CN104097474A - Rear parallel wings for amphicar - Google Patents
Rear parallel wings for amphicar Download PDFInfo
- Publication number
- CN104097474A CN104097474A CN201310113984.XA CN201310113984A CN104097474A CN 104097474 A CN104097474 A CN 104097474A CN 201310113984 A CN201310113984 A CN 201310113984A CN 104097474 A CN104097474 A CN 104097474A
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- Prior art keywords
- amphicar
- vertical tail
- rear parallel
- tailplane
- wings
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- 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.)
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Abstract
The invention discloses rear parallel wings for an amphicar. The rear parallel wings comprise vertical tail wings, a horizontal tail wing and an elevating rudder; the vertical tail wings are arranged on the lower side of the horizontal tail wing; the elevating rudder is arranged on the upper side of the horizontal tail. The elevating rudder is arranged on the upper side of the horizontal tail wing to effectively assist the amphicar in implementing stable lifting; the vertical tail wings are symmetrically arranged at two ends of the lower side of the horizontal tail wing and are of double-layer structures with reinforcing ribs, so that the structure is firm and the stability of the rear parallel wings is improved; the outer side faces of the vertical tails are provided with rudders to fulfill the aim of quickly adjusting the direction of the amphicar; the vertical tail wings are connected with the horizontal tail wing through bolts to fulfill the aim of facilitating connection and production; the vertical tail wings and the horizontal tail wing are integrally formed to fulfill the aims of having a compact structure and improving the wind guiding effect; the rear parallel wings are simple in structure and practical.
Description
Technical field
The present invention relates to amphicar technical field, relate in particular to a kind of rear parallel wing for amphicar.
Background technology
The densely populated metropolis of current developed country, traffic congestion is increasingly serious.Three dwell automobile or amphicar are effectively alleviated the ideal chose that urban transport problems and part substitute land transportation transportation means just.
In prior art, be not specifically designed to the rear parallel wing of amphicar, in prior art, rear parallel wing structure is comparatively complicated, and inconvenient when amphibious vehicle rises or decline, existence affects the problem of flight effect.Based on the problems referred to above, be necessary it to be improved.
Summary of the invention
For overcoming above-mentioned technical deficiency, object of the present invention provides sound construction, simple a kind of rear parallel wing for amphicar.
For achieving the above object, technical scheme of the present invention is as follows:
A rear parallel wing for amphicar, comprises vertical tail, tailplane and elevating rudder, and described vertical tail is arranged on tailplane downside, and described tailplane upside arranges elevating rudder.
In the present invention, the quantity of described vertical tail is two, and described two vertical tails are symmetricly set on the two ends of tailplane downside.
In the present invention, on described vertical tail, reinforced rib is set.
In the present invention, described vertical tail comprises ground floor empennage and second layer empennage, and described ground floor empennage and second layer empennage compress mutually by bolt.
In the present invention, also comprise yaw rudder, described yaw rudder is arranged on the lateral surface of vertical tail.
In the present invention, described vertical tail and tailplane are bolted.
In the present invention, described vertical tail and tailplane are one-body molded.
The present invention compared with the existing technology, has the following advantages and beneficial effect:
1, by the upside at tailplane, elevating rudder is set, effectively auxiliary amphicar realizes steady lifting.
2, at tailplane downside two ends, be symmetrical arranged vertical tail, vertical tail is the double-deck structure with reinforced rib, and not only sound construction, strengthens stability of the present invention more.
3, the lateral surface at vertical tail arranges yaw rudder, reaches the object of amphicar quick adjustment direction.
4, vertical tail and tailplane are bolted, and reach convenient and connect, object convenient for production.
5, vertical tail and tailplane are one-body molded, reach close structure, promote the object of wind effect.
Accompanying drawing explanation
Fig. 1 structural representation of the present invention;
The structural representation that Fig. 2 tailplane is connected with vertical tail;
The profile schematic diagram of Fig. 3 tailplane;
The structural representation of Fig. 4 tailplane.
Wherein: 1, vertical tail; 2, tailplane; 22, tailplane upside; 3, elevating rudder; 4, yaw rudder; 5, bolt; 6, empennage support.
The specific embodiment
Below in conjunction with accompanying drawing illustrated embodiment, the present invention is further illustrated.
Embodiment
Referring to Fig. 1---Fig. 4, Fig. 1 is structural representation of the present invention; The structural representation that Fig. 2 tailplane is connected with vertical tail; The profile schematic diagram of Fig. 3 tailplane; The structural representation of Fig. 4 tailplane.
For a rear parallel wing for amphicar, comprise vertical tail 1, tailplane 2 and elevating rudder 3, vertical tail 1 is arranged on tailplane downside (not shown), and tailplane upside 22 arranges elevating rudder 3.
The quantity of vertical tail 1 is two, and two vertical tails are symmetricly set on the two ends of tailplane downside, reaches the object of steady water conservancy diversion.
Reinforced rib (not shown) is set on vertical tail 1, strengthens the fastness of vertical tail 1 structure.
Vertical tail 1 comprises ground floor empennage and second layer empennage, and ground floor empennage and second layer empennage compress mutually by bolt, and an independent vertical tail 1 has two aspects, and not only sound construction, also makes after one deck damage, and opposite side can also normally be used.
A rear parallel wing for amphicar, also comprises yaw rudder 4, and yaw rudder 4 is arranged on the lateral surface of vertical tail 1; This use novel preferred embodiment in, two vertical tails 1 are symmetrical arranged, in the whole interior that two vertical tails 1 form is, outside is said lateral surface, now on two vertical tails 1, respectively has a yaw rudder 4; If only have a vertical tail 1, there is respectively a yaw rudder 4 both sides of vertical tail 1 so.
Vertical tail 1 is connected by bolt 5 with tailplane 2, and workout cost reaches the convenient object of installing and changing, and makes vertical tail 1 or tailplane 2 one of them damage, only needs to change that part and just can continue use.
In another embodiment of the invention, vertical tail 1 and tailplane 2 are one-body molded, reach close structure, promote the object of wind effect.
In the preferred embodiment of the present invention, vertical tail 1 connects amphicar by empennage support 6.
The above-mentioned description to embodiment is can understand and use the present invention for ease of those skilled in the art.Person skilled in the art obviously can easily make various modifications to these embodiment, and General Principle described herein is applied in other embodiment and needn't passes through performing creative labour.Therefore, the invention is not restricted to above-described embodiment, those skilled in the art are according to announcement of the present invention, and not departing from the improvement that category of the present invention makes and revise all should be within protection scope of the present invention.
Claims (7)
1. for a rear parallel wing for amphicar, it is characterized in that, comprise vertical tail, tailplane and elevating rudder, described vertical tail is arranged on tailplane downside, and described tailplane upside arranges elevating rudder.
2. a kind of rear parallel wing for amphicar according to claim 1, is characterized in that: the quantity of described vertical tail is two, and described two vertical tails are symmetricly set on the two ends of tailplane downside.
3. a kind of rear parallel wing for amphicar according to claim 2, is characterized in that: on described vertical tail, reinforced rib is set.
4. according to a kind of rear parallel wing for amphicar described in one of claims 1 to 3 claim, it is characterized in that: described vertical tail comprises ground floor empennage and second layer empennage, described ground floor empennage and second layer empennage compress mutually by bolt.
5. a kind of rear parallel wing for amphicar according to claim 4, is characterized in that, also comprise yaw rudder, described yaw rudder is arranged on the lateral surface of vertical tail.
6. a kind of rear parallel wing for amphicar according to claim 4, is characterized in that: described vertical tail and tailplane are bolted.
7. a kind of rear parallel wing for amphicar according to claim 4, is characterized in that: described vertical tail and tailplane are one-body molded.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310113984.XA CN104097474A (en) | 2013-04-03 | 2013-04-03 | Rear parallel wings for amphicar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310113984.XA CN104097474A (en) | 2013-04-03 | 2013-04-03 | Rear parallel wings for amphicar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104097474A true CN104097474A (en) | 2014-10-15 |
Family
ID=51666185
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310113984.XA Pending CN104097474A (en) | 2013-04-03 | 2013-04-03 | Rear parallel wings for amphicar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104097474A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741852A (en) * | 2016-12-08 | 2017-05-31 | 顺丰科技有限公司 | Tailplane and shipping unmanned plane with trim elevator high |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10108596C1 (en) * | 2001-02-22 | 2002-10-24 | Abs Services Ag Kuesnacht | Ground effect vehicle for skimming over surface of water has planing float hull, low-mounted folding wings and high-mounted horizontal stabilizer and air propeller |
| CN1948084A (en) * | 2006-05-18 | 2007-04-18 | 刘宏茂 | Lift force control method of rotating wing fan and vertiautomobile |
| CN101372198A (en) * | 2008-07-08 | 2009-02-25 | 陈博 | Hovercar |
| EP2327571A2 (en) * | 2009-11-27 | 2011-06-01 | Rainer Farrag | Flying device capable of being coupled with a single track road vehicle |
| CN102616096A (en) * | 2012-04-24 | 2012-08-01 | 赵辉 | Solar flying automobile with folding wings |
| CN203267696U (en) * | 2013-04-03 | 2013-11-06 | 上海同捷科技股份有限公司 | Rear parallel wing for amphibious automobile |
-
2013
- 2013-04-03 CN CN201310113984.XA patent/CN104097474A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10108596C1 (en) * | 2001-02-22 | 2002-10-24 | Abs Services Ag Kuesnacht | Ground effect vehicle for skimming over surface of water has planing float hull, low-mounted folding wings and high-mounted horizontal stabilizer and air propeller |
| CN1948084A (en) * | 2006-05-18 | 2007-04-18 | 刘宏茂 | Lift force control method of rotating wing fan and vertiautomobile |
| CN101372198A (en) * | 2008-07-08 | 2009-02-25 | 陈博 | Hovercar |
| EP2327571A2 (en) * | 2009-11-27 | 2011-06-01 | Rainer Farrag | Flying device capable of being coupled with a single track road vehicle |
| CN102616096A (en) * | 2012-04-24 | 2012-08-01 | 赵辉 | Solar flying automobile with folding wings |
| CN203267696U (en) * | 2013-04-03 | 2013-11-06 | 上海同捷科技股份有限公司 | Rear parallel wing for amphibious automobile |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741852A (en) * | 2016-12-08 | 2017-05-31 | 顺丰科技有限公司 | Tailplane and shipping unmanned plane with trim elevator high |
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| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20141015 |
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| RJ01 | Rejection of invention patent application after publication |