CN218357374U - Mechanical prop wing with multi-rod linkage mechanism - Google Patents
Mechanical prop wing with multi-rod linkage mechanism Download PDFInfo
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- CN218357374U CN218357374U CN202220640327.5U CN202220640327U CN218357374U CN 218357374 U CN218357374 U CN 218357374U CN 202220640327 U CN202220640327 U CN 202220640327U CN 218357374 U CN218357374 U CN 218357374U
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Abstract
A mechanical prop wing with a multi-rod linkage mechanism is characterized in that: the back plate is fixed on the back of a human body through the shoulder straps and the waist and abdomen straps, a left electric control driving platform and a right electric control driving platform are fixedly arranged on the back side face of the back plate, the power output end of the left electric control driving platform is connected with a left multi-rod swing mechanism in a transmission mode, and the power output end of the right electric control driving platform is connected with a right multi-rod swing mechanism in a transmission mode. Provides a mechanical prop wing with a multi-rod linkage mechanism, which has novel design, light weight and strong flexibility.
Description
Technical Field
The utility model belongs to the technical field of the stage property, concretely relates to has many pole link gear machinery stage property wing.
Background
At present, static 'wings' are used in stage props at home and abroad, and the 'wings' prop is hard to represent in the performance or display of actors and has no inspiration. Even if the high-end props 'wings' shown by the models in international fashion shows are broken through only in material, and the dead and sunken 'wings' enable bright and bright models to be reduced.
Of course, there are also stage props that make changes, such as connecting the "wings" to the arms via pull lines, and controlling the swing of the "wings" by the arm movements of the actors. However, this control is very primitive and does not make the "wings" look more flexible, but rather interferes with the display of the normal body movements of the actors. Many times a compromise has to be made when sparing the dance.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a solve the weak point among the prior art, provide a novel in design, light in weight, the strong machinery stage property wing that has multi-rod link gear of flexibility.
In order to solve the technical problem, the utility model adopts the following technical scheme: the mechanical prop wing with the multi-rod linkage mechanism comprises a back plate, wherein the back plate is fixed on the back of a human body through shoulder straps and waist and belly straps, an electric control box, a left electric control driving platform and a right electric control driving platform are fixedly arranged on the back side surface of the back plate, the power output end of the left electric control driving platform is in transmission connection with a left multi-rod swinging mechanism, and the power output end of the right electric control driving platform is in transmission connection with a right multi-rod swinging mechanism; and the signal output end of the electric control box is respectively connected with the signal input ends of the left electric control driving platform and the right electric control driving platform.
The left electric control driving platform and the right electric control driving platform are identical in structure and are arranged in a left-right symmetrical mode; the right electric control driving platform comprises a first mounting frame fixedly arranged on the back plate, a wing-waving servo motor is arranged on the first mounting frame, a main shaft of the wing-waving servo motor faces upwards vertically, a second mounting frame is arranged on the main shaft of the wing-waving servo motor, a first wing-spreading servo motor is arranged on the second mounting frame, the main shaft of the first wing-spreading servo motor is perpendicular to the main shaft of the wing-waving servo motor, a third mounting frame is arranged on the main shaft of the first wing-spreading servo motor, a second wing-spreading servo motor is arranged on the third mounting frame, and the main shaft of the second wing-spreading servo motor is parallel to the main shaft of the first wing-spreading servo motor.
The left multi-rod swinging mechanism and the right multi-rod swinging mechanism have the same structure and are arranged in a left-right symmetrical mode; the right multi-rod swing mechanism comprises a first rod seat, a second rod seat, a wing spreading swing rod, a push-pull rod, a first wing rod and a second wing rod, the first rod seat is fixedly arranged at the top of the third installation frame, the left end of the first wing rod is fixedly arranged on the first rod seat, the right end of the first wing rod is rotatably connected with the second rod seat through a middle hinge, the left end of the second wing rod is fixedly arranged on the second rod seat, one end of the wing spreading swing rod is hinged to a main shaft of the second wing spreading servo motor, the other end of the wing spreading swing rod is hinged to the left end of the push-pull rod, the right end of the push-pull rod is hinged to the lower portion of the second rod seat, a plurality of hinged supports are arranged on the first wing rod and the second wing rod at intervals, a wing rod is hinged to the lower portion of each hinged support, a first wing moving connecting rod is hinged to the position between any two adjacent wing rods connected with the first wing rod, and a second wing moving connecting rod is hinged to the any two adjacent wing rods connected with the second wing rod.
A first inclined pull rod is hinged between the rightmost feather rod connected with the first fin rod and the second rod seat, and a second inclined pull rod is hinged between the rightmost feather rod connected with the second fin rod and the position of the hinge close to the middle of the right end of the first fin rod.
A third rod seat is fixedly arranged at the right end of the second finned rod, and two end feather rods are fixedly connected with the third rod seat.
The bionic wings are formed by bonding feather-like decorating parts on all rod pieces of the left multi-rod swinging mechanism and the right multi-rod swinging mechanism.
Adopt above-mentioned technical scheme, the utility model discloses a key feature does:
1) The left multi-rod swing mechanism and the right multi-rod swing mechanism (wing framework) are designed in three degrees of freedom, and are respectively driven by three servo motors (a wing-swinging servo motor, a first wing-spreading servo motor and a second wing-spreading servo motor) to spread wings, erect wings and swing wings. Every three servo motors are arranged together to form a group of electric control driving platforms. Each group of electric control driving platforms drives one set of multi-rod swinging mechanism.
In addition, two upper arms of the human body are respectively bound with an arm bandage, a three-axis electronic gyroscope for monitoring arm actions is arranged on the arm bandage, a button battery and a first communication module are arranged in the arm bandage, and the button battery box supplies power to the three-axis electronic gyroscope and the first communication module. The fixed electrical control box that is equipped with in backplate trailing flank, be equipped with the battery in the electrical control box, motor driver, second communication module and vary voltage module, the battery adopts the 24V lithium cell, the vary voltage module changes 5V voltage module for 24V, the battery is connected with motor driver and vary voltage module respectively, motor driver passes through the control line respectively with the servo motor of waving the wing, first exhibition wing servo motor and second exhibition wing servo motor are connected, the vary voltage module is connected with second communication module, the signal output part of second communication module is connected with motor driver's signal input part, the signal input part of second communication module and first communication module's signal output part wireless communication transmission signal.
2) And the three-axis electronic gyroscopes on the left upper arm and the right upper arm respectively control the servo motor driving platform on the corresponding side through the first wireless communication module, and respectively control the left multi-rod swing mechanism and the right multi-rod swing mechanism to perform different actions. The feather rod on the multi-rod swing mechanism (single wing) is controlled by the multi-rod mechanism and can move along with the wing rod. The multi-rod swing mechanism has reasonable design and flexible action.
3) The wing framework is mainly made of carbon fiber materials and is made of polymer composite materials, the self weight of the whole wing framework is not more than 2 kilograms, and the wing framework is very light.
The utility model provides a motion that right side automatically controlled drive platform drive right side multi-rod swing mechanism spreads wings is accomplished by second spread wing servo motor, second spread wing servo motor drive pendulum rod rotates, spread wing pendulum rod drive push-and-pull rod, push-and-pull rod drive second wing rod uses well hinge to rotate as the fulcrum, second rod seat also rotates thereupon, first draw bar to one side of being connected with the second rod seat drives all feather poles that first wing rod is connected and expandes, drive tip feather pole and all feather poles of being connected with the second wing rod through the second draw bar to one side simultaneously and all expand to realize spreading the wing action. The first diagonal draw bar and the second diagonal draw bar play a role in linking the synchronous extension or retraction of the feather rods on the first fin rod and the second fin rod. The feather connecting rod plays a role in linking all the feather rods in the wing spreading process.
The right electric control driving platform drives the right multi-rod swing mechanism to erect the fins, the first fin spreading servo motor drives the third mounting frame to rotate upwards, and the first fin spreading servo motor can drive the whole right multi-rod swing mechanism to rotate upwards to realize the fin erecting action as the first rod seat and the second fin spreading servo motor are both arranged on the third mounting frame.
The right electric control driving platform drives the right multi-rod swing mechanism to swing the wings, and the wing swing servo motor drives the second mounting frame to swing back and forth, namely the wing swing servo motor drives the whole right multi-rod swing mechanism to swing back and forth, so that wing swing is achieved.
To sum up, the utility model discloses principle science, simple structure, transmission are reasonable reliable, provide a wearable stage property, adopt three servo motor action of triaxial electronic gyroscope's mode control through radio communication, drive the various actions of many pole swing mechanism simulation stage property "wing". The original hard stage prop is made to be flexible instantly. The utility model discloses the beautiful model is walked to especially adapted T platform, and stage actor and COSPLAY fan use. Has wide market application prospect.
Drawings
FIG. 1 is a side view of the present invention when worn on the back;
fig. 2 is a schematic perspective view of the wing of the present invention when it is unfolded;
fig. 3 is a schematic plan view of the wing of the present invention when it is unfolded;
fig. 4 is a schematic perspective view of the wing of the present invention when retracted;
fig. 5 is a schematic plan view of the wing of the present invention when retracted.
Detailed Description
As shown in fig. 1-5, the utility model discloses a machinery stage property wing with multi-bar linkage, including backplate 1, backplate 1 is fixed at human back through baldric 3 and waist binder 4, and 1 trailing flank of backplate is fixed to be equipped with left automatically controlled drive platform and right automatically controlled drive platform, and the power take off end transmission of left automatically controlled drive platform is connected with left multi-bar swing mechanism, and the power take off end transmission of right automatically controlled drive platform is connected with right multi-bar swing mechanism, is provided with respectively on left multi-bar swing mechanism and the right multi-bar swing mechanism and prevents that the feather decoration constitutes bionical wing.
The left electric control driving platform and the right electric control driving platform are identical in structure and are arranged in a left-right symmetrical mode; the right electric control driving platform comprises a first mounting frame 8 fixedly arranged on the back plate 1, a wing-waving servo motor 9 is arranged on the first mounting frame 8, a main shaft of the wing-waving servo motor 9 vertically faces upwards, a second mounting frame 10 is arranged on the main shaft of the wing-waving servo motor 9, a first wing-spreading servo motor 11 is arranged on the second mounting frame 10, the main shaft of the first wing-spreading servo motor 11 is perpendicular to the main shaft of the wing-waving servo motor 9, a third mounting frame 12 is arranged on the main shaft of the first wing-spreading servo motor 11, a second wing-spreading servo motor 13 is arranged on the third mounting frame 12, and the main shaft of the second wing-spreading servo motor 13 is parallel to the main shaft of the first wing-spreading servo motor 11.
The left multi-rod swinging mechanism and the right multi-rod swinging mechanism have the same structure and are arranged in a bilateral symmetry way; the right multi-rod swinging mechanism comprises a first rod seat 14, a second rod seat 15, a wing spreading swinging rod 16, a push-pull rod 17, a first wing rod 18 and a second wing rod 19, the first rod seat 14 is fixedly arranged at the top of the third mounting frame 12, the left end of the first wing rod 18 is fixedly arranged on the first rod seat 14, the right end of the first wing rod 18 is rotatably connected with the second rod seat 15 through a middle hinge 20, the left end of the second wing rod 19 is fixedly arranged on the second rod seat 15, one end of the wing spreading swinging rod 16 is hinged on a main shaft of the second wing spreading servo motor 13, the other end of the wing spreading swinging rod 16 is hinged with the left end of the push-pull rod 17, the right end of the push-pull rod 17 is hinged on the lower portion of the second rod seat 15, a plurality of hinged supports 21 are arranged on the first wing rod 18 and the second wing rod 19 at intervals, a feather rod 22 is hinged on the lower portion of each hinged support 21, a first wing moving connecting rod 23 is hinged between any two feather rods 22 connected with the first wing rod 18, and a second wing moving connecting rod 24 is arranged between any two feather rods 22 connected with the second wing rod 19.
A first inclined pull rod 25 is hinged between the rightmost feather rod 22 connected with the first fin rod 18 and the second rod seat 15, and a second inclined pull rod 26 is hinged between the rightmost feather rod 22 connected with the second fin rod 19 and the position of the right end of the first fin rod 18, which is close to the middle hinge 20.
The right end of the second wing rod 19 is fixedly provided with a third rod seat 27, and the third rod seat 27 is fixedly connected with two end feather rods 28.
In addition, an arm bandage 2 is respectively bound on two upper arms 5 of the human body, a triaxial electronic gyroscope 6 for monitoring arm actions is arranged on the arm bandage 2, a button battery and a first communication module are arranged in the arm bandage 2, and the button battery box supplies power for the triaxial electronic gyroscope 6 and the first communication module. Fixed electrical control box 7 that is equipped with in 1 trailing flank of backplate, be equipped with the battery in electrical control box 7, motor driver, second communication module and vary voltage module, the battery adopts the 24V lithium cell, vary voltage module is 24V commentaries on classics 5V voltage module, the battery is connected with motor driver and vary voltage module respectively, motor driver passes through the control line respectively with waving wing servo motor, first exhibition wing servo motor and second exhibition wing servo motor are connected, vary voltage module is connected with second communication module, the signal output part of second communication module is connected with motor driver's signal input part, the signal input part of second communication module and first communication module's signal output part wireless communication transmission signal. Each device in triaxial electronic gyroscope 6, first communication module and electrical control box 7 is prior art, and is available on the market, therefore concrete structure is no longer repeated. In addition, the process of transmitting the action signal monitored in real time by the three-axis electronic gyroscope 6 and controlling the action of the servo motor by the motor driver does not relate to a new computer program.
The utility model provides a wing pole, feather pole 22, feather move the connecting rod and all adopt the carbon fiber tube preparation, and articulated part all adopts the polymer based composite preparation, and articulated part passes through the adhesive and corresponds the connecting piece bonding together.
The technical scheme of the utility model has following key feature:
1) The left multi-rod swing mechanism and the right multi-rod swing mechanism (wing skeletons) are designed in three degrees of freedom and are respectively driven by three servo motors (a wing swinging servo motor 9, a first wing spreading servo motor 11 and a second wing spreading servo motor 13) to spread wings, erect wings and swing wings. Every three servo motors are arranged together to form a group of electric control driving platforms. Each group of electric control driving platforms drives one set of multi-rod swinging mechanism. The left arm and the right arm are respectively provided with a three-axis electronic gyroscope 6, each three-axis electronic gyroscope 6 controls the servo motor driving platform on the corresponding side through a first wireless communication module, and the left multi-rod swing mechanism and the right multi-rod swing mechanism can be controlled to perform different actions respectively.
2) The feather rod 22 on the multi-rod swing mechanism (single wing) is controlled by the multi-rod mechanism and can move along with the wing rod. The multi-rod swing mechanism has reasonable design and flexible action.
3) The wearable electronic control bionic wing is mainly made of carbon fiber materials, the high polymer composite materials are used as accessories to manufacture the wing framework, the dead weight of the whole wing framework is not more than 2 kilograms, the whole wing framework is very light and convenient, and feather-proof decorating parts made of pearl wool are adhered to the wing rod and the feather rod 22 to complete the manufacture of the wearable electronic control bionic wing.
The utility model provides a motion that right side automatically controlled drive platform drive right side multi-rod swing mechanism spreads wings is accomplished by second servo motor 13 that spreads wings, second servo motor 13 that spreads wings drives the pendulum rod 16 that spreads wings and rotates, 16 drive push-and-pull rod 17 of pendulum rod that spreads wings, push-and-pull rod 17 drives second wing rod 19 and uses well hinge 20 to rotate as the fulcrum, second rod seat 15 also rotates thereupon, first oblique pull rod 25 of being connected with second rod seat 15 drives all feather rods 22 that first wing rod 18 is connected and expandes, simultaneously through the oblique pull rod 26 of second drive tip feather rod 28 and all feather rods 22 of being connected with second wing rod 19 all expand, thereby realize the action of spreading wings. The first diagonal draw bar 25 and the second diagonal draw bar 26 play a role of linking the feather rods 22 on the first wing rod 18 and the second wing rod 19 to synchronously extend or retract. The feather connecting rod plays a role in linking all the feather rods 22 in the wing spreading process.
The action of the right multi-rod swing mechanism driven by the right electric control driving platform to erect the fins is completed by the first fin spreading servo motor 11, the first fin spreading servo motor 11 drives the third mounting frame 12 to rotate upwards, and the first rod seat 14 and the second fin spreading servo motor 13 are both arranged on the third mounting frame 12, so that the first fin spreading servo motor 11 can drive the whole right multi-rod swing mechanism to rotate upwards to realize the action of erecting the fins.
The right electric control driving platform drives the right multi-rod swing mechanism to swing the wings is completed by the wing swing servo motor 9, the wing swing servo motor 9 drives the second mounting frame 10 to swing back and forth, namely the wing swing servo motor 9 drives the whole right multi-rod swing mechanism to swing back and forth, and therefore wing swing is achieved.
The present embodiment is not intended to limit the shape, material, structure, etc. of the present invention in any form, and all of the technical matters of the present invention belong to the protection scope of the present invention to any simple modification, equivalent change and modification made by the above embodiments.
Claims (6)
1. Have many poles link gear machinery stage property wing, its characterized in that: the back plate is fixed on the back of a human body through the shoulder straps and the waist and abdomen straps, a left electric control driving platform and a right electric control driving platform are fixedly arranged on the back side face of the back plate, the power output end of the left electric control driving platform is connected with a left multi-rod swing mechanism in a transmission mode, and the power output end of the right electric control driving platform is connected with a right multi-rod swing mechanism in a transmission mode.
2. The mechanical prop wing with multi-bar linkage of claim 1, wherein: the left electric control driving platform and the right electric control driving platform are identical in structure and are arranged in a left-right symmetrical mode; the right electric control driving platform comprises a first mounting frame fixedly arranged on the back plate, a fin-waving servo motor is arranged on the first mounting frame, a main shaft of the fin-waving servo motor faces upwards vertically, a second mounting frame is arranged on the main shaft of the fin-waving servo motor, a first fin-spreading servo motor is arranged on the second mounting frame, the main shaft of the first fin-spreading servo motor is perpendicular to the main shaft of the fin-waving servo motor, a third mounting frame is arranged on the main shaft of the first fin-spreading servo motor, a second fin-spreading servo motor is arranged on the third mounting frame, and the main shaft of the second fin-spreading servo motor is parallel to the main shaft of the first fin-spreading servo motor.
3. The mechanical prop wing with multi-bar linkage of claim 2, wherein: the left multi-rod swinging mechanism and the right multi-rod swinging mechanism have the same structure and are arranged in a bilateral symmetry way; the right multi-rod swing mechanism comprises a first rod seat, a second rod seat, a wing spreading swing rod, a push-pull rod, a first wing rod and a second wing rod, the first rod seat is fixedly arranged at the top of the third installation frame, the left end of the first wing rod is fixedly arranged on the first rod seat, the right end of the first wing rod is rotatably connected with the second rod seat through a middle hinge, the left end of the second wing rod is fixedly arranged on the second rod seat, one end of the wing spreading swing rod is hinged to a main shaft of the second wing spreading servo motor, the other end of the wing spreading swing rod is hinged to the left end of the push-pull rod, the right end of the push-pull rod is hinged to the lower portion of the second rod seat, a plurality of hinged supports are arranged on the first wing rod and the second wing rod at intervals, a wing rod is hinged to the lower portion of each hinged support, a first wing moving connecting rod is hinged to the position between any two adjacent wing rods connected with the first wing rod, and a second wing moving connecting rod is hinged to the any two adjacent wing rods connected with the second wing rod.
4. The mechanical prop wing with multi-bar linkage of claim 3, wherein: a first diagonal draw bar is hinged between the rightmost feather rod connected with the first fin rod and the second rod seat, and a second diagonal draw bar is hinged between the rightmost feather rod connected with the second fin rod and the position of the hinge in the position, close to the right middle of the first fin rod, of the rightmost left side of the second fin rod.
5. The mechanical prop wing with multi-bar linkage of claim 4, wherein: the right end of the second wing rod is fixedly provided with a third rod seat which is fixedly connected with two end feather rods.
6. The mechanical prop wing with multi-bar linkage of claim 5, wherein: the artificial feather decorating parts are bonded on all the rod pieces of the left multi-rod swinging mechanism and the right multi-rod swinging mechanism to form the bionic wings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220640327.5U CN218357374U (en) | 2022-03-23 | 2022-03-23 | Mechanical prop wing with multi-rod linkage mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220640327.5U CN218357374U (en) | 2022-03-23 | 2022-03-23 | Mechanical prop wing with multi-rod linkage mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218357374U true CN218357374U (en) | 2023-01-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220640327.5U Active CN218357374U (en) | 2022-03-23 | 2022-03-23 | Mechanical prop wing with multi-rod linkage mechanism |
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| Country | Link |
|---|---|
| CN (1) | CN218357374U (en) |
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2022
- 2022-03-23 CN CN202220640327.5U patent/CN218357374U/en active Active
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Effective date of registration: 20240603 Address after: 465450 Shunxiang Chemical Fiber Factory Building 15, Guandu River Industrial Agglomeration Zone, Guangshan County, Xinyang City, Henan Province Patentee after: Henan Ruixin Machinery Equipment Manufacturing Co.,Ltd. Country or region after: China Address before: 450005 No. 94 Hanghai Middle Road, Erqi District, Zhengzhou City, Henan Province Patentee before: HUANGHE S & T College Country or region before: China |