CN104548617A - Model spaceship wing - Google Patents
Model spaceship wing Download PDFInfo
- Publication number
- CN104548617A CN104548617A CN201410813034.2A CN201410813034A CN104548617A CN 104548617 A CN104548617 A CN 104548617A CN 201410813034 A CN201410813034 A CN 201410813034A CN 104548617 A CN104548617 A CN 104548617A
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- wing
- airship
- cylinder
- movable part
- main body
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Abstract
The invention discloses a model spaceship wing which is mounted on the side of a spaceship main body and comprises a sheet-shaped or plate-shaped wing main body. The model spaceship wing is characterized in that the wing main body is in shaft joint with the spaceship main body, is connected with a first driving device and is capable of folding and unfolding relative to the spaceship main body under the driving of the first driving device. The model spaceship wing is capable of folding and unfolding relative to the spaceship main body, has the simulation action function and serves as a toy, a teaching aid and a showpiece.
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.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 the structure that the main body of relative airship is static, cannot realize taking down the exhibits of wing, and emulation property is poor.
Summary of the invention
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.
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 wing-body comprises wing skeleton and is wrapped in the panel of wing skeleton outside, and described wing skeleton comprises at least two by the main bone extended near airship main body one end away from airship main body one end, and the secondary bone of each main bone of some connections.
Preferably, described wing-body comprises wing-body and is located at the movable part of wing-body front end, 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.
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.
The beneficial effect that the present invention reaches:
1. model airship wing of the present invention, can receive relative to the exhibition of airship main body, have 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.
3. be provided with the wing skeleton of main bone and secondary bone in wing-body as main support structure, while saving material, greatly improve wing crushing resistance, not fragile, contribute to increasing the service life.
4. the front end movable part arranging wing-body further can rotate up and down relative to wing-body, and especially movable part can swing between wing-body both sides, then can complete the action of more replicating machines, simulated effect is better.
5. 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.
6. spring is set at the upper cover of piston rod of at least one cylinder, then can increases 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.
Accompanying drawing explanation
Fig. 1 is the connection diagram of wing-body and airship main body in the preferred embodiment of the present invention;
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 preferred embodiment of the present invention;
Fig. 4 is the enlarged diagram of the second drive unit in Fig. 3;
Wherein: 2, airship main body, 4, wing-body, 42, wing skeleton, 422, main bone, 424, secondary bone, 44, panel, 46, wing-body, 48, movable part, 482, sheet metal, 484, panel, the 6, first drive unit, the 62, first cylinder, 64, the first oscillating bearing, the 8, second drive unit, the 82, second cylinder, 822, piston rod, 824, cylindrical shell, the 84, second cylinder, 842, piston rod, 86, second joint bearing, 87, spring, 9, hinge, 92, U-shaped frame, 94, U-shaped frame.
Embodiment
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.
1-4 as shown in the figure, 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 6, can relative to airship main body 2 adduction and expansion under the first drive unit 6 drives.
Concrete, wing-body 4 comprises wing skeleton 42 and is wrapped in the panel 44 of wing skeleton 42 outside.Wing-body 4 is coupling by wing skeleton 42 and airship main body 2 on the one hand, and wing-body 4 also connects the first drive unit 6 by wing skeleton 42 on the other hand, and wing skeleton 42 and panel 44 can synchronous axial system.First drive unit 6 is specially the first cylinder 62 that axis being parallel is arranged in wing-body 4 in-plane, and the axis of the first cylinder 62 and airship main body 2 axis C in a certain angle, one end of first cylinder 62 is coupling in airship main body 2, and the other end connects the wing skeleton 42 of wing-body 4 by one first oscillating bearing 64.
Wing skeleton 42 comprises three respectively by the main bone 422 extended near airship main body 2 one end away from airship main body 2 one end, and the secondary bone 424 of each main bone 422 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 46 and is located at the sheet movable part 48 of wing-body 46 front end, movable part 48 is coupling in wing-body 46, and be connected with one second drive unit 8, can rotate both sides up and down relative to wing-body 46 respectively under the second drive unit 8 drives, thus can swing between wing-body 46 both sides.
Movable part 48 specifically comprise as skeleton sheet metal 482 and be arranged on the panel 484 of sheet metal 482 both sides, movable part 48 connects the second drive unit 8 by sheet metal 482, and panel 484 with sheet metal 482 is fixing can synchronous axial system.Sheet metal 482 and wing-body 46 are coupling especially by hinge 9, and namely wing-body 46 is fixed in one end of hinge 9, and the other end is fixed on sheet metal 482.Second drive unit 8 specifically comprises two the second cylinders 82,84, and the second drive unit 8 is by the sheet metal 482 of second joint bearing 86 movable part connecting 48, and drives movable part 48 to rotate relative to wing-body 46.More specifically, two the second cylinders 82,84 join end to end setting, and preceding second cylinder 82 is by second joint bearing 86 movable part connecting 48.
The axis direction of the second cylinder 82 and the second cylinder 84 overlaps, relative to sheet metal 482, second cylinder 82 of closer sheet metal 482 is front, compared with the second cylinder 84 away from sheet metal 482 rear, and the cylindrical shell 824 of the second cylinder 82 is fixed on a U-shaped frame 92, cylindrical shell 824 is placed between U-shaped frame 92 two ends, and piston rod 822 stretches out forward U-shaped frame 92, and the second cylinder 84 is also fixed on a U-shaped frame 94 in an identical manner.Concrete, U-shaped frame 94 is fixed on wing-body 46, its piston rod 842 of the second cylinder 84 of rear end fixed thereon connects the tail end of U-shaped frame 92, and its piston rod 822 front end of the second cylinder 82 of the front end that U-shaped frame 92 is arranged is connected with sheet metal 482 by second joint bearing 86.Therefore, the drive unit driven forward sheet metal 482 that two second cylinders 82,84 form can make sheet metal 482 wrap page 9 rotor shaft direction together with panel 484 and be rotated down motion; Pull back sheet metal 482 sheet metal 482 can be made together with panel 484 to wrap page 9 rotor shaft direction rotate up motion.
More specifically, on the piston rod 822 of the second cylinder 82 and the piston rod 842 of the second cylinder 84 be arranged with spring 87 respectively.Then can increase power-assisted when the second cylinder 82 and/or the second cylinder 82 driven forward movable part 48 overturn, play position-limiting action when the second cylinder 82 and/or the second cylinder 82 reclaim and drive movable part 48 reverse flip, thus can flip angle be controlled.Spring 87 according to two the second cylinders 82,84 coordinates, and the angle that movable part 48 rotates respectively to both sides relative to wing-body 46 can be the same or different.It is 60 ° that the setting of preferred spring 87 can control the amplitude peak that movable part 48 rotates to side relative to wing-body 46, then fidelity is high.
Introduce a kind of simulated actions process of model airship wing wing-body of the present invention below, the present invention is not construed as limiting.
It is outside that first cylinder 62 promotes wing-body 4, then wing-body 4 launches gradually relative to airship main body 2, to the first cylinder 62 cannot continue to promote wing-body 4 again, then the first cylinder 62 reclaims and pulls wing-body 4 inside, then wing-body 4 gets back to virgin state relative to airship main body 2 adduction to the first cylinder 62.
Introduce a kind of simulated actions process of citing model airship wing nose movable part of the present invention below, the present invention is not construed as limiting.
First front end second cylinder 82 piston rod 822 driven forward sheet metal 482 drives whole movable part 48 to wrap page 9 rotor shaft direction to be rotated down to turning over 10 ° of angles relative to initial planar; Then, rear end second cylinder 84 piston rod 842 pulls back front end second cylinder 82 cylindrical shell 824, make front end second cylinder 82 drive movable part 48 to wrap page 9 rotor shaft direction backward to rotate up, and when the stroke that distance counteracting front end second cylinder 82 that rear end second cylinder 84 is advanced backward is initially pushed ahead, movable part 48 resets, second cylinder 84 piston rod 842 continues to pull the second cylinder 82 to drop back, then movable part 48 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 48.
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 (8)
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.
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 wing-body comprises wing skeleton and is wrapped in the panel of wing skeleton outside, described wing skeleton comprises at least two by the main bone extended near airship main body one end away from airship main body one end, and the secondary bone of each main bone of some connections.
4. a kind of model airship wing according to claim 2, it is characterized in that, described wing-body comprises wing-body and is located at the movable part of wing-body front end, described movable part is coupling in wing-body, and be connected with one second drive unit, at least can rotate to side relative to wing-body under described second drive unit drives.
5. a kind of model airship wing according to claim 4, is characterized in that, described movable part can swing between wing-body both sides.
6. a kind of model airship wing according to claim 4, 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.
7. a kind of model airship wing according to claim 6, 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.
8. a kind of model airship wing according to claim 7, it is characterized in that, described at least one, the upper cover of piston rod of the second cylinder is provided with spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410813034.2A CN104548617A (en) | 2014-12-24 | 2014-12-24 | Model spaceship wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410813034.2A CN104548617A (en) | 2014-12-24 | 2014-12-24 | Model spaceship wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104548617A true CN104548617A (en) | 2015-04-29 |
Family
ID=53066345
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410813034.2A Pending CN104548617A (en) | 2014-12-24 | 2014-12-24 | Model spaceship wing |
Country Status (1)
| Country | Link |
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| CN (1) | CN104548617A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107885922A (en) * | 2017-10-27 | 2018-04-06 | 北京空间技术研制试验中心 | Spacecraft modeling information management method |
| CN108945429A (en) * | 2018-07-02 | 2018-12-07 | 北京航空航天大学 | A kind of micro flapping wing air vehicle wing, which is fluttered and opened up, receives multi-mode drive unit |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN87102199A (en) * | 1987-03-16 | 1988-09-28 | 任世钧 | Flight toy with changeable wings |
| 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 |
| CN102438713A (en) * | 2009-05-01 | 2012-05-02 | 思盈科技公司 | Toy with folding retractable wings |
| CN203854858U (en) * | 2014-04-25 | 2014-10-01 | 于国防 | Ornithopter |
| CN204352551U (en) * | 2014-12-24 | 2015-05-27 | 苏州原点工业设计有限公司 | A kind of model airship wing |
-
2014
- 2014-12-24 CN CN201410813034.2A patent/CN104548617A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN87102199A (en) * | 1987-03-16 | 1988-09-28 | 任世钧 | Flight toy with changeable wings |
| 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 |
| CN102438713A (en) * | 2009-05-01 | 2012-05-02 | 思盈科技公司 | Toy with folding retractable wings |
| CN203854858U (en) * | 2014-04-25 | 2014-10-01 | 于国防 | Ornithopter |
| CN204352551U (en) * | 2014-12-24 | 2015-05-27 | 苏州原点工业设计有限公司 | A kind of model airship wing |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107885922A (en) * | 2017-10-27 | 2018-04-06 | 北京空间技术研制试验中心 | Spacecraft modeling information management method |
| CN108945429A (en) * | 2018-07-02 | 2018-12-07 | 北京航空航天大学 | A kind of micro flapping wing air vehicle wing, which is fluttered and opened up, receives multi-mode drive unit |
| CN108945429B (en) * | 2018-07-02 | 2020-10-30 | 北京航空航天大学 | Wing flapping and unfolding and folding multi-mode driving device of miniature flapping wing aircraft |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150429 |