TWI683062B - Fan blade unit and fan impeller structure thereof - Google Patents
Fan blade unit and fan impeller structure thereof Download PDFInfo
- Publication number
- TWI683062B TWI683062B TW107134129A TW107134129A TWI683062B TW I683062 B TWI683062 B TW I683062B TW 107134129 A TW107134129 A TW 107134129A TW 107134129 A TW107134129 A TW 107134129A TW I683062 B TWI683062 B TW I683062B
- Authority
- TW
- Taiwan
- Prior art keywords
- convex
- groove
- item
- fan
- patent application
- Prior art date
Links
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
一種扇葉單元及其扇輪結構,該扇葉單元包含一主體,主體具有一根部及一端部並界定一主體厚度,該根部連接一輪轂,該端部朝向相反該輪轂的方向徑向延伸,所述端部界定有一第一方向及一第二方向;複數凸體,設置於該端部;及至少一凹槽,形成於該等凸體之間,所述凹槽沿該第一方向設置;其中該等凸體與該凹槽界定一總厚度等於或不大於該主體厚度,該扇輪結構運用上述扇葉單元,藉此當扇輪轉動時,該等凸體之間的凹槽與風扇外框壁產生高壓區,抑制氣流由下翼面往上翼面翻滾所產生的翼尖渦流。 A fan blade unit and a fan wheel structure thereof. The fan blade unit includes a main body having a portion and an end portion defining a thickness of the main body, the root portion is connected to a hub, and the end portion extends radially in a direction opposite to the hub, The end defines a first direction and a second direction; a plurality of convex bodies are provided at the end; and at least one groove is formed between the convex bodies, the groove is provided along the first direction ; Wherein the protrusions and the groove define a total thickness equal to or less than the thickness of the main body, the fan wheel structure uses the fan blade unit, whereby when the fan wheel rotates, the groove between the protrusions and The high-pressure area is generated on the outer frame wall of the fan to suppress the vortex of the wing tip generated by the airflow rolling from the lower wing surface to the upper wing surface.
Description
本發明係有關一種散熱風扇領域,特別是一種散熱扇葉結構及具有該散熱扇葉結構之散熱扇輪。 The invention relates to the field of cooling fans, in particular to a cooling fan blade structure and a cooling fan wheel with the cooling fan blade structure.
習知之軸流風扇扇葉在葉尖處因翼面上下壓力分布不同,導致氣流由高壓的下翼面往低壓的上翼面翻滾,在翼尖段產生強烈的翼尖渦流,此渦流使風扇流場不穩定而增加噪音與降低特性。 The conventional axial fan blades have different pressure distributions on the blade surface at the blade tip, causing the airflow to roll from the high-pressure lower wing surface to the low-pressure upper wing surface, which generates a strong wing tip vortex in the wing tip section. This vortex makes the fan The flow field is unstable and increases noise and reduces characteristics.
為了減弱翼尖渦流的強度,習知的做法包含增加翼尖90外緣的葉面面積、設計翼尖小翼91(如第1A圖),在翼尖往翼根的地方增加環型構造92(如圖1B)等,主要都是藉增加的結構阻擋下翼面流體往上翼面翻滾,減弱渦流強度。
In order to reduce the strength of the wingtip vortex, the conventional method includes increasing the leaf area of the outer edge of the
但上述的方法卻產生了其他的問題,第1A圖之翼尖小翼91做法改變了風扇葉尖的原始幾何,使流體流經葉尖的路徑受到阻礙或彎折而減弱了風扇的特性,第1B圖的環型構造92增加結構在葉尖端上方,會同時增加此點的荷重,造成結構的不穩定,端點處振動變大,在高速高溫運轉下有變形的風險。
However, the above method has other problems. The
是以,要如何解決上述之問題與缺失,即為本案之發明人與從事此行業之相關廠商所亟欲研究改善之方向所在者。 Therefore, how to solve the above-mentioned problems and deficiencies is where the inventors of the present case and related manufacturers engaged in this industry are desperate to study the direction of improvement.
爰此,為有效解決上述之問題,本發明目的在提供一種軸流風扇的每一扇葉單元的端部具有複數凸體藉以構成一凹槽,透過凹槽在轉動時產生高壓區以抑制翼尖渦流的扇葉單元及其扇輪結構。 Secondly, in order to effectively solve the above-mentioned problems, the object of the present invention is to provide a plurality of convex bodies at the end of each blade unit of an axial fan to form a groove through which a high-pressure area is generated during rotation to suppress the wing Sharp vortex fan blade unit and its fan wheel structure.
本發明的另一主要目的在於提供一種減少翼尖渦流造成的壓力損失,進而提升工作特性的扇葉單元及其扇輪結構。 Another main object of the present invention is to provide a fan blade unit and its fan wheel structure that reduce the pressure loss caused by the wing tip vortex, thereby improving the working characteristics.
本發明的另一主要目的在於提供一種減少翼尖渦流與風扇外框壁的交互作用而降低扇葉端部震動的扇葉單元及其扇輪結構。 Another main object of the present invention is to provide a fan blade unit and a fan wheel structure that reduce the interaction between the wing tip vortex and the outer frame wall of the fan to reduce the vibration at the end of the fan blade.
為達上述之目的,本發明提供一種扇葉單元,包含一主體,具有一根部及一端部並界定一主體厚度,該根部連接一輪轂,該端部朝向相反該輪轂的方向徑向延伸,所述端部界定有一第一方向及一第二方向;複數凸體,設置於該端部;及至少一凹槽,形成於該等凸體之間,所述凹槽沿該第一方向設置;其中該等凸體與該凹槽界定一總厚度等於或不大於該主體厚度。 To achieve the above purpose, the present invention provides a fan blade unit including a main body having a portion and an end portion and defining a thickness of the main body, the root portion is connected to a hub, and the end portion extends radially in a direction opposite to the hub. The end defines a first direction and a second direction; a plurality of convex bodies are provided at the end; and at least one groove is formed between the convex bodies, the grooves are provided along the first direction; Wherein the convex body and the groove define a total thickness equal to or not greater than the thickness of the main body.
本發明進一步提供了一種扇輪結構包含一輪轂;及複數扇葉單元,每一扇葉單元具有一主體,該主體具有一根部、一端部、複數凸體及至少一凹槽,其中該主體界定一主體厚度,該根部連接該輪轂的外側,該端部朝向相反該輪轂的方向徑向延伸,該端部界定有一第一方向及一第二方向,該等凸體設置於該端部,該凹槽形成於該等凸體之間,所述凹槽沿該第一方向設置;其中該等凸體與該凹槽界定一總厚度等於或不大於該主體厚度。 The invention further provides a fan wheel structure comprising a hub; and a plurality of fan blade units, each fan blade unit having a main body having a portion, an end portion, a plurality of convex bodies and at least one groove, wherein the main body defines A thickness of the main body, the root portion is connected to the outer side of the hub, the end portion extends radially in a direction opposite to the hub, the end portion defines a first direction and a second direction, the protrusions are disposed at the end portion, the A groove is formed between the protrusions, and the groove is arranged along the first direction; wherein the protrusions and the groove define a total thickness equal to or less than the thickness of the body.
藉由上述的結構,扇葉端部的凹槽在轉動時產生高壓區,透過高壓區抑制扇翼尖渦流所產生的各種不利影響,進而達到降低噪音、提升特性及降低扇葉端部的震動。 With the above structure, the groove at the end of the blade generates a high-pressure area during rotation, and suppresses various adverse effects caused by the vortex of the blade tip through the high-pressure area, thereby achieving noise reduction, improving characteristics and reducing vibration at the end of the blade .
1‧‧‧輪轂 1‧‧‧Wheel
2‧‧‧扇葉單元 2‧‧‧Fan unit
21‧‧‧主體 21‧‧‧Main
211‧‧‧根部 211‧‧‧Root
212‧‧‧端部 212‧‧‧End
213‧‧‧上表面 213‧‧‧Upper surface
214‧‧‧下表面 214‧‧‧Lower surface
215‧‧‧主體厚度 215‧‧‧Body thickness
22‧‧‧第一凸體 22‧‧‧The first convex body
221‧‧‧第一頂面 221‧‧‧First top
222‧‧‧第一底面 222‧‧‧First bottom
223‧‧‧第一左面 223‧‧‧ first left
224‧‧‧第一右面 224‧‧‧ first right
225‧‧‧第一凸體厚度 225‧‧‧Thickness of the first convex body
23‧‧‧第二凸體 23‧‧‧Second convex body
231‧‧‧第二頂面 231‧‧‧Second top surface
232‧‧‧第二底面 232‧‧‧Second bottom surface
233‧‧‧第二左面 233‧‧‧ second left
234‧‧‧第二右面 234‧‧‧ second right
235‧‧‧第二凸體厚度 235‧‧‧thickness of the second convex body
24‧‧‧第三凸體 24‧‧‧The third convex body
241‧‧‧第三頂面 241‧‧‧The third top
242‧‧‧第三底面 242‧‧‧The third bottom
243‧‧‧第三左面 243‧‧‧ third left
244‧‧‧第三右面 244‧‧‧ third right
245‧‧‧第三凸體厚度 245‧‧‧thickness of the third convex body
3‧‧‧凹槽 3‧‧‧groove
3a‧‧‧第一凹槽 3a‧‧‧First groove
3b‧‧‧第二凹槽 3b‧‧‧Second groove
4‧‧‧風扇外框壁 4‧‧‧Fan outer frame wall
HPA‧‧‧高壓區 HPA‧‧‧High pressure area
W‧‧‧寬度 W‧‧‧Width
H、H1、H2‧‧‧高度 H, H1, H2‧‧‧ Height
D1‧‧‧第一方向 D1‧‧‧First direction
D2‧‧‧第二方向 D2‧‧‧Second direction
第1A圖為習知風扇扇葉的第一種實施方式;第1B圖為習知風扇扇葉的第二種實施方式;第2A圖為本發明扇輪結構的立體示意圖;第2B圖為本發明扇葉結構的立體示意圖;第2C圖為本發明扇葉端部的剖面示意圖;第2D圖為本發明扇葉轉動產生高壓區的流體走向示意圖;第3A圖為本發明扇葉單一凹槽結構的替代實施示意圖(一);第3B圖為本發明扇葉單一凹槽結構的替代實施示意圖(二);第3C圖為本發明扇葉單一凹槽結構的替代實施示意圖(三);第3D圖為本發明扇葉單一凹槽結構的替代實施示意圖(四);第3E圖為本發明扇葉單一凹槽結構的替代實施示意圖(五);第3F圖為本發明扇葉單一凹槽結構的替代實施示意圖(六);第3G圖為本發明扇葉單一凹槽結構的替代實施示意圖(七);第3H圖為本發明扇葉單一凹槽結構的替代實施示意圖(八);第4A圖為本發明扇葉複數凹槽結構的替代實施示意圖(一);第4B圖為本發明扇葉複數凹槽結構的替代實施示意圖(二)。 Fig. 1A is the first embodiment of the conventional fan blade; Fig. 1B is the second embodiment of the conventional fan blade; Fig. 2A is a perspective schematic view of the fan wheel structure of the invention; Fig. 2B is this Stereo schematic view of the fan blade structure of the invention; Figure 2C is a schematic cross-sectional view of the end of the fan blade of the present invention; Figure 2D is a schematic diagram of the fluid flow direction of the high-pressure region generated by the rotation of the fan blade of the invention; Figure 3A is a single groove of the fan blade of the invention Schematic diagram of an alternative implementation of the structure (1); FIG. 3B is a schematic diagram of the alternative implementation of the single groove structure of the fan blade of the present invention (2); FIG. 3C is a schematic diagram of the alternative implementation of the single groove structure of the fan blade of the present invention (3); 3D is a schematic diagram of an alternative implementation of a single groove structure of a fan blade of the present invention (4); FIG. 3E is a schematic diagram of an alternative implementation of a single groove structure of a fan blade of the present invention (5); FIG. 3F is a single groove of the fan blade of the present invention Schematic diagram of an alternative implementation of the structure (6); Figure 3G is a schematic diagram of an alternative implementation of the single groove structure of the fan blade of the present invention (seven); Figure 3H is a schematic diagram of an alternative implementation of the single groove structure of the fan blade of the present invention (eight); FIG. 4A is a schematic diagram of an alternative implementation of the plural groove structure of the fan blade of the present invention (1); FIG. 4B is a schematic diagram of an alternative implementation of the plural groove structure of the fan blade of the present invention (2).
本發明之上述目的及其結構與功能上的特性,將依據所附圖式之較佳實施例予以說明。 The above objects, structural and functional characteristics of the present invention will be described based on the preferred embodiments of the accompanying drawings.
請參閱第2A圖及第2B圖及第2C圖,本發明主要包含一輪轂1及複數扇葉單元2,該輪轂1的外側表面設置該等扇葉單元2,每一扇葉單元2具有一主
體21,該主體21具有一根部211及一端部212及一上表面213及一下表面214並界定一主體厚度215,所述根部211及該端部212分別位於該主體21相反的兩端,該根部211與該輪轂1的外側表面連接。
Please refer to FIG. 2A and FIG. 2B and FIG. 2C. The present invention mainly includes a
該扇葉單元2的端部212界定一第一方向D1及一第二方向D2,該第一方向D1及該第二方向D2相互垂直,該第一方向D1為端部212的長邊,該第二方向D2為端部212的寬邊,該端部212設置有複數凸體,該等凸體進一步的界定為一第一凸體22及一第二凸體23,該第一凸體22及該第二凸體23沿著第一方向D1設置,該第一凸體22及該第二凸體23及端部212形成一凹槽3。
The
該第一凸體22具有一第一頂面221、一第一底面222、一第一左面223及一第一右面224並界定一第一凸體厚度225,該第二凸體23具有一第二頂面231、一第二底面232、一第二左面233及一第二右面234並界定一第二凸體厚度235,該第一底面222及該第二底面232與該端部212連接,進一步的,該第一凸體22及該第二凸體23及端部212可為一體成型製成或個別獨立分開的元件進行組合,一體成型可以透過灌模或除料或塑膠射出滑塊製程的方式製作出第一凸體22及第二凸體23,而個別獨立分開再組合可以透過嵌合、鉚合、扣合、黏合、鎖固、焊接或熔接等方式進行結合。
The first
該凹槽3具有一高度H及一寬度W,該寬度W的長短取決於該第一、二凸體22、23的長度,該高度H的大小取決於該第一、二凸體22、23的厚度,也就是說可以透過控制該第一、二凸體22、23的長度及厚度來決定該凹槽3的高度H及寬度W。
The
請參考第2A圖、第2B圖、第2C圖及第2D圖,當該輪轂1轉動時帶動該扇葉單元2高速旋轉,該凹槽3的內部如同一個流體死區,流體在凹槽3的
內部產生微型渦流,使該凹槽3與風扇外框壁4之間產生一個高壓區HPA,如此下方的氣流(下表面214下方的氣體)就無法穿過扇葉單元2與風扇外框壁4的間隙與上方的氣流(上表面213上方的氣體)交互作用而產生翼尖渦流,進而避免翼尖渦流產生的噪音、降低端部震動進而提升風扇特性。
Please refer to Figures 2A, 2B, 2C, and 2D. When the
尤其要說明的,前述凹槽3的高度H及寬度W會影響高壓區HPA的大小,當寬度W越大時,所能產生的高壓區HPA強度越大,當高度H越大時,所能產生的高壓區HPA範圍越大,所以可以根據風扇工作時的工作點需求來決定最佳的高度H及寬度W。
In particular, the height H and the width W of the
請參閱第3A圖、第3B圖、第3C圖、第3D圖、第3E圖、第3F圖、第3G圖及第3H圖,並輔以參考第2A圖至第2D圖,分別為不同態樣的扇葉單元2,這些實施例變化具有相同的技術特徵,皆為雙凸體單凹槽的結構,第3A~3D圖是由該扇葉單元2的側視角度對凹槽3進行說明,第3E~3H圖是該扇葉單元2的端部212角度俯視對凹槽3進行說明。
Please refer to Figures 3A, 3B, 3C, 3D, 3E, 3F, 3G, and 3H, and refer to Figures 2A to 2D, which are different states. For the
第3A圖的第一右面224及第二左面233為傾斜態樣,使凹槽3呈現三角形,這樣有助於高壓區HPA更快的產生,進一步的凹槽3還可為圓形、橢圓形、平行四邊形、梯形、正多邊形或非對稱形狀。
第3B圖的第一左面223與上表面213之間有一高低差(非連續平面),該第二右面234與下表面214有一高低差(非連續平面),這些高低差產生了導引氣流的效果,讓扇葉單元2下方的氣流更難以靠近凹槽3所產生的高壓區HPA,更加強化了抑制翼尖渦流的產生。
The first
第3C圖的第一左面223及第二右面234為傾斜態樣,上表面213與第一左面223為連續但不平行的平面,下表面214與第二右面234為連續但不平行的
平面,第一、二凸體22、23的這種形狀產生了阻擋氣流的效果,讓扇葉單元2下方的氣流更難以靠近凹槽3所產生的高壓區HPA,更加強化了抑制翼尖渦流的產生。
The first
第3D圖的端部212具有複數受接部,第一凸體22的第一底面222具有一組合部,第二凸體23的第二底面232具有一組合部,透過組合的方式可以調整凹槽3的高度H,或替換成其他形狀的第一、二凸體22、23改變凹槽3的形狀或產生上述第3B圖中提到的高低差,達到快速改變凹槽3形狀的功效。
The
上述的各種技術特徵可以任意的搭配使用,例如第3A圖及第3C圖的特徵結合,讓第一、二凸體22、23呈現三角形態樣,達到更快產生高壓區及阻擋氣流的效果,或者第3B圖與第3C圖的特徵結合,達到更快產生高壓區及導引氣流的效果。
The above various technical features can be used in any combination. For example, the combination of the features of Figures 3A and 3C allows the first and second
進一步的,在第3B、3C、3D圖的實施例中,第一、二凸體厚度225、235及凹槽3高度H及第一、二導槽25、26的導槽厚度總和不大於該主體厚度215。
Further, in the embodiments of FIGS. 3B, 3C, and 3D, the sum of the thicknesses of the first and second
第3E圖的第一凸體22、第二凸體23相互平行且等距設置,使該凹槽3每一處的寬度W皆相同且置中,這樣的設置方式使高壓區HPA穩定的產生於該扇葉單元2的同一處。
The first
第3F圖的第一凸體22、第二凸體23為傾斜設置,使凹槽3逐漸傾斜但該凹槽3每一處的高度H皆相同,這樣的設置方式配合葉片2轉動使高壓區HPA穩定的作用在風扇外框壁4的同一處。
The first
第3G圖的第一凸體22、第二凸體23為相互漸寬及漸縮的變化設置,使凹槽3漸擴及漸縮,該凹槽3的高度不相同,如圖中所示高度H1小於高度H1,這樣的設置方式使高壓區HPA隨著凹槽3的高度不同產生範圍變化。
The first
第3H圖的第一凸體22、第二凸體23為相互曲線設置,使凹槽3呈現一波浪形的態樣且每一處的高度H相同,這樣的設置方式使高壓區HPA隨著凹槽3的變化作用於風扇外框壁4的不同處,達到抑制翼尖渦流的產生。
The first
另外,雖然上述圖中的凹槽3相對於該扇葉單元2都是置中設置,但不限於此可以任意的設置,例如較靠近上表面213或下表面214以產生不同的抑制功效。
In addition, although the
特別需要說明的是,在上述的實施例中,第一凸體厚度225、第二凸體厚度235及凹槽3高度H的總和等於該主體厚度215,且第一凸體22的第一左面223不突出於主體21的上表面213,第二凸體23的第二右面234不突出於主體21的下表面214(請參閱第2C圖_),也就是說本案的扇葉單元2的總厚度不會因為設置凸體後而產生變化,扇葉單元2的總厚度等於主體厚度215。
In particular, in the above embodiment, the sum of the thickness of the first
請參考第4A圖及第4B圖,並輔與參考第2A~2D圖、第3A~3H圖,本實施例與上述實施例大致相同,相同之處不再贅述,其差異在於該端部212更具有一第三凸體24,該第三凸體24具有第三頂面241、第三底面242、第三左面243及第三右面244,該第三凸體24位於該第一凸體22及該第二凸體23之間。
Please refer to FIGS. 4A and 4B, supplemented by reference to FIGS. 2A to 2D and 3A to 3H. This embodiment is substantially the same as the above embodiment, and the same points are not repeated. The difference is that the end 212 A third
在本實施例中具有複數凹槽,一第一凹槽3a形成於該第一凸體22及該第三凸體24之間,該第一右面224、該端部212及該第三左面243包圍該第一凹
槽3a,一第二凹槽3b形成於該第二凸體23及該第三凸體24之間,該第三右面244、該端部212及該第二左面233包圍該第二凹槽3b。
In this embodiment, there are a plurality of grooves, a
所述該第三凸體24與端部212可為一體成型製成或個別獨立分開的元件進行組合,一體成型可以透過灌模或除料或塑膠射出或滑塊製程的方式製作出第一凸體22、第二凸體23及第三凸體24,而個別獨立分開再組合可以透過嵌合、鉚合、扣合、黏合、鎖固、焊接或熔接等方式進行結合。
The third
請同時參閱第4A圖及第4B圖,第4A圖中的第三凸體24置中設置使第一凹槽3a及第二凹槽3b的寬度相同,第4B圖中的第三凸體24為非置中設置使第一凹槽3a及第二凹槽3b的寬度相異,透過增加了第三凸體24產生了第一凹槽3a及第二凹槽3b,進而產生兩個高壓區,使下方的氣流更難以穿過扇葉單元2與風扇外框壁4的間隙與上方的氣流交互作用而產生翼尖渦流。
Please refer to FIG. 4A and FIG. 4B at the same time. The
進一步的,上述的第一、二、三凸體22、23、24都可以任意運用搭配第3A圖至第3H圖的技術特徵,進而產生同樣的功效,故在此不再贅述,該第一、二、三凸體22、23、24可為相同材質或相異材質,該材質包括高分子材料及金屬材料及複合材料其中任一。
Further, the above-mentioned first, second, and third
特別需要說明的是,在上述的實施例中,第一凸體厚度225、第二凸體厚度235、第三凸體厚度245及該凹槽3高度H1、H2的總和不大於該主體厚度215,且第一凸體22的第一左面223不突出於主體21的上表面213,第二凸體23的第二右面234不突出於主體21的下表面214(請參閱第4A、4B圖_),也就是說本案的扇葉單元2的總厚度不會因為設置凸體後而產生變化,扇葉單元2的總厚度等於主體厚度215。
In particular, in the above embodiment, the sum of the thickness of the first
另外,雖然上述僅提到三個凸體以產生兩個凹槽,但不限於此,能更進一步的增加第四凸體或第五凸體形成更多的凹槽,這些增加的凸體皆設於第一、二凸體22、23之間,當凹槽數量為三個以上,可以透過凸體之間的設置變化使這些凹槽具有全相同高度、全相異高度或者部分相同或部分相異,根據使用需求來加以規劃以產生不同的高壓區。
In addition, although only three convex bodies are mentioned above to produce two grooves, but it is not limited to this, the fourth convex body or the fifth convex body can be further added to form more grooves, and all of these added convex bodies Located between the first and second
綜上所述,本發明具有下述優點:1、抑制氣流在翼尖產生渦流;2、提升風扇工作特性;3、降低扇葉端部震動;4、降低噪音;5、凹槽結構調整變化容易;6、扇葉整體厚度不變。 In summary, the present invention has the following advantages: 1. Suppresses the vortex generated by the airflow at the wing tip; 2. Improves the fan's operating characteristics; 3. Reduces the blade end vibration; 4. Reduces the noise; 5. The groove structure adjustment changes Easy; 6. The overall thickness of the fan blade is unchanged.
惟以上所述者,僅係本發明之較佳可行之實施例而已,舉凡利用本發明上述之方法、形狀、構造、裝置所為之變化,皆應包含於本案之權利範圍內。 However, the above are only preferred and feasible embodiments of the present invention, and any changes made by using the above-mentioned methods, shapes, structures, and devices of the present invention should be included in the scope of the rights of this case.
1‧‧‧輪轂 1‧‧‧Wheel
2‧‧‧扇葉單元 2‧‧‧Fan unit
21‧‧‧主體 21‧‧‧Main
211‧‧‧根部 211‧‧‧Root
212‧‧‧端部 212‧‧‧End
22‧‧‧第一凸體 22‧‧‧The first convex body
23‧‧‧第二凸體 23‧‧‧Second convex body
3‧‧‧凹槽 3‧‧‧groove
Claims (14)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW107134129A TWI683062B (en) | 2018-09-27 | 2018-09-27 | Fan blade unit and fan impeller structure thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TW107134129A TWI683062B (en) | 2018-09-27 | 2018-09-27 | Fan blade unit and fan impeller structure thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
TWI683062B true TWI683062B (en) | 2020-01-21 |
TW202012794A TW202012794A (en) | 2020-04-01 |
Family
ID=69942927
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
TW107134129A TWI683062B (en) | 2018-09-27 | 2018-09-27 | Fan blade unit and fan impeller structure thereof |
Country Status (1)
Country | Link |
---|---|
TW (1) | TWI683062B (en) |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006214371A (en) * | 2005-02-04 | 2006-08-17 | Matsushita Electric Ind Co Ltd | Blower |
TWI596281B (en) * | 2017-03-23 | 2017-08-21 | Asia Vital Components Co Ltd | Fan structure |
-
2018
- 2018-09-27 TW TW107134129A patent/TWI683062B/en active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2006214371A (en) * | 2005-02-04 | 2006-08-17 | Matsushita Electric Ind Co Ltd | Blower |
TWI596281B (en) * | 2017-03-23 | 2017-08-21 | Asia Vital Components Co Ltd | Fan structure |
Also Published As
Publication number | Publication date |
---|---|
TW202012794A (en) | 2020-04-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7597544B2 (en) | Blade of axial flow-type rotary fluid machine | |
US8245519B1 (en) | Laser shaped film cooling hole | |
US20110206527A1 (en) | Compressor aerofoil | |
JP2010530333A (en) | Small wings | |
US20180119555A1 (en) | Gas turbine engine airfoils having multimodal thickness distributions | |
EP3168459A1 (en) | Vortex generator, wind turbine blade, and wind turbine power generating apparatus | |
US10634159B2 (en) | Heat dissipation fan blade structure and heat dissipation fan thereof | |
EA028485B1 (en) | Centrifugal machine | |
JP2015127541A5 (en) | ||
US9631648B2 (en) | Flow body with low-friction surface structure | |
JP2003278696A (en) | Propeller fan | |
TWI683062B (en) | Fan blade unit and fan impeller structure thereof | |
WO2011098807A1 (en) | Apparatus and Method for Aerodynamic Drag Reduction | |
JP6121046B2 (en) | Axial blower | |
JP6734576B2 (en) | Fan and compressor wings | |
CN208918910U (en) | Blade unit and its fan wheel structure | |
JPH049718B2 (en) | ||
TWM575063U (en) | Fan blade unit and its fan wheel structure | |
US11473591B2 (en) | Fan blade unit and fan impeller structure thereof | |
CN107021202B (en) | Aircraft nose with edge | |
KR101852572B1 (en) | Axial Fan | |
CN113847277B (en) | Supersonic porous adsorption type compressor blade with corrugated grooves on suction surface | |
US20200157942A1 (en) | Method for modifying blades of fan, compressor and turbine of axial flow type, and blade obtained by modification | |
TWI618863B (en) | Heat dissipation fan blade structure and heat dissipation fan thereof | |
WO2019216350A1 (en) | Aircraft with no vertical tail |