TWM635058U - Adjustable tail wing - Google Patents
Adjustable tail wing Download PDFInfo
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- TWM635058U TWM635058U TW111209100U TW111209100U TWM635058U TW M635058 U TWM635058 U TW M635058U TW 111209100 U TW111209100 U TW 111209100U TW 111209100 U TW111209100 U TW 111209100U TW M635058 U TWM635058 U TW M635058U
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Abstract
本創作係關於一種可調式尾翼,乃至少包括有兩基座與至少一可調式翼板,該等基座乃可設於一交通工具之殼體上,該可調式翼板之兩端乃分別樞接設於該兩基座上,該可調式翼板可依交通工具之行駛速度,對應手動調整其傾斜角度,藉此可導引氣流提供適當之下壓力,達到穩定駕駛之目的。 This invention relates to an adjustable tail, which includes at least two bases and at least one adjustable wing plate, the bases can be set on the shell of a vehicle, and the two ends of the adjustable wing plate are respectively Pivoted on the two bases, the adjustable wing can be manually adjusted to its angle of inclination according to the driving speed of the vehicle, so as to guide the airflow and provide appropriate downward pressure to achieve the purpose of stable driving.
Description
本創作係關於一種可調式尾翼,特指一種裝設於一交通工具上,並具有至少一可調式翼板可對應不同行駛速度導引氣流提供下壓力,達到穩定行駛目的之結構者。 The invention relates to an adjustable rear wing, specifically a structure that is installed on a vehicle and has at least one adjustable wing plate that can guide the air flow to provide downforce corresponding to different driving speeds, so as to achieve the purpose of stable driving.
據悉,一般的交通工具在行駛時,常會產生各式氣流,該氣流更會對交通工具產生一上升力,若該交通工具乃為陸上交通工具,即會導致其輪子與地面間的抓地力下降,致使駕駛者無法穩定地駕馭該交通工具,當遇到突發狀況時,往往容易會因而釀出事故。 It is reported that general vehicles often generate various airflows when they are running, and the airflow will even generate a lifting force on the vehicle. If the vehicle is a land vehicle, it will cause the grip between its wheels and the ground to decrease , causing the driver to be unable to steer the vehicle stably, and when encountering unexpected situations, it is often easy to cause an accident.
故大多交通工具會裝設有至少一尾翼,該尾翼乃具有一傾斜角度,用以引導氣流通過,令氣流對該交通工具產生一下壓力,藉此達到可穩定駕駛交通工具之目的,但因該尾翼之傾斜角度乃為固定,乃對於一行駛速度範圍具有較佳地穩定效果,當該交通工具之行駛速度超出該範圍,即無法較佳地達到提供穩定駕駛之目的。 Therefore, most vehicles will be equipped with at least one tail fin, which has an angle of inclination to guide the airflow to pass through, so that the airflow will generate a pressure on the vehicle, so as to achieve the purpose of driving the vehicle stably. The inclination angle of the rear wing is fixed, which has a better stabilizing effect for a driving speed range. When the driving speed of the vehicle exceeds this range, the purpose of providing stable driving cannot be better achieved.
為此,如何提供一種可在不同行駛速度範圍,皆能穩定駕駛交通工具之結構或裝置,即為本創作之創作人所亟欲研究改善之方向所在。 For this reason, how to provide a kind of structure or device that can stably drive vehicles in different speed ranges is the direction that the creator of this creation desires to study and improve.
故,本創作之創作人有鑑於上述缺失,乃搜集相關資料,經由多方評估及考量,並以從事於此行業累積之多年經驗,經由不斷試作及 修改,始設計出此種新型專利者。 Therefore, in view of the above deficiencies, the creator of this creation collected relevant information, evaluated and considered in many ways, and based on years of experience accumulated in this industry, through continuous trials and Revise, begin to design this kind of novel patentee.
本創作之主要目的,係在提供一種可調式尾翼,乃至少包括有兩基座與至少一可調式翼板,該等基座乃可設於一交通工具之殼體上,該可調式翼板之兩端乃分別樞接設於該兩基座上,該可調式翼板可依交通工具之行駛速度,對應手動調整其傾斜角度,藉此可導引氣流提供適當之下壓力,達到穩定駕駛之目的。 The main purpose of this creation is to provide an adjustable tail, which at least includes two bases and at least one adjustable wing plate, and these bases can be arranged on the shell of a vehicle, and the adjustable wing plate The two ends are pivotally connected to the two bases respectively. The adjustable wing can be adjusted manually according to the speed of the vehicle, so that the angle of inclination can be adjusted manually, so that the airflow can be guided to provide an appropriate downward pressure to achieve stable driving. purpose.
為達上述目的,其可調式翼板乃至少具有一第一角度與一第二角度,該可調式翼板之角度可調整於該第一角度至第二角度之間,該基座乃具有至少一固定單元,以將該可調式翼板固定,達到調整該可調式翼板傾斜角度之功效。 In order to achieve the above purpose, the adjustable wing plate has at least a first angle and a second angle, the angle of the adjustable wing plate can be adjusted between the first angle and the second angle, and the base has at least A fixing unit is used to fix the adjustable wing plate to achieve the effect of adjusting the inclination angle of the adjustable wing plate.
1:可調式尾翼 1: Adjustable tail
2:基座 2: Base
21:固定單元 21: fixed unit
3:可調式翼板 3: Adjustable wing plate
4:固定翼板 4: fixed wing
第1圖係為本創作之一種可調式尾翼的立體結構示意圖; Figure 1 is a schematic diagram of the three-dimensional structure of an adjustable tail fin of this creation;
第2圖係為本創作之一種可調式尾翼的立體剖面示意圖; Figure 2 is a three-dimensional sectional schematic diagram of an adjustable empennage of this creation;
第3圖係為第2圖的分解結構示意圖; Figure 3 is a schematic diagram of the exploded structure of Figure 2;
第4圖係為本創作之一種可調式尾翼的剖面結構示意圖; The 4th figure is the sectional structure schematic diagram of a kind of adjustable empennage of this creation;
第5圖係為本創作之一種可調式尾翼的實施結構示意圖。 Fig. 5 is the implementation structure schematic diagram of a kind of adjustable empennage of this creation.
為達成上述或其他目的及功效,本創作所採用之技術手段及構造,茲繪圖就本創作較佳實施例詳加說明其特徵與功能如下,俾利完全了解。 In order to achieve the above-mentioned or other purposes and effects, the technical means and structures adopted in this creation are hereby drawn to illustrate in detail the characteristics and functions of the preferred embodiments of this creation as follows, so that Li can fully understand it.
請參閱第1至5圖,第1圖係為本創作之一種可調式尾翼的立體結構示意圖;第2圖係為本創作之一種可調式尾翼的立體剖面示意圖;第3圖係為第2圖的分解結構示意圖;第4圖係為本創作之一種可調式尾翼的剖面結構示意圖;第5圖係為本創作之一種可調式尾翼的實施結構示意圖。 Please refer to Figures 1 to 5. Figure 1 is a three-dimensional structural schematic diagram of an adjustable tail of this invention; Figure 2 is a three-dimensional cross-sectional schematic diagram of an adjustable tail of this invention; Figure 3 is a schematic diagram of the second picture Fig. 4 is a schematic diagram of a section structure of an adjustable empennage of this creation; Fig. 5 is a schematic diagram of an implementation structure of an adjustable empennage of this creation.
如該等圖所示,本創作主要提供之一種可調式尾翼1,乃至少包含:
As shown in these figures, the
兩基座2,乃可設於一交通工具之殼體上;以及,
Two
至少一可調式翼板3,其兩端乃分別樞接設於該兩基座2上;
At least one
其中,該可調式尾翼1更具有至少一固定翼板4,其兩端乃分別連接固設於該兩基座2上;
Wherein, the
其中,該固定翼板4乃相對設於該可調式翼板3的下方;
Wherein, the
其中,該兩基座2乃設於該交通工具之尾部的殼體上;
Wherein, the two
其中,該可調式翼板3乃至少具有一第一角度與一第二角度;
Wherein, the
其中,該基座2乃具有至少一固定單元21,用以將該可調式翼板3固定;
Wherein, the
本創作主要是應用諸如汽車、機車等交通工具上,但不僅限於此,亦可應用於其他任一交通工具上,且本創作之基座2乃係設於該交通工具之尾部殼體上,透過手動調整該可調式翼板3的傾斜角度,令本創作之可調式尾翼1可於各行駛速度範圍中,導引氣流提供適當之下壓力,藉此達到提供穩定駕駛之目的及其功效者;
This creation is mainly applied to vehicles such as automobiles and locomotives, but is not limited to this, and can also be applied to any other vehicles, and the
承上述,如第2及3圖所示,本創作之可調式尾翼1更具有至少一固定翼板4,其兩端乃分別連接固設於該兩基座2上,並相對設於該可調式翼板3下方,藉由該固定翼板4之傾斜角度,令本創作可再進一步加強
氣流產生之下壓力,達到穩定駕駛之目的;
Inheriting the above, as shown in Figures 2 and 3, the
另外,如第3至5圖所示,本創作中該可調式翼板3乃係樞接於該基座2上,且該基座2乃具有至少一固定單元21可用以固定該可調式翼板3,當該可調式翼板3於一第一角度與一第二角度間調整至所需的傾斜角度時,即可利用該固定單元21加以固定,以此達到調整該可調式翼板3的傾斜角度;
In addition, as shown in Figures 3 to 5, the
綜上所述,相較於習用尾翼結構所存在之種種缺失與無法解決之問題,本創作乃透過基座2與可調式翼板3之特殊設計,讓駕駛者在透過調整可調式翼板3的傾斜角度後,可於不同的行駛速度中導引氣流提供對應適當的下壓力,達到穩定駕駛之目的。
To sum up, compared with the various deficiencies and unsolvable problems in the conventional tail structure, this creation uses the special design of the
惟,以上所述僅為本創作之較佳實施例而已,非因此即拘限本創作之專利範圍,故舉凡運用本創作說明書及圖式內容所為之簡易修飾及等效結構變化,均應同理包含於本創作之專利範圍內,合予陳明。 However, the above description is only a preferred embodiment of this creation, and does not limit the patent scope of this creation. Therefore, all simple modifications and equivalent structural changes made by using the instructions and drawings of this creation should be the same The theory is included in the patent scope of this creation, and I agree with Chen Ming.
1:可調式尾翼 1: Adjustable tail
2:基座 2: Base
3:可調式翼板 3: Adjustable wing plate
4:固定翼板 4: fixed wing
Claims (6)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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TW111209100U TWM635058U (en) | 2022-08-22 | 2022-08-22 | Adjustable tail wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW111209100U TWM635058U (en) | 2022-08-22 | 2022-08-22 | Adjustable tail wing |
Publications (1)
Publication Number | Publication Date |
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TWM635058U true TWM635058U (en) | 2022-12-01 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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TW111209100U TWM635058U (en) | 2022-08-22 | 2022-08-22 | Adjustable tail wing |
Country Status (1)
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TW (1) | TWM635058U (en) |
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2022
- 2022-08-22 TW TW111209100U patent/TWM635058U/en unknown
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