CN204520040U - A kind of model aircraft showing stand - Google Patents
A kind of model aircraft showing stand Download PDFInfo
- Publication number
- CN204520040U CN204520040U CN201420655819.7U CN201420655819U CN204520040U CN 204520040 U CN204520040 U CN 204520040U CN 201420655819 U CN201420655819 U CN 201420655819U CN 204520040 U CN204520040 U CN 204520040U
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- gear
- motor
- turning cylinder
- shaft coupling
- base plate
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Abstract
A kind of model aircraft showing stand, belong to model display bracing frame technical field, comprise longitudinal extension device, up-and-down rod, single-chip microcomputer, controller, cross base plate, pressure sensor, first linear gear, first external gear, first turning cylinder, first shaft coupling, first motor, tripod, gear shaft, internal gear, bearing, 3rd shaft coupling, reducing motor, second turning cylinder, second external gear, second linear gear, transversal stretching device, vehicle wheel frame, wheel, second motor, first support and the second shaft coupling, described two pressure sensors symmetry is arranged on the left and right sides on longitudinal extension device top, longitudinal extension device is arranged on up-and-down rod, up-and-down rod is arranged on gear shaft, the pressure signal that up-and-down rod can be collected according to two pressure sensors carries out the adjustment tilting to realize axial angle, and the center of gravity of this model display frame and model aircraft is overlapped, and solves the problem that model display frame and model aircraft rock because of crank.
Description
Technical field
The utility model relates to a kind of model aircraft showing stand, belongs to model display bracing frame technical field.
Background technology
Model aircraft is with a long history, it produces along with the development of mankind's aviation industry, need when aircraft manufacturing company releases new aircraft to replace true aircraft to show with model aircraft, numerous client is allowed to understand the new aircraft properties released, model aircraft shows too busy to get away bracing frame, the model aircraft showing stand of prior art is all fixed structure, height can not be carried out regulate, the client being not suitable for different height watches model aircraft, and model display frame can not regulate axial angle, and model aircraft is irregularly shaped object, the center of gravity of model aircraft is difficult to find, therefore model aircraft is placed on model display frame, easily make model display frame crank and rock.In order to solve above-mentioned difficulties, needing to develop a energy and regulate height and the model display frame of axial angle can be regulated.
Summary of the invention
The purpose of this utility model is to provide a kind of model aircraft showing stand.
Problem to be solved in the utility model is that the model display frame of prior art can not carry out highly regulating and can not regulate the problem of axial angle.
For realizing the purpose of this utility model, the technical solution adopted in the utility model is:
A kind of model aircraft showing stand, comprises longitudinal extension device, up-and-down rod, single-chip microcomputer, controller, cross base plate, pressure sensor, first linear gear, first external gear, first turning cylinder, first shaft coupling, first motor, tripod, gear shaft, internal gear, bearing, 3rd shaft coupling, reducing motor, second turning cylinder, second external gear, second linear gear, transversal stretching device, vehicle wheel frame, wheel, second motor, bracing frame, second shaft coupling and pillar, described two pressure sensors symmetry is arranged on the left and right sides on longitudinal extension device top, longitudinal extension device is arranged on up-and-down rod, up-and-down rod is arranged on gear shaft, gear shaft overcoat has two internal gears, gear on internal gear and gear shaft coincide mutually, bearing holder (housing, cover) is outside internal gear, bearing is arranged on cross base plate, gear shaft is connected with reducing motor by the 3rd shaft coupling, reducing motor is arranged on cross base plate, single-chip microcomputer and controller are arranged on cross base plate, two pressure sensors are connected with single-chip microcomputer respectively by wire, and single-chip microcomputer is connected with controller by wire, and controller is connected with reducing motor by wire, cross base plate installs four transversal stretching devices, and four transversal stretching devices are symmetrically installed, and four pillar one end are hingedly mounted on cross bottom panel side, and four pillar other ends are arranged on vehicle wheel frame top, and wheel is arranged on vehicle wheel frame.
Described longitudinal extension device comprises the first linear gear, the first external gear, the first turning cylinder, the first shaft coupling, the first motor and tripod, two pressure sensor symmetries are arranged on the left and right sides on the first linear gear top, first linear gear and the first external gear are arranged in up-and-down rod, first external gear is arranged on the first linear gear, first turning cylinder is arranged in the first external gear, first turning cylinder is connected with the first motor by the first shaft coupling, first motor is arranged on tripod, and tripod is arranged on up-and-down rod.
Described transversal stretching device comprises the second turning cylinder, the second external gear, the second linear gear, the second shaft coupling, the second motor and bracing frame, second linear gear and the second external gear are arranged in cross base plate, second external gear is arranged on the second linear gear, second turning cylinder is arranged in the second external gear, second turning cylinder is connected with the second motor by the second shaft coupling, second motor is arranged on bracing frame, and bracing frame is arranged on cross bottom panel side.
The utility model has the advantages that: the pressure signal that up-and-down rod can be collected according to two pressure sensors carries out tilting to realize the adjustment of axial angle, the center of gravity of this model display frame and model aircraft is overlapped, solve the problem that model display frame and model aircraft rock because of crank, avoid model aircraft and fall on the ground; Longitudinal extension device makes the distance between model aircraft and ground adjustable, the client of different height is facilitated to observe model aircraft, transversal stretching device expands the contact area on this model display frame and ground, make this model display frame and model aircraft be in plateau, the model aircraft making this model display frame be applicable to Different Weight uses.
Accompanying drawing explanation
Fig. 1 is the front view of a kind of model aircraft showing stand of the utility model;
Fig. 2 is the cut-away illustration of the front view of a kind of model aircraft showing stand of the utility model longitudinal extension device;
Fig. 3 is the cut-away illustration of the top view of a kind of model aircraft showing stand of the utility model transversal stretching device;
Fig. 4 is the cut-away illustration of the top view of a kind of model aircraft showing stand of the utility model cross base plate;
In figure: 1, longitudinal extension device 2, up-and-down rod 3, single-chip microcomputer 4, controller 5, cross base plate
6, pressure sensor 7, first linear gear 8, first external gear 9, first turning cylinder 10, first shaft coupling
11, the first motor 12, tripod 13, gear shaft 14, internal gear 15, bearing 16, the 3rd shaft coupling
17, reducing motor 18, second turning cylinder 19, second external gear 20, second linear gear 21, transversal stretching device 22, vehicle wheel frame 23, wheel 24, second motor 25, bracing frame 26, second shaft coupling 27, pillar.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further described.
A kind of model aircraft showing stand, comprises longitudinal extension device 1, up-and-down rod 2, single-chip microcomputer 3, controller 4, cross base plate 5, pressure sensor 6, first linear gear 7, first external gear 8, first turning cylinder 9, first shaft coupling 10, first motor 11, tripod 12, gear shaft 13, internal gear 14, bearing 15, 3rd shaft coupling 16, reducing motor 17, second turning cylinder 18, second external gear 19, second linear gear 20, transversal stretching device 21, vehicle wheel frame 22, wheel 23, second motor 24, bracing frame 25, second shaft coupling 26 and pillar 27, described two pressure sensor 6 symmetries are arranged on the left and right sides on longitudinal extension device 1 top, the pressure signal of position collected by pressure sensor 6, longitudinal extension device 1 is arranged on up-and-down rod 2, up-and-down rod 2 is arranged on gear shaft 13, gear shaft 13 overcoat has two internal gears 14, gear on internal gear 14 and gear shaft 13 coincide mutually, bearing 15 is enclosed within outside internal gear 14, bearing 15 is arranged on cross base plate 5, gear shaft 13 is connected with reducing motor 17 by the 3rd shaft coupling 16, reducing motor 17 is arranged on cross base plate 5, single-chip microcomputer 3 and controller 4 are arranged on cross base plate 5, two pressure sensors 6 are connected with single-chip microcomputer 3 respectively by wire, single-chip microcomputer 3 is connected with controller 4 by wire, controller 4 is connected with reducing motor 17 by wire, two pressure sensors 6 by the pressure signal transmission collected to single-chip microcomputer 3, single-chip microcomputer 3 is transferred to controller 4 after analyzing the size of two pressure signals, controller 4 controls reducing motor 17 to the large sideway swivel of pressure signal, driven gear axle 13 is to the large sideway swivel of pressure signal, make up-and-down rod 2 along with gear shaft 13 is to the large lopsidedness of pressure signal, the axial angle realizing up-and-down rod 2 regulates, the center of gravity of this model display frame and model aircraft is overlapped, solve the problem that model display frame and model aircraft rock because of crank, avoid model aircraft to fall on the ground, cross base plate 5 installs four transversal stretching devices 21, four transversal stretching devices 21 are symmetrically installed, four pillar 27 one end are hingedly mounted on cross base plate 5 side, four pillar 27 other ends are arranged on vehicle wheel frame 22 top, wheel 23 is arranged on vehicle wheel frame 22, wheel 23 facilitates this model display frame to move, and pillar 27 can be up cocked, makes wheel 23 leave ground.
Described longitudinal extension device 1 comprises the first linear gear 7, first external gear 8, first turning cylinder 9, first shaft coupling 10, first motor 11 and tripod 12, two pressure sensor 6 symmetries are arranged on the left and right sides on the first linear gear 7 top, the pressure signal of position collected by pressure sensor 6, first linear gear 7 and the first external gear 8 are arranged in up-and-down rod 2, first external gear 8 is arranged on the first linear gear 7, first turning cylinder 9 is arranged in the first external gear 8, first turning cylinder 9 is connected with the first motor 11 by the first shaft coupling 10, first motor 11 is arranged on tripod 12, tripod 12 is arranged on up-and-down rod 2, first motor 11 rotarily drives the first turning cylinder 9 and rotates, first external gear 8 is rotated along with the first turning cylinder 9, and then make the first linear gear 7 or shrink in up-and-down rod 2 or stretch outside up-and-down rod 2, realize the height adjustable of this model display frame, make the distance between model aircraft and ground adjustable, the client of different height is facilitated to observe model aircraft.
Described transversal stretching device 21 comprises the second turning cylinder 18, second external gear 19, second linear gear 20, second shaft coupling 26, second motor 24 and bracing frame 25, second linear gear 20 and the second external gear 19 are arranged in cross base plate 5, second external gear 19 is arranged on the second linear gear 20, second turning cylinder 18 is arranged in the second external gear 19, second turning cylinder 18 is connected with the second motor 24 by the second shaft coupling 26, second motor 24 is arranged on bracing frame 25, bracing frame 25 is arranged on cross base plate 5 side, second motor 24 rotarily drives the second turning cylinder 18 and rotates, second external gear 19 is rotated along with the second turning cylinder 18, and then make the second linear gear 20 or shrink in cross base plate 5 or stretch outside cross base plate 5, expand the contact area on this model display frame and ground, this model display frame and model aircraft is made to be in plateau, the model aircraft making this model display frame be applicable to Different Weight uses.
Using method of the present utility model is: be placed into by model aircraft on this model display frame, two pressure sensors 6 by the pressure signal transmission collected to single-chip microcomputer 3, single-chip microcomputer 3 to be analyzed Signal transmissions after the size of two pressure signals to controller 4, controller 4 controls reducing motor 17 to the large sideway swivel of pressure signal, driven gear axle 13 is to the large sideway swivel of pressure signal, make up-and-down rod 2 along with gear shaft 13 is to the large lopsidedness of pressure signal, in the process that up-and-down rod 2 tilts, two pressure sensor 6 real-time collecting pressure signals, when the pressure signal that two pressure sensors 6 are collected is identical, through single-chip microcomputer 3 analyze after by signal transmission to controller 4, controller 4 controls reducing motor 17 and stops operating, model display frame and model aircraft is made to be in plateau, for the client adapting to different height observes model aircraft, open the first motor 11, first motor 11 rotarily drives the first turning cylinder 9 and rotates, first external gear 8 is rotated along with the first turning cylinder 9, and then make the first linear gear 7 or shrink in up-and-down rod 2 or stretch outside up-and-down rod 2, this model display frame is adjusted to and is applicable to height, model aircraft is in and is applicable to height, rely on wheel 23 this model display frame removable, when the model aircraft heavier-weight shown, pillar 27 is up cocked, make wheel 23 leave ground, open the second motor 24, second motor 24 and rotarily drive the second turning cylinder 18 and rotate, second external gear 19 is rotated along with the second turning cylinder 18, and then the second linear gear 20 is stretched outside cross base plate 5, expand the contact area on this model display frame and ground, make this model display frame and model aircraft be in plateau.
Claims (3)
1. a model aircraft showing stand, comprises longitudinal extension device (1), up-and-down rod (2), single-chip microcomputer (3), controller (4), cross base plate (5), pressure sensor (6), first linear gear (7), first external gear (8), first turning cylinder (9), first shaft coupling (10), first motor (11), tripod (12), gear shaft (13), internal gear (14), bearing (15), 3rd shaft coupling (16), reducing motor (17), second turning cylinder (18), second external gear (19), second linear gear (20), transversal stretching device (21), vehicle wheel frame (22), wheel (23), second motor (24), bracing frame (25), second shaft coupling (26) and pillar (27), it is characterized in that: described two pressure sensor (6) symmetries are arranged on the left and right sides on longitudinal extension device (1) top, longitudinal extension device (1) is arranged on up-and-down rod (2), up-and-down rod (2) is arranged on gear shaft (13), gear shaft (13) overcoat has two internal gears (14), gear on internal gear (14) and gear shaft (13) coincide mutually, bearing (15) is enclosed within internal gear (14) outward, bearing (15) is arranged on cross base plate (5), gear shaft (13) is connected with reducing motor (17) by the 3rd shaft coupling (16), reducing motor (17) is arranged on cross base plate (5), single-chip microcomputer (3) and controller (4) are arranged on cross base plate (5), two pressure sensors (6) are connected with single-chip microcomputer (3) respectively by wire, single-chip microcomputer (3) is connected with controller (4) by wire, controller (4) is connected with reducing motor (17) by wire, upper installation four the transversal stretching devices (21) of cross base plate (5), four transversal stretching devices (21) are symmetrically installed, four pillar (27) one end are hingedly mounted on cross base plate (5) side, four pillar (27) other ends are arranged on vehicle wheel frame (22) top, and wheel (23) is arranged on vehicle wheel frame (22).
2. a kind of model aircraft showing stand according to claim 1, it is characterized in that: described longitudinal extension device (1) comprises the first linear gear (7), first external gear (8), first turning cylinder (9), first shaft coupling (10), first motor (11) and tripod (12), two pressure sensor (6) symmetries are arranged on the left and right sides on the first linear gear (7) top, first linear gear (7) and the first external gear (8) are arranged in up-and-down rod (2), first external gear (8) is arranged on the first linear gear (7), first turning cylinder (9) is arranged in the first external gear (8), first turning cylinder (9) is connected with the first motor (11) by the first shaft coupling (10), first motor (11) is arranged on tripod (12), tripod (12) is arranged on up-and-down rod (2).
3. a kind of model aircraft showing stand according to claim 1, it is characterized in that: described transversal stretching device (21) comprises the second turning cylinder (18), second external gear (19), second linear gear (20), second shaft coupling (26), second motor (24) and bracing frame (25), second linear gear (20) and the second external gear (19) are arranged in cross base plate (5), second external gear (19) is arranged on the second linear gear (20), second turning cylinder (18) is arranged in the second external gear (19), second turning cylinder (18) is connected with the second motor (24) by the second shaft coupling (26), second motor (24) is arranged on bracing frame (25), bracing frame (25) is arranged on cross base plate (5) side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420655819.7U CN204520040U (en) | 2014-11-06 | 2014-11-06 | A kind of model aircraft showing stand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420655819.7U CN204520040U (en) | 2014-11-06 | 2014-11-06 | A kind of model aircraft showing stand |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204520040U true CN204520040U (en) | 2015-08-05 |
Family
ID=53734111
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420655819.7U Expired - Fee Related CN204520040U (en) | 2014-11-06 | 2014-11-06 | A kind of model aircraft showing stand |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204520040U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105935229A (en) * | 2016-06-22 | 2016-09-14 | 无锡德斯凯动力科技有限公司 | Supercharger accessory sale device convenient to use |
| CN108240887A (en) * | 2017-12-27 | 2018-07-03 | 安徽金大仪器有限公司 | A kind of radio data pressure meter with installation auxiliary device |
| CN109489478A (en) * | 2018-12-28 | 2019-03-19 | 中国人民解放军69218部队 | Aerial target display console |
| CN110723376A (en) * | 2018-07-17 | 2020-01-24 | 宁国诚石橡塑制品有限公司 | Classifiable product placing rack for selling rubber products |
| CN111998737A (en) * | 2020-09-03 | 2020-11-27 | 中国人民解放军63921部队 | Carrying running device for firework setting off |
| CN112033228A (en) * | 2020-09-03 | 2020-12-04 | 中国人民解放军63921部队 | Dynamic setting off fireworks tree |
| CN112033229A (en) * | 2020-09-03 | 2020-12-04 | 中国人民解放军63921部队 | Dynamic firework setting off device |
| CN114030804A (en) * | 2021-11-17 | 2022-02-11 | 安徽农业大学 | A can take out fast and transfer goods storage device for in logistics management |
-
2014
- 2014-11-06 CN CN201420655819.7U patent/CN204520040U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105935229A (en) * | 2016-06-22 | 2016-09-14 | 无锡德斯凯动力科技有限公司 | Supercharger accessory sale device convenient to use |
| CN108240887A (en) * | 2017-12-27 | 2018-07-03 | 安徽金大仪器有限公司 | A kind of radio data pressure meter with installation auxiliary device |
| CN110723376A (en) * | 2018-07-17 | 2020-01-24 | 宁国诚石橡塑制品有限公司 | Classifiable product placing rack for selling rubber products |
| CN110723376B (en) * | 2018-07-17 | 2021-08-24 | 宁国诚石橡塑制品有限公司 | Classifiable product placing rack for selling rubber products |
| CN109489478A (en) * | 2018-12-28 | 2019-03-19 | 中国人民解放军69218部队 | Aerial target display console |
| CN109489478B (en) * | 2018-12-28 | 2023-09-01 | 中国人民解放军69218部队 | Aerial target display console |
| CN111998737A (en) * | 2020-09-03 | 2020-11-27 | 中国人民解放军63921部队 | Carrying running device for firework setting off |
| CN112033228A (en) * | 2020-09-03 | 2020-12-04 | 中国人民解放军63921部队 | Dynamic setting off fireworks tree |
| CN112033229A (en) * | 2020-09-03 | 2020-12-04 | 中国人民解放军63921部队 | Dynamic firework setting off device |
| CN112033229B (en) * | 2020-09-03 | 2022-12-20 | 中国人民解放军63921部队 | Dynamic firework setting off device |
| CN114030804A (en) * | 2021-11-17 | 2022-02-11 | 安徽农业大学 | A can take out fast and transfer goods storage device for in logistics management |
| CN114030804B (en) * | 2021-11-17 | 2022-09-23 | 安徽农业大学 | A can take out fast and transfer goods storage device for in logistics management |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150805 Termination date: 20151106 |
|
| EXPY | Termination of patent right or utility model |