CN104548611A - Model airship wing with movable front end - Google Patents
Model airship wing with movable front end Download PDFInfo
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- CN104548611A CN104548611A CN201410812699.1A CN201410812699A CN104548611A CN 104548611 A CN104548611 A CN 104548611A CN 201410812699 A CN201410812699 A CN 201410812699A CN 104548611 A CN104548611 A CN 104548611A
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- wing
- movable part
- cylinder
- model airship
- movable
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Abstract
The invention discloses a model airship wing with a movable front end. The model airship wing comprises a wing body and a flaky or platy moving part arranged on the front end of the wing body. The model airship wing is characterized in that the moving part is connected to the wing body by a shaft, is connected with a drive device, and can at least rotate towards one side relative to the wing body under the driving of the drive device. According to the model airship wing disclosed by the invention, the front end can rotate relative to the wing body, so that the model airship wing has a simulative movement function, and can be used as a toy, a teaching aid or a showpiece. Especially, the moving part can swing between two sides of the wing body, so that more actions can be finished and the simulation effect is better.
Description
Technical field
The present invention relates to a kind of airship model.
Background technology
Along with the progress of science and technology, the mankind have been no longer unreachable dreams by airship exploration of the universe.Model airship, as the model of real airship, is subject to the welcome in market with the identity of toy exhibit and teaching equipment in other words.But existing model airship, technology only rests on simple outward appearance and imitates, and wing is the entirety of geo-stationary, cannot realize the action of wing nose, and emulation property is poor.
Summary of the invention
The model airship wing that a kind of front end is movable, comprise wing-body and be located at sheet or the tabular movable part of wing-body front end, it is characterized in that, described movable part is coupling in wing-body, and be connected with a drive unit, at least can rotate to side relative to wing-body under described drive unit drives.
Preferably, described movable part can swing between wing-body both sides.
Preferably, described drive unit comprises two cylinders, and drive unit connects described movable part by oscillating bearing, and drives described movable part to rotate relative to wing-body.
Preferably, two described cylinders join end to end setting, and preceding described cylinder connects described movable part by described oscillating bearing.
Preferably, described at least one, the upper cover of piston rod of cylinder is provided with spring.
Preferably, the amplitude peak that described movable part can rotate to side relative to wing-body is 60 °.
The beneficial effect that the present invention reaches:
1. model airship wing of the present invention, front end can be rotated relative to wing-body, has artificial activity function, both can as toy, again can as teaching aid, exhibit.Especially design activity portion can swing between wing-body both sides, then can complete more actions, simulated effect is better.
2. 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.
3. 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.
4. arranging the amplitude peak that movable part can rotate to side relative to wing-body is 60 °, then can realize the combination of action by a larger margin and many actions, fidelity is higher.
Accompanying drawing explanation
Fig. 1 is the cut-away view of the preferred embodiment of the present invention;
Fig. 2 is the enlarged diagram of drive unit in Fig. 1;
Wherein: 2, wing-body, 4, movable part, 42, metallic plate, 44, panel, 6, drive unit, 62, cylinder, 622, piston rod, 624, cylindrical shell, 64, cylinder, 642, piston rod, 65, spring, 66, oscillating bearing, 682, U-shaped frame, 684, U-shaped frame, 8, hinge.
Detailed description of the invention
Below in conjunction with accompanying drawing, the invention will be further described.Following examples only for technical scheme of the present invention is clearly described, and can not limit the scope of the invention with this.
As shown in Figure 1-2, the model airship wing that a kind of front end is movable, comprise wing-body 2 and be located at the sheet movable part 4 of wing-body 2 front end, movable part 4 is coupling in wing-body 2, and be connected with a drive unit 6, can rotate to both sides relative to wing-body 2 respectively under drive unit 6 drives, thus can swing between wing-body 2 both sides.
Concrete, movable part 4 comprise as skeleton metallic plate 42 and be arranged on the panel 44 of metallic plate 42 both sides, movable part 4 by metallic plate 42 connecting drive device 6, and panel 44 with metallic plate 42 is fixing can synchronous axial system.Metallic plate 42 and wing-body 2 are coupling especially by hinge 8, and namely wing-body 2 is fixed in one end of hinge 8, and the other end is fixed on metallic plate 42.Drive unit 6 specifically comprises two cylinders 62,64, and drive unit 6 is by the metallic plate 42 of oscillating bearing 66 movable part connecting 4, and drives movable part 4 to rotate relative to wing-body 2.More specifically, two cylinders 62,64 join end to end setting, and preceding cylinder 62 is by oscillating bearing 66 movable part connecting 4.
The axis direction of cylinder 62 and cylinder 64 overlaps, relative to metallic plate 42, the cylinder 62 of closer metallic plate 42 is front, compared with the cylinder 64 away from metallic plate 42 rear, and the cylindrical shell of cylinder 62 is fixed on a U-shaped frame 682, cylindrical shell 624 is placed between U-shaped frame 682 two ends, and piston rod 622 stretches out forward U-shaped frame 682, and cylinder 64 is also fixed on a U-shaped frame 684 in an identical manner.Concrete, U-shaped frame 684 is fixed on wing-body 2, and its piston rod 642 of the cylinder 64 of rear end fixed thereon connects the tail end of U-shaped frame 682, and its piston rod 622 front end of cylinder 62 of the front end that U-shaped frame 682 is arranged is connected with metallic plate 42 by oscillating bearing 66.Therefore, the drive unit 6 driven forward metallic plate 42 that two cylinders 62,64 form can make metallic plate 42 wrap page 8 rotor shaft direction together with panel 44 and be rotated down motion; Pull back metallic plate 42 metallic plate 42 can be made together with panel 44 to wrap page 8 rotor shaft direction rotate up motion.
More specifically, on the piston rod 622 of cylinder 62 and the piston rod 642 of cylinder 64 be arranged with spring 65 respectively.Then can increase power-assisted when cylinder 64 and/or cylinder 62 driven forward movable part 4 overturn, play position-limiting action when cylinder 64 and/or cylinder 62 reclaim and drive movable part 4 reverse flip, thus can flip angle be controlled.Spring 65 according to two cylinders 62,64 coordinates, and the angle that movable part 4 rotates respectively to both sides relative to wing-body 2 can be the same or different.It is 60 ° that the setting of preferred spring 65 can control the amplitude peak that movable part 4 rotates to side relative to wing-body 2, then fidelity is high.
Introduce a kind of simulated actions process of citing model airship wing nose of the present invention below, the present invention is not construed as limiting.
First the whole movable part 4 of front end cylinder 62 piston rod 622 driven forward metallic plate 42 wraps page 8 rotor shaft direction and is rotated down to turning over 10 ° of angles relative to initial planar; Then, rear end cylinder 64 piston rod pulls back front end cylinder 62 cylindrical shell 624, make front end cylinder 62 drive movable part 4 to wrap page 8 rotor shaft direction backward to rotate up, and when the stroke that the distance counteracting front end cylinder 62 that rear end cylinder 64 is advanced backward is initially pushed ahead, movable part 4 resets, cylinder 64 piston rod pulls on dynamic air cylinder 62 and drops back, then movable part 4 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 4.
The above is only the preferred embodiment of the present invention; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the technology of the present invention principle; can also make some improvement and distortion, these improve and distortion also should be considered as protection scope of the present invention.
Claims (6)
1. the model airship wing that a front end is movable, comprise wing-body and be located at sheet or the tabular movable part of wing-body front end, it is characterized in that, described movable part is coupling in wing-body, and be connected with a drive unit, at least can rotate to side relative to wing-body under described drive unit drives.
2. the model airship wing that a kind of front end according to claim 1 is movable, is characterized in that, described movable part can swing between wing-body both sides.
3. the model airship wing that a kind of front end according to claim 1 is movable, is characterized in that, described drive unit comprises two cylinders, and drive unit connects described movable part by oscillating bearing, and drives described movable part to rotate relative to wing-body.
4. the model airship wing that a kind of front end according to claim 3 is movable, is characterized in that, two described cylinders join end to end setting, and preceding described cylinder connects described movable part by described oscillating bearing.
5. the model airship wing that a kind of front end according to claim 4 is movable, is characterized in that, described at least one, the upper cover of piston rod of cylinder is provided with spring.
6. the model airship wing that a kind of front end according to claim 1 is movable, is characterized in that, the amplitude peak that described movable part can rotate to side relative to wing-body is 60 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410812699.1A CN104548611A (en) | 2014-12-24 | 2014-12-24 | Model airship wing with movable front end |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410812699.1A CN104548611A (en) | 2014-12-24 | 2014-12-24 | Model airship wing with movable front end |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104548611A true CN104548611A (en) | 2015-04-29 |
Family
ID=53066339
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410812699.1A Pending CN104548611A (en) | 2014-12-24 | 2014-12-24 | Model airship wing with movable front end |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104548611A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2074662U (en) * | 1990-09-29 | 1991-04-10 | 何方能 | Folding wing aerocraft |
| US5019007A (en) * | 1990-07-09 | 1991-05-28 | Miller Jack V | Toy glider with variable dihedral wings |
| CN101020502A (en) * | 2007-01-24 | 2007-08-22 | 田顺强 | Flapping wing unit of flapping wing aircraft |
| CN202279235U (en) * | 2011-09-06 | 2012-06-20 | 成都飞机设计研究所 | Variant canard tailless aerodynamic configuration |
| CN203854858U (en) * | 2014-04-25 | 2014-10-01 | 于国防 | Ornithopter |
-
2014
- 2014-12-24 CN CN201410812699.1A patent/CN104548611A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5019007A (en) * | 1990-07-09 | 1991-05-28 | Miller Jack V | Toy glider with variable dihedral wings |
| CN2074662U (en) * | 1990-09-29 | 1991-04-10 | 何方能 | Folding wing aerocraft |
| CN101020502A (en) * | 2007-01-24 | 2007-08-22 | 田顺强 | Flapping wing unit of flapping wing aircraft |
| CN202279235U (en) * | 2011-09-06 | 2012-06-20 | 成都飞机设计研究所 | Variant canard tailless aerodynamic configuration |
| CN203854858U (en) * | 2014-04-25 | 2014-10-01 | 于国防 | Ornithopter |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150429 |
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| RJ01 | Rejection of invention patent application after publication |