CN203267696U

CN203267696U - Rear parallel wing for amphibious automobile

Info

Publication number: CN203267696U
Application number: CN 201320161662
Authority: CN
Inventors: 雷雨成; 赖赣明; 胡涛; 张朝军
Original assignee: TJI Innova Engineering and Technology Co Ltd
Current assignee: TJI Innova Engineering and Technology Co Ltd
Priority date: 2013-04-03
Filing date: 2013-04-03
Publication date: 2013-11-06
Anticipated expiration: 2023-04-03

Abstract

The utility model discloses a rear parallel wing for an amphibious automobile, which comprises vertical tail wings, a horizontal tail wing and a lifting rudder, wherein the vertical tail wings are arranged on the lower side of the horizontal tail wing, and the lifting rudder is arranged on the upper side of the horizontal tail wing. According to the rear parallel wing, the lifting rudder is arranged on the upper side of the horizontal tail wing, so that stable lifting of the amphibious automobile is assisted effectively; the vertical tail wings are symmetrically arranged at the two ends of the lower side of the horizontal tail wing, and are in double-layer structures with reinforcing ribs, so that the structure is firm, and the stability of the rear parallel wing is improved; direction rudders are arranged on the outer side surfaces of the vertical tail wings, so that a purpose of quickly adjusting a direction of the amphibious automobile is achieved; the vertical tail wings are connected with the horizontal tail wing by bolts, so that a purpose of convenience in connection and production is achieved; the vertical tail wings and the horizontal tail wing are formed integrally, so that purposes of a compact structure and an improved air guide effect are achieved; and the rear parallel wing is simple in structure and very practical.

Description

A kind of rear parallel wing for amphicar

Technical field

The utility model relates to the amphicar technical field, relates 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 the 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 descend, existence affects the problem of flight effect.Based on the problems referred to above, be necessary it is improved.

The utility model content

For overcoming above-mentioned technical deficiency, the purpose of this utility model provides sound construction, simple a kind of rear parallel wing for amphicar.

For achieving the above object, the technical solution of the utility model is as follows:

A kind of rear parallel wing for amphicar comprises vertical tail, tailplane and elevating rudder, and described vertical tail is arranged on the tailplane downside, and described tailplane upside arranges elevating rudder.

In the utility model, 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 utility model, on described vertical tail, reinforced rib is set.

In the utility model, 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 utility model, also comprise yaw rudder, described yaw rudder is arranged on the lateral surface of vertical tail.

In the utility model, described vertical tail and tailplane are bolted.

In the utility model, described vertical tail and tailplane are one-body molded.

The utility model is compared with prior art, has the following advantages and beneficial effect:

1, by the upside at tailplane, elevating rudder is set, effectively auxiliary amphicar realizes steady lifting.

2, be symmetrical arranged vertical tail at tailplane downside two ends, vertical tail has the structure of reinforced rib for double-deck, and not only sound construction, strengthen stability of the present utility model more.

3, the lateral surface at vertical tail arranges yaw rudder, reaches the purpose of amphicar quick adjustment direction.

4, vertical tail and tailplane are bolted, and reach convenient and connect, purpose convenient for production.

5, vertical tail and tailplane are one-body molded, reach close structure, promote the purpose of wind effect.

Description of drawings

Fig. 1 structural representation of the present utility model;

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 the accompanying drawing illustrated embodiment, the utility model is further described.

Embodiment

Referring to Fig. 1---Fig. 4, Fig. 1 are structural representation of the present utility model; 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.

A kind of rear parallel wing for amphicar comprises vertical tail 1, tailplane 2 and elevating rudder 3, and 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 purpose of steady water conservancy diversion.

The 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, sound construction not only, and after one deck was damaged, opposite side can also normally use.

A kind of 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 was, the outside was said lateral surface, respectively have a yaw rudder 4 on two vertical tails 1 this moment; 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 with tailplane by bolt 5 connections, and workout cost reaches the convenient purpose of installing and changing, and makes vertical tail 1 or tailplane 2 one of them damage, only need change that part and just can continue to use.

In another kind of embodiment of the present utility model, vertical tail 1 and tailplane 2 are one-body molded, reach close structure, promote the purpose of wind effect.

The utility model preferred embodiment in, vertical tail 1 connects amphicar by empennage support 6.

The above-mentioned description to embodiment is can understand and use the utility model for ease of those skilled in the art.The person skilled in the art obviously can easily make various modifications to these embodiment, and in the General Principle of this explanation is applied to other embodiment and needn't pass through performing creative labour.Therefore, the utility model is not limited to above-described embodiment, and those skilled in the art are according to announcement of the present utility model, and not breaking away from the improvement that the utility model category makes and revise all should be within protection domain of the present utility model.

Claims

1. a rear parallel wing that is used for amphicar, is characterized in that, comprise vertical tail, tailplane and elevating rudder, described vertical tail is arranged on the tailplane downside, and described tailplane upside arranges elevating rudder.

2. a kind of rear parallel wing for amphicar according to claim 1, it is characterized in that: the quantity of described vertical tail is two, 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.

One of according to claim 1 to 3 described a kind of rear parallel wing for amphicar, 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, it is characterized in that: described vertical tail and tailplane are bolted.

7. a kind of rear parallel wing for amphicar according to claim 4, it is characterized in that: described vertical tail and tailplane are one-body molded.