CN110585748B - Phoenix-shaped stage-art device and model steering control system thereof - Google Patents

Phoenix-shaped stage-art device and model steering control system thereof Download PDF

Info

Publication number
CN110585748B
CN110585748B CN201910904097.1A CN201910904097A CN110585748B CN 110585748 B CN110585748 B CN 110585748B CN 201910904097 A CN201910904097 A CN 201910904097A CN 110585748 B CN110585748 B CN 110585748B
Authority
CN
China
Prior art keywords
phoenix
model
model frame
truss
wind direction
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.)
Active
Application number
CN201910904097.1A
Other languages
Chinese (zh)
Other versions
CN110585748A (en
Inventor
朱晨华
刘华
吴永建
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.)
Hangzhou West Lake Fountain Installation Serials Co ltd
Original Assignee
Hangzhou West Lake Fountain Installation Serials 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 Hangzhou West Lake Fountain Installation Serials Co ltd filed Critical Hangzhou West Lake Fountain Installation Serials Co ltd
Priority to CN201910904097.1A priority Critical patent/CN110585748B/en
Publication of CN110585748A publication Critical patent/CN110585748A/en
Application granted granted Critical
Publication of CN110585748B publication Critical patent/CN110585748B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63JDEVICES FOR THEATRES, CIRCUSES, OR THE LIKE; CONJURING APPLIANCES OR THE LIKE
    • A63J1/00Stage arrangements
    • A63J1/02Scenery; Curtains; Other decorations; Means for moving same
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63JDEVICES FOR THEATRES, CIRCUSES, OR THE LIKE; CONJURING APPLIANCES OR THE LIKE
    • A63J5/00Auxiliaries for producing special effects on stages, or in circuses or arenas
    • A63J5/02Arrangements for making stage effects; Auxiliary stage appliances

Landscapes

  • Toys (AREA)

Abstract

The invention relates to the technical field of stage-design devices, in particular to a stage-design device with a phoenix shape and a model steering control system thereof. The utility model provides a phoenix figurative stage-art device, including supporting component and be located the phoenix molding subassembly of supporting component top, phoenix molding subassembly includes phoenix model frame and drives the driving component of phoenix model frame along vertical plane motion, phoenix model frame includes the body model frame, rotate the wing root model frame of connecting in body model frame both sides, rotate the wing tip model frame of connecting in wing root model frame one end of keeping away from body model frame, be equipped with the flexible power component of drive wing root model frame wobbling on the body model frame, be equipped with the flexible power component of drive wing tip model frame wobbling on the wing root model frame. The drive assembly adjusts the movement of the phoenix model frame along a vertical plane to exhibit positional changes of the phoenix as it flies. The telescopic power element controls the wing root model frame and the wing tip model frame to swing so as to show the flapping gesture of the wings when the phoenix flies.

Description

Phoenix-shaped stage-art device and model steering control system thereof
Technical Field
The invention relates to the technical field of stage-design devices, in particular to a stage-design device with a phoenix shape and a model steering control system thereof.
Background
Stage art is an important component of drama and other stage performances, including scenery, lights, make-up, clothing, effects, props, and the like. Their integrated design is called stage design.
The prior patent with the publication number of CN201551857U discloses a stage prop bird. In the scheme, the eccentric wheel is driven to rotate by the motor, and the connecting rod is driven to swing up and down to display the wing state of the bird fan in the rotating process of the eccentric wheel.
The prior art solution described above has the following drawbacks: the wings can only swing along the hinging points and can be used as a stage performance auxiliary device, but when the wing is used as a stage main performance unit with a phoenix shape, the too stiff wing motions obviously cannot support the requirements of motion and beauty when the phoenix flies.
Disclosure of Invention
One of the objects of the present invention is to provide a phoenix shaped stage device that is advantageous in that it is capable of exhibiting the action of a phoenix flying.
The above object of the present invention is achieved by the following technical solutions: the utility model provides a phoenix figurative stage-art device, includes supporting component and is located the phoenix molding subassembly of supporting component top, phoenix molding subassembly includes phoenix model frame and drives phoenix model frame along the drive assembly of vertical plane motion, and phoenix model frame includes the body model frame, rotates the wing root model frame of connecting in body model frame both sides, rotates the wing tip model frame of connecting in wing root model frame one end of keeping away from body model frame, is equipped with the flexible power component of drive wing root model frame wobbling on the body model frame, is equipped with the flexible power component of drive wing tip model frame wobbling on the wing root model frame.
Through adopting above-mentioned technical scheme, adjust phoenix model frame through drive assembly and follow vertical plane motion to demonstrate the position change of phoenix when flying. The wing root model frame and the wing tip model frame are controlled to swing through the telescopic power element so as to show the flapping gesture of the wings of the phoenix during flying. Therefore, the phoenix flying gesture during the stage-design performance can be better displayed.
The invention is further provided with: the driving assembly comprises a first truss, a first telescopic power element, a second truss and a second telescopic power element, wherein the lower end of the first truss is rotationally connected with the supporting assembly, the first telescopic power element drives the first truss to swing, the second truss is rotationally connected with the upper end of the first truss, the second telescopic power element drives the second truss to swing, the upper end of the second truss is rotationally connected with the phoenix model frame, and the third telescopic power element drives the phoenix model frame to swing is arranged on the second truss.
Through adopting above-mentioned technical scheme, drive first truss swing through first flexible power component, drive second truss swing through the flexible power component of second, both cooperate to realize that the phoenix can move to the arbitrary position in the scope. The phoenix is driven to swing through the third telescopic power element to show the pitching and pitching states.
The invention is further provided with: the support assembly is provided with a groove, the lower end of the first telescopic power element is rotationally connected to the bottom of the groove, the rotational connecting point of the second telescopic power element and the first truss is located on the lower side face of the upper end of the first truss, the other end of the second telescopic power element penetrates through the first truss and then is rotationally connected with the second truss, the rotational connecting point of the third telescopic power element and the second truss is located on the lower side face of the upper end of the second truss, and the other end of the third telescopic power element penetrates through the second truss and then is rotationally connected with the phoenix model frame.
Through adopting above-mentioned technical scheme, because flexible power component still has certain length when contracting to the shortest state, consequently set up first flexible power component in the recess bottom, second flexible power component connects in first truss downside, and third flexible power component connects the downside at the second truss for can use recess degree of depth, truss thickness direction as the space that holds flexible power component after flexible power component contracts to the shortest state, make flexible power component accomodate completely and play back phoenix can fall on supporting component.
The invention is further provided with: the support assembly comprises a base station positioned in the water tank, a first cavity is formed in the base station, a servo motor is installed in the first cavity, the servo motor drives a first driving rod in the horizontal direction to rotate through chain transmission, a second cavity is formed in the base station at the side face of the first cavity, one end of the first driving rod stretches into the second cavity is connected with a first bevel gear, a vertical second driving rod is installed in the second cavity, and a second bevel gear meshed with the first bevel gear is installed on the second driving rod. The upper end of the second driving rod exceeds the upper end face of the base station, a rotary platform is fixed at the upper end of the second driving rod, and the driving assembly is connected with the rotary platform.
Through adopting above-mentioned technical scheme, servo motor drives first actuating lever through chain drive and rotates, and first actuating lever drives the rotation of second actuating lever through first bevel gear and second bevel gear cooperation for rotary platform rotates thereupon.
The invention is further provided with: the outside of phoenix model frame all pastes has the concrete molding paster that outlines the phoenix appearance.
By adopting the technical scheme, the phoenix model frame is finally formed into a phoenix model through the adhesive concrete modeling paster.
The invention is further provided with: and a plurality of flame injectors are arranged at the tail end of the phoenix model frame.
By adopting the technical scheme, flame is sprayed by the flame sprayer to form flame phoenix tail feather.
Another object of the present invention is to provide a model orientation control system of a stage design device with a phoenix model, which is advantageous in that the stage design device can be prevented from toppling over under the action of strong wind.
The above object of the present invention is achieved by the following technical solutions:
The model orientation control system of the phoenix-shaped stage-art device is characterized in that: the wind direction detection device comprises a model direction detection module, a wind direction detection module and an execution module;
The model orientation detection module is used for detecting the head end orientation of the phoenix model frame;
the wind direction detection module is used for detecting the real-time wind direction;
And the execution module drives the servo motor to rotate when the direction measured by the model facing the detection module is different from the direction measured by the wind direction detection module, and closes the servo motor when the direction measured by the model facing the detection module is the same as the direction measured by the wind direction detection module.
Through adopting above-mentioned technical scheme, detect phoenix model orientation through model orientation detection module, detect the wind direction through wind direction detection module, servo motor adjusts phoenix model orientation the same with the wind direction, leads to phoenix model body and wing part to receive great side thrust and topple over when avoiding the strong wind of side direction to blow to the phoenix model. Meanwhile, the showing state of the phoenix model can be changed, so that the same position can appreciate the flying postures of the phoenix in different directions.
The invention is further provided with: the model orientation detection module comprises eight proximity switches, and the eight proximity switches are arranged according to orientation sequence numbers; the wind direction detection module comprises a wind direction sensor, and eight response positions of the wind direction sensor respectively control eight normally closed switches in response; each proximity switch and a normally closed switch S for detecting the wind in the same direction form a unidirectional detection group, different unidirectional detection groups are connected in parallel to form a detection circuit, one end of the detection circuit is connected with a power supply VCC, the other end of the detection circuit is grounded, a contact switch SB is connected in series between the detection circuit and the power supply VCC, and a relay coil KM1 is connected in series between the detection circuit and the grounding end.
Through adopting above-mentioned technical scheme, through establishing ties proximity switch and normally closed switch of corresponding orientation for only respond relay coil KM1 can lose electricity simultaneously at proximity switch and normally closed switch of same orientation.
The invention is further provided with: the execution module comprises a servo motor connected in series between a power supply VCC and a grounding end, and a relay normally open switch KM1-1 is connected in series between the servo motor and the power supply VCC.
By adopting the technical scheme, when the relay coil KM1 is electrified, the normally open switch KM1-1 of the relay is closed to start the servo motor, and otherwise, the servo motor is closed.
The invention is further provided with:
the system also comprises an operation module, wherein the operation module comprises an operation chip, and the operation process comprises the following steps:
step one, acquiring model orientation data and wind direction data;
the corresponding normally closed switches are numbered sequentially when the proximity switch and the wind direction sensor respond, so that the model orientation data number a and the wind direction data number b can be obtained according to the responses of the proximity switch and the wind direction sensor;
Step two, calculating a forward rotation adjusting distance and a reverse rotation adjusting distance of the rotating platform;
Calculating to obtain forward rotation adjustment pitch distance x and reverse rotation adjustment distance y of the rotary platform according to the model orientation data number a and the wind direction data number b;
step three, comparing the sizes of x and y;
When x is smaller than y, judging that the servo motor is required to drive the rotary platform to rotate positively; when x is larger than y, the servo motor drives the rotary platform to rotate reversely.
Through adopting above-mentioned technical scheme, obtain the phoenix model through operation module and rotate fast to the direction to the wind direction to make the phoenix module rotate fast to the state to the wind direction along this direction. Because the wind direction is gradually changed, rotating the phoenix model along the shortest distance means that the model rotation direction is the same as the wind direction gradually changing direction, and the time and the times of the phoenix model side to the wind direction can be reduced.
In summary, the beneficial technical effects of the invention are as follows:
1. The gesture of phoenix flying during the performance of the stage is better displayed;
2. Adjust phoenix model orientation the same with the wind direction, lead to when avoiding the strong wind of side direction to blow to the phoenix model that the phoenix model body and wing part receive great side direction thrust and empty, can change the demonstration state of phoenix model simultaneously for the different azimuthal flight gesture of phoenix can be appreciated to the coplanar.
Drawings
FIG. 1 is a schematic structural view of a first embodiment;
FIG. 2 is a schematic cross-sectional view of the first embodiment;
FIG. 3 is a schematic view of a structure of a frame of a phoenix model in accordance with the first embodiment;
FIG. 4 is a partial schematic view of the first embodiment;
FIG. 5 is a circuit diagram of a model orientation detection module and a wind direction detection module in the second embodiment;
FIG. 6 is a circuit diagram of an execution module in the second embodiment;
FIG. 7 is a schematic diagram of the correspondence between normally closed switches and wind direction in the second embodiment;
fig. 8 is a schematic structural diagram of a wind direction detection module in the third embodiment.
Reference numerals: 1. a support assembly; 2. a phoenix modeling component; 3. a base station; 4. a first cavity; 5. a servo motor; 6. a first driving lever; 7. a second cavity; 8. a first bevel gear; 9. a second driving lever; 10. a second bevel gear; 11. rotating the platform; 12. a groove; 13. a first truss; 14. a second truss; 15. a phoenix model frame; 16. a first telescoping power element; 17. a second telescopic power element; 18. a third telescoping power element; 19. a body model frame; 20. a wing root model frame; 21. a fin tip model frame; 22. a fourth telescoping power element; 23. a fifth telescoping power element; 24. a flame injector; 25. a steel plate; 26. wind wings.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
Embodiment one:
As shown in fig. 1, a phoenix-shaped stage device comprises a support assembly 1 and a phoenix-shaped assembly 2 above the support assembly 1.
As shown in fig. 2, the support assembly 1 includes a base 3 positioned in a pool of water, with the uppermost end of the base 3 being above the water surface. The base 3 is internally provided with a first cavity 4, the bottom of the first cavity 4 is provided with a servo motor 5, and a first driving rod 6 in the horizontal direction is arranged in the first cavity 4 at a position close to the middle part along the height direction. The servo motor 5 drives the first driving rod 6 to rotate through chain transmission. Both ends of the first driving lever 6 are inserted into the base 3, and bearings are installed in the base 3 as rotational supports of the first driving lever 6.
As shown in fig. 2, a second cavity 7 is formed in the base 3 at a position on the side of the first cavity 4. One end of the first driving rod 6 extends into the second cavity 7, and one end of the first driving rod 6 extending into the second cavity 7 is connected with a first bevel gear 8. A second vertical driving rod 9 is arranged in the second cavity 7, and the upper end and the lower end of the second driving rod 9 are supported by bearings embedded in the base 3. The second drive rod 9 is provided with a second bevel gear 10 which meshes with the first bevel gear 8. The upper end of the second driving rod 9 exceeds the upper end surface of the base 3, and a rotary platform 11 is fixed to the upper end of the second driving rod 9. The middle part of the upper end surface of the rotary platform 11 is provided with a groove 12.
As shown in fig. 2, the phoenix modeling assembly 2 comprises a first truss 13 rotatably connected with a rotary platform 11, wherein a second truss 14 is rotatably connected to the upper end of the first truss 13, and a phoenix model frame 15 is rotatably connected to the upper end of the second truss 14. The rotary connection point of the first truss 13 and the rotary platform 11 is located on the side face of the groove 12, the bottom of the groove 12 is rotationally connected with a first telescopic power element 16, the upper end of the first telescopic power element 16 is rotationally connected with the first truss 13, and swing of the first truss 13 is controlled through telescopic of the first telescopic power element 16. The lower side edge of the upper end of the first truss 13 is rotationally connected with a second telescopic power element 17, the other end of the second telescopic power element 17 penetrates through the first truss 13 and is rotationally connected with the second truss 14, and the swing of the second truss 14 is controlled through the telescopic action of the second telescopic power element 17. The lower side of the upper end of the second truss 14 is in transmission connection with a third telescopic power element 18, the other end of the third telescopic power element 18 penetrates through the second truss 14 and then is in rotary connection with the phoenix model frame 15, and the phoenix model frame 15 swings under the telescopic control of the third telescopic power element 18. The first truss 13, the second truss 14, the third truss, the first telescoping power element 16, the second telescoping power element 17, and the third telescoping power element 18 form a drive assembly that drives the phoenix pattern frame 15 to move along a vertical plane.
As shown in fig. 3, the phoenix model frame 15 includes a body model frame 19 formed by constructing section steel, wing root model frames 20 rotatably connected to both sides of the body model frame 19, and wing tip model frames 21 rotatably connected to one end of the wing root model frames 20 away from the body model frame 19. A fourth telescopic power element 22 is rotatably connected to the body model frame 19 at a position above the rotation connection point of the fin root model frame 20 and the body model frame 19, and the swing of the fin root model frame 20 is controlled by the telescopic motion of the fourth telescopic power element 22. The side surface of one end, far away from the trunk model frame 19, of the fin root model frame 20 is rotatably connected with a fifth telescopic power element 23, one end, far away from the fin root model frame 20, of the fifth telescopic power element 23 is rotatably connected with the fin tip model frame 21, and the fin tip model frame 21 is controlled to swing through the telescopic of the fifth telescopic power element 23. All telescopic power elements can be cylinders. The outside of the phoenix model frame 15 is respectively stuck with a concrete modeling patch, and the appearance of the phoenix is sketched through the concrete modeling patch. The tail end of the phoenix model frame 15 is mounted with a plurality of flame injectors 24, and flames are injected as phoenix tail feathers through the flame injectors 24.
As shown in fig. 2 and 4, the side of the rotary table 11 facing the head of the phoenix model frame 15 is coated with a steel plate 25, and the steel plate 25 is coated with only one eighth of the length of the circumference of the rotary table 11. Eight proximity switches are uniformly arranged around the rotary platform 11, and the proximity switches respond only when the steel plate 25 rotates to a position opposite to the proximity switches. The base 3 is also provided with a wind direction sensor which has eight response positions, and the directions of the eight response positions are in one-to-one correspondence with the directions of the eight proximity switches relative to the rotary platform 11.
Embodiment two:
as shown in fig. 5 and 6, a model orientation control system of a stage device includes a model orientation detection module, a wind direction detection module, an execution module, and an operation module. The model orientation detection module comprises eight proximity switches, the eight proximity switches are arranged according to orientation sequence numbers, the proximity switches are marked as a first proximity switch towards the east, a second proximity switch towards the southeast, a third proximity switch towards the south, a fourth proximity switch towards the southwest, a fifth proximity switch towards the west, a sixth proximity switch towards the northwest, a seventh proximity switch towards the north, and an eighth proximity switch towards the northeast. As shown in fig. 7, the wind direction detection module includes a wind direction sensor, and eight response positions of the wind direction sensor respectively control the eight normally closed switches S1, S2, S3, S4, S5, S6, S7, S8 to be turned off in response.
As shown in fig. 5, each proximity switch and a normally closed switch S for detecting the wind in the same direction form a unidirectional detection group, different unidirectional detection groups are connected in parallel to form a detection circuit, one end of the detection circuit is connected with a power supply VCC, and the other end of the detection circuit is grounded. A contact switch SB is connected in series between the detection circuit and the power supply VCC, and a relay coil KM1 is connected in series between the detection circuit and the grounding end.
As shown in fig. 6, the execution module includes a servomotor 5 connected in series between a power supply VCC and a ground terminal, and a normally open relay switch KM1-1 is connected in series between the servomotor 5 and the power supply VCC.
The operation module comprises an operation chip, and the operation process comprises the following steps:
step one, obtaining model orientation data and wind direction data
The corresponding normally closed switches are numbered sequentially when the proximity switch and the wind direction sensor respond, so that the model orientation data number a and the wind direction data number b can be obtained according to the responses of the proximity switch and the wind direction sensor.
Step two, calculating the forward rotation adjustment distance and the reverse rotation adjustment distance of the rotating platform 11
The clockwise rotation of the rotary table 11 in the plan view is defined as the normal rotation.
Calculating the forward modulation pitch separation x of the rotary platform 11:
calculating the reverse rotation adjustment distance y of the rotating platform 11:
Step three, comparing the x and y sizes
When x is smaller than y, the servo motor 5 drives the rotary platform 11 to rotate positively; when x is greater than y, the servo motor 5 drives the rotary stage 11 to rotate reversely.
After the wind direction sensor detects the changed wind direction, the normally closed switch S in the original direction is closed, and the normally closed switch S in the corresponding wind direction is opened. At this time, the operation module performs the operation to determine in which rotation direction the rotary table 11 rotates to reach the destination, the stroke is short. When the number of the responsive proximity switch is different from the number of the normally closed switch S, the relay coil KM1 is electrified, the normally open switch KM1-1 of the relay is closed, and the servo motor 5 is started to drive the rotary platform 11 to rotate.
When the number of the corresponding proximity switch is the same as that of the normally closed switch S, the model is the same as the wind direction, the proximity switch passage, the normally closed switch is disconnected, the relay coil KM1 is powered off, the normally open switch KM1-1 of the relay is disconnected, and the servo motor 5 is powered off and does not drive the rotary platform 11 to rotate.
Embodiment III:
a phoenix-shaped stage device, as shown in fig. 8, differs from the first embodiment only in that the wind direction detection module uses wind wings 26 rotating along a vertical axis, and that one proximity switch is provided in each of eight directions of the wind wings 26 to detect the orientation of the wind wings 26, in which eight proximity switches replace the eight normally closed switches S of the above scheme in the circuit.
The embodiments of the present invention are all preferred embodiments of the present invention, and are not intended to limit the scope of the present invention in this way, therefore: all equivalent changes in structure, shape and principle of the invention should be covered in the scope of protection of the invention.

Claims (8)

1. Model orientation control system of a stage-design device, the stage-design device includes supporting component (1) and is located phoenix molding subassembly (2) of supporting component (1) top, characterized by: the phoenix modeling assembly (2) comprises a phoenix model frame (15) and a driving assembly for driving the phoenix model frame (15) to move along a vertical plane, the phoenix model frame (15) comprises a body model frame (19), wing root model frames (20) rotatably connected to two sides of the body model frame (19), wing tip model frames (21) rotatably connected to one ends, far away from the body model frame (19), of the wing root model frames (20), telescopic power elements for driving the wing root model frames (20) to swing are arranged on the body model frames (19), and telescopic power elements for driving the wing tip model frames (21) to swing are arranged on the wing root model frames (20);
The support assembly (1) comprises a base table (3) positioned in a water tank, a first cavity (4) is formed in the base table (3), a servo motor (5) is installed in the first cavity (4), the servo motor (5) drives a first driving rod (6) in the horizontal direction to rotate through chain transmission, a second cavity (7) is formed in the base table (3) at the side of the first cavity (4), one end of the first driving rod (6) stretches into the second cavity (7) and is connected with a first bevel gear (8), a vertical second driving rod (9) is installed in the second cavity (7), a second bevel gear (10) meshed with the first bevel gear (8) is installed on the second driving rod (9), the upper end of the second driving rod (9) exceeds the upper end face of the base table (3), a rotary platform (11) is fixed at the upper end of the second driving rod (9), and the driving assembly is connected with the rotary platform (11).
The model orientation control system comprises a model orientation detection module, a wind direction detection module and an execution module;
the model orientation detection module is used for detecting the head end orientation of the phoenix model frame (15);
the wind direction detection module is used for detecting the real-time wind direction;
And the execution module is used for driving the servo motor (5) to rotate when the direction measured by the model orientation detection module is different from the direction measured by the wind direction detection module, and closing the servo motor (5) when the direction measured by the model orientation detection module is the same as the direction measured by the wind direction detection module.
2. The model orientation control system of a stage assembly of claim 1, wherein: the driving assembly comprises a first truss (13) with the lower end rotationally connected with the supporting assembly (1), a first telescopic power element (16) for driving the first truss (13) to swing, a second truss (14) rotationally connected with the upper end of the first truss (13), a second telescopic power element (17) for driving the second truss (14) to swing, the upper end of the second truss (14) is rotationally connected with the phoenix model frame (15), and a third telescopic power element (18) for driving the phoenix model frame (15) to swing is arranged on the second truss (14).
3. The model orientation control system of a stage assembly of claim 2, wherein: the support assembly (1) is provided with a groove (12), the lower end of the first telescopic power element (16) is rotationally connected to the bottom of the groove (12), a rotational connection point of the second telescopic power element (17) and the first truss (13) is located on the lower side face of the upper end of the first truss (13), the other end of the second telescopic power element (17) penetrates through the first truss (13) and then is rotationally connected with the second truss (14), a rotational connection point of the third telescopic power element (18) and the second truss (14) is located on the lower side face of the upper end of the second truss (14), and the other end of the third telescopic power element (18) penetrates through the second truss (14) and then is rotationally connected with the phoenix model frame (15).
4. The model orientation control system of a stage assembly of claim 1, wherein: the outside of phoenix model frame (15) all is pasted and is had the concrete molding paster that outlines the phoenix appearance.
5. The model orientation control system of a stage assembly of claim 1, wherein: the tail end of the phoenix model frame (15) is provided with a plurality of flame injectors (24).
6. The model orientation control system of a stage assembly of claim 1, wherein: the model orientation detection module comprises eight proximity switches, and the eight proximity switches are arranged according to orientation sequence numbers; the wind direction detection module comprises a wind direction sensor, and eight response positions of the wind direction sensor respectively control eight normally closed switches in response; each proximity switch and a normally closed switch S for detecting the wind in the same direction form a unidirectional detection group, different unidirectional detection groups are connected in parallel to form a detection circuit, one end of the detection circuit is connected with a power supply VCC, the other end of the detection circuit is grounded, a contact switch SB is connected in series between the detection circuit and the power supply VCC, and a relay coil KM1 is connected in series between the detection circuit and the grounding end.
7. The model orientation control system of the stage assembly of claim 6, wherein: the execution module comprises a servo motor (5) connected in series between a power supply VCC and a grounding end, and a relay normally open switch KM1-1 is connected in series between the servo motor (5) and the power supply VCC.
8. The model orientation control system of the stage assembly of claim 6, wherein: the system also comprises an operation module, wherein the operation module comprises an operation chip, and the operation process comprises the following steps:
step one, acquiring model orientation data and wind direction data;
the corresponding normally closed switches are numbered sequentially when the proximity switch and the wind direction sensor respond, so that the model orientation data number a and the wind direction data number b can be obtained according to the responses of the proximity switch and the wind direction sensor;
step two, calculating forward rotation adjustment pitch distance and reverse rotation adjustment distance of the rotary platform (11);
Calculating to obtain a forward modulation pitch distance x and a reverse modulation distance y of the rotary platform (11) according to the model orientation data number a and the wind direction data number b;
step three, comparing the sizes of x and y;
when x is smaller than y, judging that the servo motor (5) is required to drive the rotary platform (11) to rotate positively; when x is larger than y, the servo motor (5) drives the rotary platform (11) to rotate reversely.
CN201910904097.1A 2019-09-24 2019-09-24 Phoenix-shaped stage-art device and model steering control system thereof Active CN110585748B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910904097.1A CN110585748B (en) 2019-09-24 2019-09-24 Phoenix-shaped stage-art device and model steering control system thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910904097.1A CN110585748B (en) 2019-09-24 2019-09-24 Phoenix-shaped stage-art device and model steering control system thereof

Publications (2)

Publication Number Publication Date
CN110585748A CN110585748A (en) 2019-12-20
CN110585748B true CN110585748B (en) 2024-05-14

Family

ID=68862986

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910904097.1A Active CN110585748B (en) 2019-09-24 2019-09-24 Phoenix-shaped stage-art device and model steering control system thereof

Country Status (1)

Country Link
CN (1) CN110585748B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113844207B (en) * 2021-09-13 2022-08-19 北京东方舞台科技有限公司 Outdoor dynamic butterfly model

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB375530A (en) * 1931-06-10 1932-06-30 John Kenneth Crowe Improvements in aeroplanes
KR910004049U (en) * 1989-08-17 1991-03-18 박철희 Wing drive device for children's amusement rides
CN2262445Y (en) * 1996-03-18 1997-09-17 舒宏琦 Mechanism for imitating actions of fowls and animals
JP2006167417A (en) * 2004-12-16 2006-06-29 Yoshio Fujino Vertical lift rotating kite with helicopter-like rotary wing
CN102772906A (en) * 2012-08-17 2012-11-14 杭州佳合舞台设备有限公司 Modeling property for stage
CN203425533U (en) * 2013-08-01 2014-02-12 常州金刚网络技术有限公司 Bionic robot for performance
CN104338330A (en) * 2013-08-01 2015-02-11 常州金刚文化科技集团有限公司 Bio-robot used for performing
CN104548612A (en) * 2014-12-24 2015-04-29 苏州原点工业设计有限公司 Model airship and aerofoil
CN106390484A (en) * 2015-07-31 2017-02-15 北京秀域科技文化有限公司 In-water fountain egret demonstrating device
CN106390485A (en) * 2015-07-31 2017-02-15 北京秀域科技文化有限公司 Water-surface demonstrating device
KR101950401B1 (en) * 2018-10-02 2019-02-20 플러스파운틴(주) Levitation water fountain apparatus using drone
CN109542108A (en) * 2017-09-22 2019-03-29 南京开天眼无人机科技有限公司 A kind of unmanned plane wind resistance patrols winged system
CN209123339U (en) * 2018-09-26 2019-07-19 张天伟 A kind of faucet dynamic kite
CN211158609U (en) * 2019-09-24 2020-08-04 杭州西湖喷泉设备成套有限公司 Dance beauty device with phoenix modeling and model steering control system thereof

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB375530A (en) * 1931-06-10 1932-06-30 John Kenneth Crowe Improvements in aeroplanes
KR910004049U (en) * 1989-08-17 1991-03-18 박철희 Wing drive device for children's amusement rides
CN2262445Y (en) * 1996-03-18 1997-09-17 舒宏琦 Mechanism for imitating actions of fowls and animals
JP2006167417A (en) * 2004-12-16 2006-06-29 Yoshio Fujino Vertical lift rotating kite with helicopter-like rotary wing
CN102772906A (en) * 2012-08-17 2012-11-14 杭州佳合舞台设备有限公司 Modeling property for stage
CN104338330A (en) * 2013-08-01 2015-02-11 常州金刚文化科技集团有限公司 Bio-robot used for performing
CN203425533U (en) * 2013-08-01 2014-02-12 常州金刚网络技术有限公司 Bionic robot for performance
CN104548612A (en) * 2014-12-24 2015-04-29 苏州原点工业设计有限公司 Model airship and aerofoil
CN106390484A (en) * 2015-07-31 2017-02-15 北京秀域科技文化有限公司 In-water fountain egret demonstrating device
CN106390485A (en) * 2015-07-31 2017-02-15 北京秀域科技文化有限公司 Water-surface demonstrating device
CN109542108A (en) * 2017-09-22 2019-03-29 南京开天眼无人机科技有限公司 A kind of unmanned plane wind resistance patrols winged system
CN209123339U (en) * 2018-09-26 2019-07-19 张天伟 A kind of faucet dynamic kite
KR101950401B1 (en) * 2018-10-02 2019-02-20 플러스파운틴(주) Levitation water fountain apparatus using drone
CN211158609U (en) * 2019-09-24 2020-08-04 杭州西湖喷泉设备成套有限公司 Dance beauty device with phoenix modeling and model steering control system thereof

Also Published As

Publication number Publication date
CN110585748A (en) 2019-12-20

Similar Documents

Publication Publication Date Title
CN105799805B (en) A kind of modularization flight climbing robot
CN103381886B (en) Initiatively variant flapping wing aircraft of a kind of Dynamic and Multi dimensional
CN209757300U (en) Embedded synchronous lifting multi-posture intelligent tail wing of automobile
CN104648667B (en) Aircraft
CN209159998U (en) A kind of bionic flapping-wing flying vehicle
CN107472528B (en) Flapping wing device with passively-turned attack angle and flight control method
CN110585748B (en) Phoenix-shaped stage-art device and model steering control system thereof
CN205642788U (en) Big angle of attack every single move of high -speed wind tunnel developments stall test device
CN104875888A (en) Detachable ring-pillar type hollow unmanned aerial vehicle and operation method thereof
CN104225928A (en) Entertainment device
CN211158609U (en) Dance beauty device with phoenix modeling and model steering control system thereof
CN201108745Y (en) Power kite
CN110371288A (en) One kind is fluttered the adjustable bionic flapping-wing flying vehicle in amplitude angle
CN107031843B (en) A kind of three jet pipes water spray aircraft
CN209290681U (en) VTOL fixed-wing unmanned plane
CN216943500U (en) Bionic jellyfish robot
CN106390484B (en) Fountain egression performance appts in water
CN103158880B (en) Empty sky electric helicopter
JP2021003915A (en) Multicopter
CN108298076A (en) A kind of propulsive mechanism of the mimicry contrary flexure pleat wing
CN210882616U (en) Folding wing mechanism of bionic flapping wing aircraft
CN210924286U (en) Spherical unmanned aerial vehicle system supporting realization of multi-mode control
CN106625710A (en) Robot
CN209662569U (en) Indoor golf simulator
CN104071331B (en) The gyro-stabilized jet airship of a kind of employing

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant