CN204352548U - Model airship and wing - Google Patents
Model airship and wing Download PDFInfo
- Publication number
- CN204352548U CN204352548U CN201420828762.6U CN201420828762U CN204352548U CN 204352548 U CN204352548 U CN 204352548U CN 201420828762 U CN201420828762 U CN 201420828762U CN 204352548 U CN204352548 U CN 204352548U
- Authority
- CN
- China
- Prior art keywords
- wing
- airship
- cylinder
- side plate
- model
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of model airship and wing, wherein wing comprises the wing-body be coupling in airship main body, can relative to airship main body adduction and expansion; The movable part of wing nose, at least can rotate to side relative to wing-body; Also be provided with at least one in wing-body can rotate relative to wing-body thus open the hatch door in hatch door hole; The bottom of airship is also provided with emitting structural and offers corresponding opening, and emitting structural comprises the gun barrel being concealed in opening inner side, and gun barrel is coupling in airship main body, can produce relative to opening and take in.Model airship of the present utility model, not only wing entirety can be received relative to the exhibition of airship main body, wing nose can rotate relative to wing-body, the state that hatch door on wing also can rotate relative to wing-body, realize closedown and open, also has the gun barrel rotated relative to airship body, and airship entirety also can 360 ° of rotations, and there is lifting astrodome, there is high artificial activity function.
Description
Technical field
The utility model relates to a kind of airship model and wing thereof.
Background technology
Along with the progress of science and technology, the mankind have been no longer unreachable dreams by airship exploration of the universe.And model airship is as the model of real airship, be also subject to the welcome in market with the identity of toy or exhibit and teaching equipment.But existing model airship, technology only rests on simple outward appearance and imitates, and wing is relative to the main body of airship and itself to be static structure simulation poor.
Utility model content
A kind of model airship wing, is arranged on airship body side, comprises sheet or tabular wing-body, it is characterized in that, described wing-body is coupling in airship main body, and is connected with one first drive unit, can relative to described airship main body adduction and expansion under described first drive unit drives; Described wing-body comprises wing-body and is located at the movable part of wing-body front end, and described movable part is coupling in wing-body, and is connected with one second drive unit, at least can rotate to side under described second drive unit drives relative to wing-body; At least one hatch door hole is provided with in described wing-body, and in hatch door hole described at least one, be equipped with a hatch door, described cabin door shaft is connected to wing-body, and be connected with one the 3rd drive unit, can rotate relative to described wing-body thus open described hatch door hole under described 3rd drive unit drives; The bottom of described airship is provided with emitting structural and offers corresponding opening, described emitting structural comprises the gun barrel being concealed in described opening inner side, described gun barrel is coupling in airship main body, and be connected with a four-drive device, can produce relative to described opening and take under described four-drive device drives.
Preferably, described first drive unit is the first cylinder that axis being parallel is arranged in described wing-body in-plane, and the axis of described first cylinder and airship main body axis in a certain angle, one end of described first cylinder is coupling in described airship main body, and the other end connects described wing-body by one first oscillating bearing.
Preferably, described movable part can swing between wing-body both sides.
Preferably, described second drive unit comprises two the second cylinders, and the second drive unit connects described movable part by a second joint bearing, and drives described movable part to rotate relative to wing-body.
Preferably, two described second cylinders join end to end setting, and preceding described second cylinder connects described movable part by described second joint bearing.
Preferably, described at least one, the upper cover of piston rod of the second cylinder is provided with spring.
Preferably, described 3rd drive unit is the 3rd cylinder be located at inside hatch door, and described 3rd cylinder-bore axis direction is vertical relative to the rotor shaft direction of wing-body with hatch door, one end of described 3rd cylinder is coupling in described wing-body, and the other end connects described hatch door by a three-knuckle bearing.
Preferably, described four-drive device comprises a four-cylinder, and described four-cylinder connects described gun barrel by one the 4th oscillating bearing, and drives described gun barrel to rotate relative to the opening surface of described opening.
Preferably, described gun barrel comprises at least one launching pod, and described launching pod is connected with one the 5th drive unit, can do under described 5th drive unit drives near and the motion of the position that is coupling away from described gun barrel and airship main body.
Preferably, described 5th drive unit comprises a motor, and described motor connects and drives a screw rod, described launching pod comprise one to coordinate with described screw rod, can along the reciprocating slide rail of screw rod and the shell being fixed on described slide rail.
The utility model also provides a kind of model airship with the utility model model airship wing.
This model airship comprises airship main body and the support for hanging described airship main body, described support comprises substrate, be fixed on the first side plate on described substrate length direction successively, second side plate, hollow circular tube, 3rd side plate, 4th side plate and the 5th side plate, the first stiffener is fixed with between described first side plate and described second side plate, described hollow circular tube is vertically arranged, the second stiffener is fixed with between one side of described hollow circular tube and described second side plate, another side of described hollow circular tube passes described 3rd side plate and fixes with described 3rd side plate, the 3rd stiffener is fixed with between another side of described hollow circular tube and described 4th side plate, described 3rd side plate is fixed with motor, the rotating shaft of described motor is connected with the first gear, described hollow circular tube is fixed with the second gear, described first gear and described second gear engage each other, the upper end of described hollow circular tube is fixed with swivel joint, the lower end of described substrate is fixed with the first counter weight device, be positioned at the second counter weight device below described first counter weight device.
Preferably, described first counter weight device comprises the first pedestal, the first balance weight assembly be arranged on described first pedestal, the lower end of described first pedestal has the first T-shaped groove, described first balance weight assembly comprises the first T-shaped block, is fixed on the first ballast box of described first T-shaped block lower end, and the upper end of described first T-shaped block is inserted in described first T-shaped groove.
Preferably, described second counter weight device comprises the second pedestal, the second balance weight assembly be arranged on described second pedestal, the lower end of described second pedestal has the second T-shaped groove, described second balance weight assembly comprises the second T-shaped block, is fixed on the second ballast box of described second T-shaped block lower end, and the upper end of described second T-shaped block is inserted in described second T-shaped groove.
Preferably, the height of described first side plate, the second side plate, the 3rd side plate, the 4th side plate and the 5th side plate increases successively.
Preferably, the cross section of described first side plate, the second side plate, the 3rd side plate, the 4th side plate and the 5th side plate is all curved.
Preferably, the front end of described first side plate is fixed with the 4th stiffener, and lower end and the described substrate of described 4th stiffener are fixed.
Preferably, the front end of described 5th side plate is fixed with five stiffeners, and lower end and the described substrate of described 5th stiffener are fixed.
Preferably, the upper end of described 3rd side plate is fixed with level board, and described motor is fixed on described level board.
Preferably, described substrate is fixed with multiple mounting hole.
Preferably, also comprise the lifting assembly being located at airship main body and the circular cylinder body be arranged on described lifting assembly, described lifting assembly comprises level board, lower horizontal board and connect two side plates of described upper level board and described lower horizontal board, the pair of horns of described upper level board is all fixed with round bump, intermediate plate is provided with between described upper level board and described lower horizontal board, support plate is fixed with between two described side plates, described support plate is positioned at the top of described intermediate plate, described support plate is fixed with motor, the rotating shaft of described motor is stretched out described upper level board and fixes with described circular cylinder body, described intermediate plate is fixed with cylinder, described cylinder is connected with described lower horizontal board, the bottom of described circular cylinder body has circular groove, described round bump is inserted in described circular groove, the sidewall of described circular cylinder body is provided with dodge gate.
Preferably, the pair of horns of described intermediate plate is all fixed with guide pillar, one end of described guide pillar is through described lower horizontal board.
Preferably, the pair of horns of described lower horizontal board is all fixed with bearing, one end of described guide pillar is successively through described bearing, lower horizontal board.
Preferably, the upper end of described intermediate plate is fixed with two the first sleeves, and lower end is fixed with two the second sleeves, and the other end of described guide pillar is successively through described second sleeve, the first sleeve.
Preferably, described upper level board, lower horizontal board and two described side plates are one-body molded.
Preferably, two wide sides of described intermediate plate are fixed with two journal stirrups respectively, and described journal stirrup has installing hole.
Preferably, the two ends of described upper level board, lower horizontal board and intermediate plate are all in circular arc.
The beneficial effect that the utility model reaches:
1. model airship wing of the present utility model, not only wing entirety can be received relative to the exhibition of airship main body, and wing nose can rotate relative to wing-body, the state that hatch door on wing also can rotate relative to wing-body, realize closedown and open, in addition, also have the gun barrel rotated relative to airship body, there is high artificial activity function, both can as toy, again can as teaching aid, exhibit.
2. arrange the first cylinder and transmit motion to wing-body by oscillating bearing, then structure is simple, and flexible movements, spreading angle is stablized controlled.Especially design activity portion can swing between wing-body both sides, then can complete more actions, simulated effect is better.
3. be provided with the drive unit of two cylinders and transmit motion to movable part by oscillating bearing, then structure is simple, and flexible movements, slow-roll stabilization is controlled.Especially two cylinders join end to end setting, then only need install oscillating bearing between anterior cylinder and movable part, namely by the cooperation of two cylinders realize wing nose relative to wing-body upwards rotation, rotate and reset.
4. establish spring at the upper cover of piston rod of at least one cylinder, then can increase power-assisted when cylinder driven forward wing nose overturns on the one hand, position-limiting action can be played when cylinder reclaims and drives wing nose reverse flip on the other hand.
5. arranging cylinder drives oscillating bearing to transmit motion to hatch door, and structure is simple, and flexible movements, slow-roll stabilization is controlled.
6. arrange cylinder and transmit motion to gun barrel by oscillating bearing, then structure is simple, and flexible movements, rotational angle is stablized controlled.
7. gun barrel is arranged on to rotate on basis and can stretches out the launching pod with indentation further, then can more real simulation emission state, and carry out multi-functional, fidelity is high.Especially the launching pod of two self-movements, can control similar and different action step, and multi-emitting cabin that is virtually reality like reality coordinates transmitting situation.
8. arrange motor as the second drive unit, with the launching pod of screw drive with slide rail, then structure is simple, easily makes, simultaneously having stable behavior, easily control.
9. hang the support of airship, side plate is vertical with stiffener to be arranged, stiffener is arranged on the middle part of side plate, not only firm, and have headspace, some accessories can be filled, avoid causing interference, be fully used in space, can realize 360 ° of rotations, omnibearing displaying is arranged on the parts on skeleton simultaneously, be provided with the first counter weight device and the second counter weight device in addition, by the adjustment of the first counter weight device and the second counter weight device, the center of gravity of substrate is positioned on the axis of hollow circular tube all the time, improves stability and the service life of skeleton.
10. the circular cylinder body be arranged on lifting assembly can be used as astrodome and holds facilities for observation, and avoid facilities for observation to skid off in circular cylinder body, circular cylinder body can realize 360 degree of rotations, observes from multi-angle, makes to observe accurately comprehensively.
Accompanying drawing explanation
Fig. 1 is the connection diagram of wing-body and airship main body in the utility model preferred embodiment;
Fig. 2 is the enlarged diagram of the A of local shown in Fig. 1;
Fig. 3 is the connection diagram of wing-body and movable part in the utility model preferred embodiment;
Fig. 4 is the enlarged diagram of the second drive unit in Fig. 3;
Fig. 5 is the position signal of hatch door on wing-body in the utility model preferred embodiment;
Fig. 6 is the connection diagram of hatch door and drive unit in the utility model preferred embodiment;
Fig. 7 is the connection top view of hatch door and drive unit in the utility model preferred embodiment;
Fig. 8 is the schematic diagram of the utility model preferred embodiment base plate and airship bottom part body position relationship;
Fig. 9 is the side view of emitting structural in the utility model preferred embodiment;
Figure 10 is the side view of the utility model preferred embodiment emitting structural inside;
Figure 11 is the stereogram of the utility model preferred embodiment emitting structural inside;
Figure 12 is the structural representation of the support of preferred embodiment of the present utility model;
Figure 13 is the front view that preferred embodiment of the present utility model rotates skeleton;
Figure 14 is the left view that the support of preferred embodiment of the present utility model is connected with the first counter weight device, the second counter weight device;
Figure 15 is the top view of the support of preferred embodiment of the present utility model;
Figure 16 is the front view of preferred embodiment bogey of the present utility model;
The structural representation that Figure 17 is the lifting assembly of preferred embodiment of the present utility model, connect between intermediate plate and cylinder;
Wherein: 2, airship main body, 22, opening, 4, wing-body, 41, wing skeleton, 412, main bone, 414, secondary bone, 42, panel, 43, wing-body, 432, hatch door hole, 44, movable part, 442, metallic plate, 444, panel, 45, hatch door, 452, metallic plate, 454, panel, 46, base plate, 47, launching pod, 472, slide rail, 474, shell, 48, metal frame, 482, metallic plate, 484, connecting plate, 5, first drive unit, 52, first cylinder, 54, first oscillating bearing, 6, second drive unit, 62, hinge, 64, second cylinder, 642, piston rod, 644, cylindrical shell, 66, second cylinder, 662, piston rod, 68, second joint bearing, 684, U-shaped frame, 686, U-shaped frame, 69, spring, 7, 3rd drive unit, 72, 3rd cylinder, 74, three-knuckle bearing, 76, hinge, 8, four-drive device, 82, hinge, 822, rotating shaft, 84, four-cylinder, 86, 4th oscillating bearing, 9, 5th drive unit, 92, motor, 94, screw rod,
321, substrate, 322, first side plate, 323, second side plate, 324, hollow circular tube, 325, 3rd side plate, 326, 4th side plate, 327, 5th side plate, 328, first stiffener, 329, second stiffener, 341, 3rd stiffener, 342, motor, 343, rotating shaft, 344, first gear, 345, second gear, 346, swivel joint, 347, first pedestal, 348, first T-shaped groove, 349, first T-shaped block, 361, first ballast box, 362, second pedestal, 363, second T-shaped groove, 364, second T-shaped block, 365, second ballast box, 366, 4th stiffener, 367, 5th stiffener, 368, level board, 369, mounting hole,
121, circular cylinder body, 122, upper level board, 123, lower horizontal board, 124, side plate, 125, round bump, 126, intermediate plate, 127, support plate, 128, motor, 129, rotating shaft, 141, cylinder, 142, circular groove, 143, dodge gate, 144, guide pillar, 145, bearing, the 146, first sleeve, 147, the second sleeve, 148, journal stirrup, 149, installing hole.
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is further described.Following examples only for clearly the technical solution of the utility model being described, and can not limit protection domain of the present utility model with this.
As shown in figs. 1-11, a kind of model airship wing, is arranged on airship main body 2 sidepiece, comprise sheet or tabular wing-body 4, wing-body 4 is coupling in airship main body 2, and is connected with one first drive unit 5, can relative to airship main body 2 adduction and expansion under the first drive unit 5 drives.
Concrete, wing-body 4 comprises wing skeleton 41 and is wrapped in the panel 42 of wing skeleton 41 outside.Wing-body 4 is coupling by wing skeleton 41 and airship main body 2 on the one hand, and wing-body 4 also connects the first drive unit 5 by wing skeleton 41 on the other hand, and wing skeleton 41 and panel 42 can synchronous axial system.First drive unit 5 is specially the first cylinder 52 that axis being parallel is arranged in wing-body 4 in-plane, and the axis of the first cylinder 52 and airship main body 2 axis C in a certain angle, one end of first cylinder 52 is coupling in airship main body 2, and the other end connects the wing skeleton 41 of wing-body 4 by one first oscillating bearing 54.
Wing skeleton 41 comprises three respectively by the main bone 412 extended near airship main body 2 one end away from airship main body 2 one end, and the secondary bone 414 of each main bone 412 of some connections.This structure both saved material while increase wing intensity, can abdicate again space for arranging other wing structure.
Wing-body 4 comprises wing-body 43 and is located at the sheet movable part 44 of wing-body 43 front end, movable part 44 is coupling in wing-body 43, and be connected with one second drive unit 6, can rotate both sides up and down relative to wing-body 43 respectively under the second drive unit 6 drives, thus can swing between wing-body 43 both sides.
Movable part 44 specifically comprise as skeleton metallic plate 442 and be arranged on the panel 444 of metallic plate 442 both sides, movable part 44 connects the second drive unit 6 by metallic plate 442, and panel 444 with metallic plate 442 is fixing can synchronous axial system.Metallic plate 442 and wing-body 43 are coupling especially by hinge 62, and namely wing-body 43 is fixed in one end of hinge 62, and the other end is fixed on metallic plate 442.Second drive unit 6 specifically comprises two the second cylinders 64,66, and the second drive unit 6 is by the metallic plate 442 of second joint bearing 68 movable part connecting 44, and drives movable part 44 to rotate relative to wing-body 43.More specifically, two the second cylinders 64,66 join end to end setting, and preceding second cylinder 64 is by second joint bearing 68 movable part connecting 44.
The axis direction of the second cylinder 64 and the second cylinder 66 overlaps, relative to metallic plate 442, second cylinder 64 of closer metallic plate 442 is front, compared with the second cylinder 66 away from metallic plate 442 rear, and the cylindrical shell 664 of the second cylinder 66 is fixed on a U-shaped frame 686, cylindrical shell 664 is placed between U-shaped frame 684 two ends, and piston rod 662 stretches out forward U-shaped frame 686, and the second cylinder 64 is also fixed on a U-shaped frame 684 in an identical manner.Concrete, U-shaped frame 686 is fixed on wing-body 43, its piston rod 662 of the second cylinder 66 of rear end fixed thereon connects the tail end of U-shaped frame 686, and its piston rod 642 front end of the second cylinder 64 of the front end that U-shaped frame 684 is arranged is connected with metallic plate 442 by second joint bearing 68.Therefore, the drive unit driven forward metallic plate 442 that two second cylinders 64,66 form can make metallic plate 442 wrap page 62 rotor shaft direction together with panel 444 and be rotated down motion; Pull back metallic plate 442 metallic plate 442 can be made together with panel 444 to wrap page 62 rotor shaft direction rotate up motion.
More specifically, on the piston rod 642 of the second cylinder 64 and the piston rod 662 of the second cylinder 66 be arranged with spring 69 respectively.Then can increase power-assisted when the second cylinder 64 and/or the second cylinder 66 driven forward movable part 44 overturn, play position-limiting action when the second cylinder 64 and/or the second cylinder 66 reclaim and drive movable part 44 reverse flip, thus can flip angle be controlled.Spring 69 according to two the second cylinders coordinates, and the angle that movable part 44 rotates respectively to both sides relative to wing-body 43 can be the same or different.It is 60 ° that the setting of preferred spring 69 can control the amplitude peak that movable part 44 rotates to side relative to wing-body 43, then fidelity is high.
Two hatch door holes 432 are provided with in wing-body 43, and in each hatch door hole 432, be equipped with the hatch door 45 of a type cooperation, hatch door 45 is coupling in wing-body 43, and be connected with one the 3rd drive unit 7, can rotate relative to wing-body 43 thus open hatch door 45 hole 432 under the 3rd drive unit 7 drives.
Hatch door 45 specifically comprise as skeleton metallic plate 452 and be arranged on the panel 454 of metallic plate 452 both sides, and metallic plate 452 and panel 454 can synchronous axial system.3rd drive unit 7 is specially two the 3rd cylinders 72 be located at inside hatch door 45, and the 3rd cylinder 72 axis direction is vertical relative to the rotor shaft direction of wing-body 43 with hatch door 45, one end of 3rd cylinder 72 is coupling in the wing skeleton 41 of wing-body 43, and the other end connects the metallic plate 452 of hatch door 45 by a three-knuckle bearing 74.Hatch door 45 is coupling in wing-body 43 by hinge 76 simultaneously, often fans hatch door 45 and arranges two hinges 76, improve stability.
Two fan hatch doors 45 are arranged on wing-body 43 relative to staggering before and after airship heading, and two the 3rd cylinders 72 of drive unit drive corresponding hatch door 45 to open and close respectively.Can further improve fidelity, simultaneously two fan hatch doors 45 are controlled by independently the 3rd cylinder 72 respectively, can realize asynchronous behavior, increase the kind of molar behavior set pattern.
Hatch door 45 is specially large, the middle little plane dumb-bell shape in two ends.Then because the shape in hatch door hole 432 also matches with it, both have certain grafting to coordinate at in-plane, thus when ensureing that hatch door 45 is closed and hatch door hole 432 contacts more closely, stablizes.The larger two ends of preferred hatch door 45 separately width be the 1.5-3 of less middle part doubly, two ends length is respectively the 1/4-1/3 of hatch door 45 overall length.
The bottom of airship is provided with emitting structural and offers corresponding opening 22, emitting structural comprises the gun barrel be concealed in inside opening 22, described gun barrel is coupling in airship main body 2, and is connected with a four-drive device 8, can produce relative to opening 22 and take under four-drive device 8 drives.
Emitting structural also comprises the base plate 46 be located at outside gun barrel, and four-drive device 8 drives gun barrel and base plate 46 synchronous axial system, and is concealed in opening 22 when gun barrel goes to, and base plate 46 can closing openings 22.Gun barrel specifically comprises two launching pods 47 setting up and down, and launching pod 47 is connected with one the 5th drive unit 9, can do under the 5th drive unit 9 drives near and the motion of the position that is coupling away from gun barrel and airship main body 2.And two launching pods 47 connected 5th drive unit 9 is separate separately.More specifically, gun barrel comprises a metal frame 48, metal frame 48 is made up of double layer of metal plate 482, be connected by vertical connecting plate 484 between double layer of metal plate 482, the lower metal plate 482 of metal frame 48 is fixed on base plate 46, and upper and lower two launching pods 47 are separately positioned on the top and bottom of upper strata metallic plate 482.Gun barrel is coupling in airship main body 2 by metal frame 48, is coupling to be fixed on metal frame 48 with one end of hinge 82, and the other end is fixed on airship main body 2, forms the rotating shaft 822 that gun barrel rotates relative to airship main body 2.
Four-drive device 8 comprises a four-cylinder 84, and four-cylinder 84 connects gun barrel and base plate 46 by one the 4th oscillating bearing 86, and drives gun barrel and base plate 46 relative to the opening surface synchronous axial system of opening 22.
5th drive unit 9 comprises a motor 92, and motor 92 axle and four-cylinder 84 axis being parallel are arranged.Motor 92 is fixed on corresponding metallic plate 482, connects and drive a screw rod 94, launching pod 47 comprise one to coordinate with screw rod 94, can along the reciprocating slide rail 472 of screw rod 94 and the shell 474 being fixed on slide rail 472.Therefore, when motor 92 works drive screw rod 94 rotate corresponding slide rail 472 can be made to move back and forth thus realize corresponding launching pod 47 relative to rotating shaft 822 lean on into and away from action, launching pod 47 exceeds base plate 46 lower limb away from moving to relative to base plate 46 during rotating shaft 822, thus imitates this state being more conducive to occur of prototype.It is contrary that turning to of two motors 92 is set further, make two launching pods 47 do near and motion away from rotating shaft 822 time direction contrary.When then can ensure launching pod 47 action, multiple times even always has a launching pod 47 to stretch out base plate 46 lower limb, be in preferably emission state in any time gun barrel.
As shown in figs. 12-15, a kind of model airship of the present utility model, comprise airship main body 2 and the rotation skeleton for hanging airship main body 2, rotate skeleton and specifically comprise the skeleton that support is also airship main body 2, support comprises substrate 321, be fixed on the first side plate 322 on substrate 321 length direction successively, second side plate 323, hollow circular tube 324, 3rd side plate 325, 4th side plate 326 and the 5th side plate 327, the first stiffener 328 is fixed with between first side plate 322 and the second side plate 323, first side plate 322, first stiffener 328 and the second side plate 323 are in I-shape construction, hollow circular tube 324 is vertically arranged, the second stiffener 329 is fixed with between one side of hollow circular tube 324 and the second side plate 323, another side of hollow circular tube 324 passes the 3rd side plate 325 and fixes with the 3rd side plate 325, the 3rd stiffener 341 is fixed with between another side of hollow circular tube 324 and the 4th side plate 326, 3rd side plate 325 is fixed with motor 342, the rotating shaft 343 of motor 342 is connected with the first gear 344, hollow circular tube 324 is fixed with the second gear 345, first gear 344 and the second gear 345 engage each other, the number of teeth of the first gear 344 is less than the number of teeth of the second gear 345, the upper end of hollow circular tube 324 is fixed with swivel joint 346, the lower end of substrate 321 is fixed with the first counter weight device, be positioned at the second counter weight device below the first counter weight device.
The utility model preferably the first counter weight device comprises the first pedestal 347, be arranged on the first balance weight assembly on the first pedestal 347, the lower end of the first pedestal 347 has the first T-shaped groove 348, first balance weight assembly comprises the first T-shaped block 349, be fixed on the first ballast box 361 of the first T-shaped block 349 lower end, the balancing weight of different size can be placed in first ballast box 361, be convenient to regulate balance weight, the upper end of the first T-shaped block 349 is inserted in the first T-shaped groove 348, when the first T-shaped block 349 is subject to extraneous thrust, can slide in the upper end of the first T-shaped block 349 in the first T-shaped groove 348.
The utility model preferably the second counter weight device comprises the second pedestal 362, be arranged on the second balance weight assembly on the second pedestal 362, second pedestal 362 is in concave shape, avoid causing interference to the first counter weight device, the lower end of the second pedestal 362 has the second T-shaped groove 363, second balance weight assembly comprises the second T-shaped block 364, be fixed on the second ballast box 365 of the second T-shaped block 364 lower end, the balancing weight of different size can be placed in second ballast box 365, be convenient to regulate balance weight, the upper end of the second T-shaped block 364 is inserted in the second T-shaped groove 363, when the second T-shaped block 364 is subject to extraneous thrust, can slide in the upper end of the second T-shaped block 364 in the second T-shaped groove 363.
As shown in figure 13, the height of the utility model preferably the first side plate 322, second side plate 323, the 3rd side plate 325, the 4th side plate 326 and the 5th side plate 327 increases successively, is convenient to close with the upper cover matching form of the airship that will show.
In order to avoid stress is concentrated, extend service life of skeleton, the cross section of this utility model preferably the first side plate 322, second side plate 323, the 3rd side plate 325, the 4th side plate 326 and the 5th side plate 327 is all curved.
In order to improve the overall steadiness of skeleton, the front end of preferred the first side plate 322 of this utility model is fixed with the lower end of the 4th stiffener the 366, four stiffener 366 and substrate 321 is fixed.
The front end of preferred the 5th side plate 327 of the utility model is fixed with the lower end of five stiffener the 50, five stiffeners 367 and substrate 321 is fixed, and skeleton is firmly overall.
The upper end of preferred the 3rd side plate 325 of the utility model is fixed with level board 368, and motor 342 is fixed on level board 368.
For the ease of installing other accessory, the utility model preferable substrate 321 is fixed with multiple mounting hole 369.
As shown in figs. 16-17, the utility model model airship preferably also comprises the bogey being located at airship main body 2.Bogey specifically comprises lifting assembly and is arranged on the circular cylinder body 121 on lifting assembly, circular cylinder body 121 is as astrodome, bottom is solid construction, upper interior portion is hollow structure, lifting assembly comprises level board 122, two side plates 124 of lower horizontal board 123 and the upper level board 122 of connection and lower horizontal board 123, the pair of horns of upper level board 122 is all fixed with round bump 125, intermediate plate 126 is provided with between upper level board 122 and lower horizontal board 123, upper level board 122 is identical with size with the shape of lower horizontal board 123, the length of intermediate plate 126 is greater than the length of level board 122, support plate 127 is fixed with between two side plates 124, support plate 127 is positioned at the top of intermediate plate 126, support plate 127 is fixed with motor 128, motor 128 can be pulse motor, first work after a period of time and stop a period of time, and then work a period of time, so repeatedly, the rotating shaft 129 of motor 128 is stretched out level board 122 and is fixed with circular cylinder body 121, intermediate plate 126 is fixed with cylinder 141, cylinder 141 is connected with lower horizontal board 123, the bottom of circular cylinder body 121 has circular groove 142, round bump 125 is inserted in circular groove 142, the sidewall of circular cylinder body 121 is provided with dodge gate 143, the facilities for observation of multiple observation external world situation can be placed in circular cylinder body 121, such as video camera, facilities for observation can be stablized and is located in circular cylinder body 121, the rotating shaft 129 of motor 128 can drive circular cylinder body 121 to carry out 360 degree of rotations, be convenient to the extraneous circumstance observing diverse location place, observe accurately comprehensively.
The pair of horns of the preferred intermediate plate 126 of the utility model is all fixed with guide pillar 144, and one end of guide pillar 144 is through lower horizontal board 123, and in realization, level board 122 and lower horizontal board 123 vertically move.
The pair of horns of the preferred lower horizontal board 123 of the utility model is all fixed with bearing 145, and one end of guide pillar 144 is successively through bearing 145, lower horizontal board 123.
In order to extend the service life of guide pillar 144, guide pillar 144 stress is avoided to concentrate, the upper end of the preferred intermediate plate 126 of the utility model is fixed with two the first sleeves 146, and lower end is fixed with two the second sleeves 147, and the other end of guide pillar 144 is successively through the second sleeve 147, first sleeve 146.
It is one-body molded that the utility model preferably goes up level board 122, lower horizontal board 123 and two side plates 124, improves the steadiness of lifting assembly.
Fixing for the ease of intermediate plate 126, two wide sides of the preferred intermediate plate of the utility model 126 are fixed with two journal stirrups 34 respectively, journal stirrup 34 have installing hole 36.
In order to avoid causing interference to other parts, the utility model preferably goes up the two ends of level board 122, lower horizontal board 123 and intermediate plate 126 all in circular arc.
The various simulated actions processes of the utility model model airship are introduced in citing below, but are only embodiment and are not construed as limiting the utility model.
Swivel joint 346 upper end of the utility model embodiment model airship is fixed on the ceiling, swivel joint 346 can rotate relative to ceiling, promote the first T-shaped block 349, second T-shaped block 364, the center of gravity of substrate 321 is made to be positioned on the axis of hollow circular tube 324 all the time, starter motor 342, motor 342 drives the first gear 344 to rotate by rotating shaft 343, first gear 344 drives the second gear 345 to rotate, second gear 345 drives hollow circular tube 324 to rotate, thus realizes 360 ° of rotations of airship main body 2.
The action of taking down the exhibits of wing-body 4.It is outside that first cylinder 52 promotes wing-body 4, then wing-body 4 launches gradually relative to airship main body 2, to the first cylinder 52 cannot continue to promote wing-body 4 again, then the first cylinder 52 reclaims and pulls wing-body 4 inside, then wing-body 4 gets back to reset condition relative to airship main body 2 adduction to the first cylinder 52.
Wing nose movable part 44 action.First the whole movable part 44 of front end second cylinder 64 piston rod 642 driven forward metallic plate 482 wraps page 62 rotor shaft direction and is rotated down to turning over 10 ° of angles relative to initial planar; Then, rear end second cylinder 66 piston rod 662 pulls back front end second cylinder 64 cylindrical shell 644, make front end second cylinder 64 drive movable part 44 to wrap page 62 rotor shaft direction backward to rotate up, and when the stroke that distance counteracting front end second cylinder 64 that rear end second cylinder 66 is advanced backward is initially pushed ahead, movable part 44 resets, second cylinder 66 piston rod 662 continues to pull the second cylinder 64 to drop back, then movable part 44 continues upwards to turn to and turns over 60 ° of angles relative to described initial planar.Repeat the swing that this process can realize movable part 44.
Wing door 45 action.The metallic plate 482 of each 3rd cylinder 72 driven forward hatch door 45, then corresponding hatch door 45 wraps page 76 rotor shaft direction and is rotated down motion, and hatch door 45 is opened: the 3rd cylinder 72 reclaims and hatch door 45 is recovered and the conplane state of wing-body 43 afterwards.In whole process, two the 3rd cylinder 72 synchronization actions, make two fan hatch doors 45 also synchronous opening/closing, are independent of each other.
The action of emitting structural.First, four-cylinder 84 promotes metal frame 48 backward and makes gun barrel and base plate 46 be rotated down to gun barrel and stretch out opening in 822 directions around the shaft, then, under motor 92 drives, in gun barrel, launching pod 47 starts away from the reciprocating motion with close rotating shaft 822, on, lower launching pod 47 alternately stretches out base plate 46 lower limb, after the above-mentioned reciprocating motion of several times, a launching pod 47 rests on the state of stretching out base plate 46 lower limb, now controlling four-cylinder 84 makes gun barrel 822 swing up and down around the shaft together with base plate 46, latter two launching pod 47 is all regained, gun barrel entirety and base plate 46 also return back to gun barrel and hide inside opening 22, and base plate 46 closing any opening 22.
The action of astrodome.Facilities for observation is placed in circular cylinder body 121, lower horizontal board 123 is positioned on a brace table, cylinder 141 starts, lower horizontal board 123 is driven to move upward, lower horizontal board 123 is moved upward along guide pillar 144 by bearing 145, thus drive the circular cylinder body 121 on upper level board 122 to move upward, after certain stroke, circular cylinder body 121 stretches out outside housing, now can observe, motor 128 starts, rotating shaft 129 drives circular cylinder body 121 to carry out 360 degree of rotations, after a period of time, motor 128 quits work, after stopping a period of time, motor 128 works on again, that the situation in the external world is observed is accurately comprehensive.When circular cylinder body 121 is recovered in housing by needs, cylinder 141 resets, lower horizontal board 123 is driven to move downward, lower horizontal board 123 is moved downward along guide pillar 144 by bearing 145, thus drive the circular cylinder body 121 on upper level board 122 to move downward, after certain stroke, circular cylinder body 121 is received in housing.
The above is only preferred embodiment of the present utility model; should be understood that; for those skilled in the art; under the prerequisite not departing from the utility model know-why; can also make some improvement and distortion, these improve and distortion also should be considered as protection domain of the present utility model.
Claims (10)
1. a model airship wing, is arranged on airship body side, comprises sheet or tabular wing-body, it is characterized in that, described wing-body is coupling in airship main body, and is connected with one first drive unit, can relative to described airship main body adduction and expansion under described first drive unit drives; Described wing-body comprises wing-body and is located at the movable part of wing-body front end, and described movable part is coupling in wing-body, and is connected with one second drive unit, at least can rotate to side under described second drive unit drives relative to wing-body; At least one hatch door hole is provided with in described wing-body, and in hatch door hole described at least one, be equipped with a hatch door, described cabin door shaft is connected to wing-body, and be connected with one the 3rd drive unit, can rotate relative to described wing-body thus open described hatch door hole under described 3rd drive unit drives; The bottom of described airship is provided with emitting structural and offers corresponding opening, described emitting structural comprises the gun barrel being concealed in described opening inner side, described gun barrel is coupling in airship main body, and be connected with a four-drive device, can produce relative to described opening and take under described four-drive device drives.
2. a kind of model airship wing according to claim 1, it is characterized in that, described first drive unit is the first cylinder that axis being parallel is arranged in described wing-body in-plane, and the axis of described first cylinder and airship main body axis in a certain angle, one end of described first cylinder is coupling in described airship main body, and the other end connects described wing-body by one first oscillating bearing.
3. a kind of model airship wing according to claim 1, it is characterized in that, described second drive unit comprises two the second cylinders, and the second drive unit connects described movable part by a second joint bearing, and drives described movable part to rotate relative to wing-body.
4. a kind of model airship wing according to claim 3, is characterized in that, two described second cylinders join end to end setting, and preceding described second cylinder connects described movable part by described second joint bearing.
5. a kind of model airship wing according to claim 4, it is characterized in that, described at least one, the upper cover of piston rod of the second cylinder is provided with spring.
6. a kind of model airship wing according to claim 1, it is characterized in that, described 3rd drive unit is the 3rd cylinder be located at inside hatch door, and described 3rd cylinder-bore axis direction is vertical relative to the rotor shaft direction of wing-body with hatch door, one end of described 3rd cylinder is coupling in described wing-body, and the other end connects described hatch door by a three-knuckle bearing.
7. a kind of model airship wing according to claim 1, it is characterized in that, described four-drive device comprises a four-cylinder, and described four-cylinder connects described gun barrel by one the 4th oscillating bearing, and drives described gun barrel to rotate relative to the opening surface of described opening.
8. a kind of model airship wing according to claim 7, it is characterized in that, described gun barrel comprises at least one launching pod, and described launching pod is connected with one the 5th drive unit, can do under described 5th drive unit drives near and the motion of the position that is coupling away from described gun barrel and airship main body.
9. use the model airship of a kind of model airship wing described in any one of claim 1-8, it is characterized in that, comprise airship main body and the support for hanging described airship main body, described support comprises substrate, be fixed on the first side plate on described substrate length direction successively, second side plate, hollow circular tube, 3rd side plate, 4th side plate and the 5th side plate, the first stiffener is fixed with between described first side plate and described second side plate, described hollow circular tube is vertically arranged, the second stiffener is fixed with between one side of described hollow circular tube and described second side plate, another side of described hollow circular tube passes described 3rd side plate and fixes with described 3rd side plate, the 3rd stiffener is fixed with between another side of described hollow circular tube and described 4th side plate, described 3rd side plate is fixed with motor, the rotating shaft of described motor is connected with the first gear, described hollow circular tube is fixed with the second gear, described first gear and described second gear engage each other, the upper end of described hollow circular tube is fixed with swivel joint.
10. a kind of model airship according to claim 9, it is characterized in that, comprise the lifting assembly being located at airship main body and the circular cylinder body be arranged on described lifting assembly, described lifting assembly comprises level board, lower horizontal board and connect two side plates of described upper level board and described lower horizontal board, intermediate plate is provided with between described upper level board and described lower horizontal board, support plate is fixed with between two described side plates, described support plate is positioned at the top of described intermediate plate, described support plate is fixed with motor, the rotating shaft of described motor is stretched out described upper level board and fixes with described circular cylinder body, described intermediate plate is fixed with cylinder, described cylinder is connected with described lower horizontal board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420828762.6U CN204352548U (en) | 2014-12-24 | 2014-12-24 | Model airship and wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420828762.6U CN204352548U (en) | 2014-12-24 | 2014-12-24 | Model airship and wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204352548U true CN204352548U (en) | 2015-05-27 |
Family
ID=53254046
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420828762.6U Expired - Fee Related CN204352548U (en) | 2014-12-24 | 2014-12-24 | Model airship and wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204352548U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104548612A (en) * | 2014-12-24 | 2015-04-29 | 苏州原点工业设计有限公司 | Model airship and aerofoil |
-
2014
- 2014-12-24 CN CN201420828762.6U patent/CN204352548U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104548612A (en) * | 2014-12-24 | 2015-04-29 | 苏州原点工业设计有限公司 | Model airship and aerofoil |
| CN104548612B (en) * | 2014-12-24 | 2017-05-24 | 苏州原点工业设计有限公司 | Model airship and aerofoil |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110718131A (en) | Launching device for simulating rocket launching | |
| CN103963867B (en) | Biomimetic mechanical dinosaur | |
| CN109529301A (en) | A kind of table tennis training multi-angle service robot | |
| CN204352548U (en) | Model airship and wing | |
| CN216562253U (en) | Earthquake demonstration device for building earthquake-resistant teaching | |
| CN102755754A (en) | Full-slewing multi-degree-of-freedom dynamic device with mechanical animal | |
| CN104548612A (en) | Model airship and aerofoil | |
| CN106005453B (en) | A kind of unmanned plane gondola jack and assembly method | |
| CN109326191B (en) | Bird mechanical structure model | |
| CN213339229U (en) | Six-freedom-degree motion platform | |
| CN204352550U (en) | A kind of model airship emitting structural | |
| CN207123973U (en) | A kind of parabola demonstration teaching aid | |
| CN204502397U (en) | A kind of model airship wing with movable hatch door | |
| CN204352551U (en) | A kind of model airship wing | |
| CN110082504A (en) | A kind of excavation simulation case apparatus, simulation experiment device and analogue experiment method | |
| CN213216252U (en) | Hanging structure for dynamically displaying airplane model | |
| CN113577731B (en) | National tradition sports teaching equipment | |
| CN206070816U (en) | Show body of wall and its arc scalable exhibition board wall connecting device | |
| RU2725119C2 (en) | Ground-based helicopter-type target installation | |
| CN204009328U (en) | Portable translucent equipment | |
| CN203870839U (en) | Rotating device for aircraft simulation training | |
| CN208027615U (en) | A kind of mathematics solid geometry teaching aid | |
| CN104548617A (en) | Model spaceship wing | |
| CN210200029U (en) | Multifunctional teaching aid for education technology | |
| CN105243919B (en) | Simulated flight device with manipulator |
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: 20150527 Termination date: 20151224 |
|
| EXPY | Termination of patent right or utility model |