifting ring, and the tension spring is fixedly mounted on one end of the lifting ring, the bottom fixed mounting of support column has fixed box, and the inboard bottom fixed mounting of fixed box has the pulling spring, and the bottom fixed mounting of pulling spring has the connection pulling plate, and the bottom fixed mounting of connection pulling plate has the connection cylinder, sets up the in-process that can demonstrate the removal at the aircraft like this, guarantees the stability of aircraft.

Preferably, balanced fixed establishment includes first haulage rope, a model, the second haulage rope, fixed connection block and fixed connection post, the top and the equal fixed mounting in bottom of model have fixed connection block, the quantity of model top fixed connection block is three groups, the equal fixed mounting in top of three fixed connection blocks has fixed connection post, the equal fixed mounting in top of fixed connection post has the second haulage rope, the one end of second haulage rope and the bottom fixed mounting who is connected the pulling plate, the quantity of model bottom fixed connection block is two sets of, the equal fixed mounting in bottom of two sets of fixed connection blocks has fixed connection post, the equal fixed mounting in bottom of fixed connection post has first haulage rope, the one end of first haulage rope and the top fixed mounting of extension spring.

Preferably, two groups of openings are formed in the mounting box.

Preferably, the outer wall of the pressing handle is sleeved with an anti-slip sleeve.

Compared with the prior art, the invention has the beneficial effects that:

(1) this model show mechanism for space flight and aviation aircraft based on self-balancing, through rotating the motor, U type guard box, the cooperation of running gear and pivot is used, can drive display device when lifting the show with aircraft model, can make the show that aircraft model can not have the angle give spectator at the in-process of show like this, the bandwagon when so not only can increasing aircraft model show, also can increase spectator's the experience of watching simultaneously, ensure that spectator can all-round watch aircraft model, thereby increase the bandwagon effect of aircraft.

(2) This model show mechanism for space flight and aviation aircraft based on self-balancing, through electronic slide rail, electronic slide, the slide fixed block, the cooperation of fixed station and mounting box is used, can be at the in-process of aircraft model show, carry out reciprocating motion with aircraft model, such setting can reach the effect of removal when the aircraft show, thereby can improve the effect of aircraft model show when the show, the state when making the viewer can know the aircraft flight, the setting of light filling lamp can carry out the light filling processing with the aircraft when the show simultaneously, thereby increase the viewing experience of viewer.

(3) This model show mechanism for space flight and aviation aircraft based on self-balancing, through the extension spring, rings, opening rings bracing piece and the cooperation of pressing the handle are used, can aircraft model at the in-process convenient to detach and the installation of show, thereby set up like this and to reduce the installation time of aircraft model when the show, increase the efficiency of installation, first haulage rope, the model, the cooperation of second haulage rope and fixed connection piece is used, can make it reach the effect of self-balancing at the in-process of aircraft model show, the condition that the aircraft model dropped has not only been avoided, simultaneously can also show the in-process of removing at the aircraft, guarantee the stability of aircraft.

Drawings

The invention is further illustrated with reference to the following figures and examples:

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a front view of the present invention;

FIG. 3 is an enlarged view of portion A of the present invention;

FIG. 4 is an enlarged view of section B of the present invention;

FIG. 5 is an enlarged view of section C of the present invention;

FIG. 6 is an enlarged view of section D of the present invention.

Reference numerals: the device comprises a stabilizing base 1, a supporting rotary column 2, a rotating exhibition stand 3, a sliding leg 4, a supporting column 5, a top plate 6, a rotating mechanism of the exhibition stand 7, a rotating motor 701, a U-shaped protection box 702, a protection plate 703, a rotating gear 704, a rotating shaft 705, a fixed toothed plate 706, a sliding mechanism 8, an electric sliding rail 801, an electric sliding seat 802, a fixed block 803, a fixed block 804, a mounting box 805, a mounting mechanism 9, a tension spring 901, a lifting ring 902, a lifting ring support rod 903 with an opening, a pressing handle 904, a hinged lever 905, a lever support block 906, a spring fixing rod 907, a spring limiting plate 908, a fixed box 909, a connecting cylinder 910, a pulling spring 911, a pulling plate 912, a balance fixing mechanism 10, a first traction rope 1001, a model 1002, a second traction rope 1003, a fixed connecting block 1004, a fixed connecting column 1005, a fixed connecting rod 11, a light supplementing lamp 12 and a light supplementing lamp fixing table 13.

Detailed Description

Reference will now be made in detail to the present preferred embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to like elements throughout.

In the description of the present invention, it should be understood that the orientation or positional relationship referred to in the description of the orientation, such as the upper, lower, front, rear, left, right, etc., is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention.

In the description of the present invention, greater than, less than, exceeding, etc. are understood as excluding the present numbers, and the above, below, inside, etc. are understood as including the present numbers. If the first and second are described for the purpose of distinguishing technical features, they are not to be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated.

In the description of the present invention, unless otherwise explicitly limited, terms such as arrangement, installation, connection and the like should be understood in a broad sense, and those skilled in the art can reasonably determine the specific meanings of the above terms in the present invention in combination with the specific contents of the technical solutions.

The first embodiment is as follows:

referring to fig. 1-6, the present invention provides a technical solution: the utility model provides a model show mechanism for space flight and aviation aircraft based on self-balancing, including unable adjustment base 1, unable adjustment base 1's top is rotated and is installed and support rotary column 2, the top fixed mounting who supports rotary column 2 has rotation stand 3, the bottom fixed mounting who rotates stand 3 has support smooth leg 4, the top fixed mounting who rotates stand 3 has support column 5, the top fixed mounting of support column 5 has roof 6, the bottom fixed mounting of roof 6 has dead lever 11, the bottom fixed mounting of dead lever 11 has light filling lamp fixed station 13, the bottom fixed mounting of light filling lamp fixed station 13 has light filling lamp 12, light filling lamp 12 can carry out the light filling with the aircraft when the show and handle, thereby increase viewer's the experience of watching, the last exhibition stand slewing mechanism 7 that is provided with of unable adjustment base 1, sliding mechanism 8, installation mechanism 9 and balanced fixed establishment 10.

Furthermore, an annular chute is formed in the top of the stabilizing base 1, a sliding block is fixedly mounted at the bottom of the supporting sliding leg 4, the sliding block is slidably mounted in the annular chute, and the supporting sliding leg 4 and the stabilizing base 1 are slidably mounted.

Example two;

referring to fig. 1-6, on the basis of the first embodiment, the exhibition stand rotating mechanism 7 includes a rotating motor 701, a U-shaped protection box 702, a protection plate 703, a rotating gear 704, a rotating shaft 705 and a fixed toothed plate 706, the outer wall of the rotating exhibition stand 3 is fixedly provided with the fixed toothed plate 706, the top of the stabilizing base 1 is fixedly provided with the rotating motor 701 and the U-shaped protection box 702, the top of the U-shaped protection box 702 is rotatably provided with the rotating shaft 705, the outer wall of the rotating shaft 705 is fixedly provided with the rotating gear 704, the rotating gear 704 on the rotating shaft 705 is meshed with the fixed toothed plate 706 on the rotating exhibition stand 3, the output shaft of the rotating motor 701 is fixedly provided with one end of the rotating shaft 705 through a coupler, one side of the U-shaped protection box 702 is fixedly provided with the protection plate 703 to control the rotating motor 701 to rotate, the rotating motor 701 can drive the rotating shaft 705 and the rotating gear 704 to rotate, the rotating gear 704 can drive the fixed toothed plate 706 and the rotating exhibition stand 3 to rotate, can drive display device when hoisting the show with aircraft model and rotate, can make the show that aircraft model can not have the angle for spectator at the in-process of show like this, the display range when so not only can increasing aircraft model show also can increase the viewing experience of viewer simultaneously, ensures that the viewer can all-round watch aircraft model to increase the bandwagon effect of aircraft.

Further, the sliding mechanism 8 includes an electric slide rail 801, an electric slide seat 802, a slide seat fixing block 803, a fixing table 804 and a mounting box 805, the top of the rotary exhibition stand 3 is provided with the electric slide rail 801, the electric slide seat 802 is slidably mounted inside the electric slide rail 801, the slide seat fixing block 803 is fixedly mounted on the top of the electric slide seat 802, the fixing table 804 is fixedly mounted on the top of the slide seat fixing block 803, the mounting box 805 is fixedly mounted on the top of the fixing table 804, the electric slide seat 802 is controlled to start, the slide seat fixing block 803 and the fixing table 804 can be driven to move when the electric slide seat 802 moves, the mounting box 805 can be driven to move when the fixing table 804 moves, the tension spring 901 and the first traction rope 1001 can be driven to move when the mounting box 805 moves, the aircraft model can be reciprocated in the aircraft model display process, and the arrangement can achieve the moving effect when the aircraft display, therefore, the effect of displaying the aircraft model can be improved during displaying, and the viewer can know the flying state of the aircraft.

Still further, the mounting mechanism 9 comprises a tension spring 901, a lifting ring 902, an open lifting ring support rod 903, a pressing handle 904, a hinged lever 905, a lever support block 906, a spring fixing rod 907, a spring limiting plate 908, a fixing box 909, a connecting cylinder 910, a pulling spring 911 and a connecting pulling plate 912, wherein the lever support block 906 is fixedly mounted on one side of the mounting box 805, the hinged lever 905 is fixedly mounted on the top of the lever support block 906, the pressing handle 904 is hinged to the hinged lever 905, the spring fixing rod 907 is fixedly mounted on one side of the pressing handle 904, the spring is fixedly mounted on the top of the spring fixing rod 907, a spring limiting plate 908 is fixedly mounted on the inner wall of one side of the mounting box 805, the bottom of the spring limiting plate 908 is fixedly mounted on the top of the spring, the open lifting ring support rod 903 is fixedly mounted on the top of the pressing handle 904, and the open lifting ring 903 is fixedly mounted on the top of the open lifting ring support rod 903, the open hanging ring is overlapped with the hanging ring 902, one end of the hanging ring 902 is fixedly provided with a tension spring 901, the bottom of the supporting column 5 is fixedly provided with a fixed box 909, the bottom of the inner side of the fixed box 909 is fixedly provided with a pulling spring 911, the bottom of the pulling spring 911 is fixedly provided with a connecting pulling plate 912, the bottom of the connecting pulling plate 912 is fixedly provided with a connecting cylinder 910, a pressing handle 904 is pressed by hand, when one end of the pressing handle 904 is pressed, the other end can be driven to be lifted, a spring fixing rod 907 is driven to be lifted, when the spring fixing rod 907 is lifted, the open hanging ring supporting rod 903 can be driven to be lifted, so that the hanging ring 902 is sleeved in the open hanging ring on the open hanging ring supporting rod 903, the pressing handle 904 is loosened, when the pressing handle 904 is loosened, the spring rebounds, the pressing handle can be reset, and the aircraft model 904 can be conveniently detached and installed in the display process, thereby set up like this and can reduce the installation time of aircraft model when the show, increase the efficiency of installation, first haulage rope 1001, model 1002, second haulage rope 1003 and fixed connection piece 1004's cooperation is used, can make its effect that reaches the self-balancing at the in-process of aircraft model show, has not only avoided the condition that the aircraft model dropped, can also demonstrate the in-process that removes at the aircraft simultaneously, guarantees the stability of aircraft.

Furthermore, two sets of openings are formed in the mounting box 805, and an anti-slip sleeve is sleeved on the outer wall of the pressing handle 904.

The working principle is as follows: when the model is used, the model 1002 is fixed through the first traction rope 1001, the second traction rope 1003 and the fixed connecting block 1004, the rotating motor 701 is controlled to rotate, the rotating motor 701 can drive the rotating shaft 705 and the rotating gear 704 to rotate when rotating, the rotating gear 704 can drive the fixed toothed plate 706 and the rotating exhibition stand 3 to rotate when rotating, so that the aircraft can rotate, the light supplement lamp 12 is controlled to be turned on when displaying, the model 1002 can be irradiated by the light supplement lamp 12, the attractiveness of the model 1002 during displaying can be improved, meanwhile, the electric sliding seat 802 is controlled to be started, the sliding seat fixing block 803 and the fixed stand 804 can be driven to move when the electric sliding seat 802 moves, the mounting box 805 can be driven to move when the mounting box 804 moves, the extension spring 901 and the first traction rope 1001 can be driven to move when the mounting box moves, so that the model 1002 can be moved, when the model 1002 is disassembled, pressing handle 904 with the hand press, when pressing handle 904's one end was pressed, can drive the other end and lift up, drive spring fixing rod 907 and lift up simultaneously, spring fixing rod 907 can drive opening rings bracing piece 903 and lift up when lifting up to in the opening rings of hanging ring 902 cover on opening rings bracing piece 903, unclamp pressing handle 904, the spring is kick-backed when pressing handle 904 unclamp, can reset pressing handle 904.

The embodiments of the present invention have been described in detail with reference to the accompanying drawings, but the present invention is not limited to the above embodiments, and various changes can be made within the knowledge of those skilled in the art without departing from the gist of the present invention.

Claims

1. The utility model provides a model show mechanism for space flight and aviation aircraft based on self-balancing, includes stable base (1), its characterized in that: the top of stabilizing base (1) is rotated and is installed and support rotary column (2), the top fixed mounting who supports rotary column (2) has rotation stand (3), the bottom fixed mounting who rotates stand (3) has support smooth leg (4), the top fixed mounting who rotates stand (3) has support column (5), the top fixed mounting of support column (5) has roof (6), the bottom fixed mounting of roof (6) has dead lever (11), the bottom fixed mounting of dead lever (11) has light filling lamp fixed station (13), the bottom fixed mounting of light filling lamp fixed station (13) has light filling lamp (12), be provided with stand slewing mechanism (7) on stabilizing base (1), slide mechanism (8), installation mechanism (9) and balanced fixed establishment (10).

2. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 1, wherein: the top of the stabilizing base (1) is provided with an annular sliding groove, the bottom of the supporting sliding leg (4) is fixedly provided with a sliding block, the sliding block is slidably arranged in the annular sliding groove, and the supporting sliding leg (4) and the stabilizing base (1) are slidably arranged.

3. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 1, wherein: exhibition stand slewing mechanism (7) are including rotating motor (701), U type guard box (702), guard plate (703), slewing gear (704), pivot (705) and fixed tooth plate (706), the outer wall fixed mounting who rotates exhibition stand (3) has fixed tooth plate (706), the top fixed mounting of stabilizing base (1) has slewing motor (701) and U type guard box (702), pivot (705) are installed in the top rotation of U type guard box (702), the outer wall fixed mounting of pivot (705) has slewing gear (704), slewing gear (704) on pivot (705) and fixed tooth plate (706) on rotating exhibition stand (3) mesh mutually, the output shaft that rotates motor (701) passes through the one end fixed mounting of shaft coupling and pivot (705), one side fixed mounting of U type guard box (702) has guard plate (703).

4. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 1, wherein: slide mechanism (8) include electronic slide rail (801), electronic slide (802), slide fixed block (803), fixed station (804) and mounting box (805), electronic slide rail (801) have been seted up at the top of rotating stand (3), the inside slidable mounting of electronic slide rail (801) has electronic slide (802), the top fixed mounting of electronic slide (802) has slide fixed block (803), the top fixed mounting of slide fixed block (803) has fixed station (804), the top fixed mounting of fixed station (804) has mounting box (805).

5. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 1, wherein: the mounting mechanism (9) comprises a tension spring (901), a lifting ring (902), an open lifting ring support rod (903), a pressing handle (904), a hinged lever (905), a lever support block (906), a spring fixing rod (907), a spring limiting plate (908), a fixing box (909), a connecting cylinder (910), a pulling spring (911) and a connecting pulling plate (912), wherein the lever support block (906) is fixedly mounted on one side of the mounting box (805), the hinged lever (905) is fixedly mounted on the top of the lever support block (906), the pressing handle (904) is hinged to the hinged lever (905), the spring fixing rod (907) is fixedly mounted on one side of the pressing handle (904), the spring is fixedly mounted on the top of the spring fixing rod (907), the spring limiting plate (908) is fixedly mounted on the inner wall of one side of the mounting box (805), and the bottom of the spring limiting plate (908) is fixedly mounted on the top of the spring, an opening hanging ring supporting rod (903) is fixedly mounted at the top of the pressing handle (904), an opening hanging ring is fixedly mounted at the top of the opening hanging ring supporting rod (903), the opening hanging ring is in lap joint with the hanging ring (902), a tension spring (901) is fixedly mounted at one end of the hanging ring (902), a fixed box (909) is fixedly mounted at the bottom of the supporting column (5), a pulling spring (911) is fixedly mounted at the bottom of the inner side of the fixed box (909), a connecting pulling plate (912) is fixedly mounted at the bottom of the pulling spring (911), and a connecting cylinder (910) is fixedly mounted at the bottom of the connecting pulling plate (912).

6. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 1, wherein: the balance fixing mechanism (10) comprises a first traction rope (1001), a model (1002), a second traction rope (1003), fixed connecting blocks (1004) and fixed connecting columns (1005), wherein the fixed connecting blocks (1004) are fixedly installed at the top and the bottom of the model (1002), the number of the fixed connecting blocks (1004) at the top of the model (1002) is three, the fixed connecting columns (1005) are fixedly installed at the tops of the three fixed connecting blocks (1004), the second traction rope (1003) is fixedly installed at the top of the fixed connecting column (1005), one end of the second traction rope (1003) is fixedly installed at the bottom of a connecting pulling plate (912), the number of the fixed connecting blocks (1004) at the bottom of the model (1002) is two, the fixed connecting columns (1005) are fixedly installed at the bottoms of the two fixed connecting blocks (1004), the first traction rope (1001) is fixedly installed at the bottoms of the fixed connecting columns (1005), one end of the first traction rope (1001) is fixedly arranged on the top of the tension spring (901).

7. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 4, wherein: two groups of openings are arranged on the mounting box (805).

8. The self-balancing based model display mechanism for the aerospace and aviation aircraft according to claim 5, wherein: the outer wall cover of pressing handle (904) is equipped with anti-skidding cover.