CN207865500U - A kind of turbine with supercharging fin and the kitchen ventilator comprising the turbine - Google Patents

A kind of turbine with supercharging fin and the kitchen ventilator comprising the turbine Download PDF

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CN207865500U
CN207865500U CN201820222275.3U CN201820222275U CN207865500U CN 207865500 U CN207865500 U CN 207865500U CN 201820222275 U CN201820222275 U CN 201820222275U CN 207865500 U CN207865500 U CN 207865500U
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turbine
fins
booster
supercharging
volute
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徐新建
高绪元
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Zhejiang Shuaikang Electric Stock Co Ltd
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Zhejiang Shuaikang Electric Stock Co Ltd
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Abstract

本申请涉及一种带有增压翅片的涡轮及包含该涡轮的油烟机。涡轮包括顶圈和底圈,叶片周向排布在顶圈和底圈之间,叶片包括交替设置的第一叶片和第二叶片,第二叶片包括增压翅片。通过设置增压翅片可以实现涡轮叶片的二次增压,首先通过第二叶片的增压翅片对气流进行增压,然后再通过第二叶片的本体部分和第一叶片进行增压,实验结果显示涡轮的压力和抽吸力可以增大20%左右。

The present application relates to a turbine with supercharging fins and a range hood comprising the turbine. The turbine includes a top ring and a bottom ring, and blades are circumferentially arranged between the top ring and the bottom ring. The blades include alternately arranged first blades and second blades, and the second blades include supercharging fins. The secondary supercharging of turbine blades can be realized by setting supercharging fins. Firstly, the airflow is supercharged through the supercharging fins of the second vane, and then supercharged through the body part of the second vane and the first vane. The experiment The results show that the pressure and suction of the turbine can be increased by about 20%.

Description

一种带有增压翅片的涡轮及包含该涡轮的油烟机Turbine with supercharging fins and range hood comprising the same

技术领域technical field

本申请涉及一种带有增压翅片的涡轮及包含该涡轮的油烟机,适用于油烟机的技术领域。The present application relates to a turbine with supercharging fins and a range hood including the turbine, which are suitable for the technical field of range hoods.

背景技术Background technique

吸油烟机是一种净化厨房环境的厨房电器。随着人们生活质量的日益提高,吸油烟机已成为现代家庭必不可少的厨房设备。通常安装在厨房炉灶上方,能将炉灶燃烧的废物和烹饪过程中产生的油烟迅速抽走并排出室外,减少室内污染,净化空气,并有防毒、防爆的安全保障作用。现有的吸油烟机中通常会发生不能够将烹饪过程中产生的油烟完全抽走的问题,导致屋内仍然有油烟的味道。产生这种现象的一个原因是吸油烟机的抽吸效果不佳。解决这一问题最常用的办法就是增大吸油烟机的电机功率和涡轮的转动速度,从而增大抽吸效果。但随之带来的问题是由于涡轮转速的增加而导致的噪音增大,影响了吸油烟机的用户体验。因此,如何能够尽可能地增大吸油烟机的抽吸效率,同时又能够降低吸油烟机的噪音成为本领域急需解决的技术问题。The range hood is a kitchen appliance that purifies the kitchen environment. With the improvement of people's quality of life, the range hood has become an indispensable kitchen equipment for modern families. Usually installed above the kitchen stove, it can quickly take away the waste burned by the stove and the oily fume generated during the cooking process and discharge it outside, reduce indoor pollution, purify the air, and have the function of anti-virus and explosion-proof safety guarantee. In the existing range hood, there is usually a problem that the oil fume generated during the cooking process cannot be completely sucked away, resulting in the smell of oil fume in the house. One reason for this phenomenon is that the suction effect of the range hood is not good. The most common way to solve this problem is to increase the motor power of the range hood and the speed of rotation of the turbine, thereby increasing the suction effect. But the problem that follows is that the noise increases due to the increase of the turbine speed, which affects the user experience of the range hood. Therefore, how to increase the suction efficiency of the range hood as much as possible and at the same time reduce the noise of the range hood has become an urgent technical problem in this field.

同时,现有技术中涡轮的叶片一般都是相同形状的弧状结构,沿周向间隔排布。从而在相邻叶片之间留有空隙,以便使气流从空隙中流动。现有技术中蜗壳的风道一般都是平顺的风道,其流量基本恒定、噪音较大。At the same time, the blades of the turbine in the prior art are generally arc-shaped structures of the same shape, arranged at intervals along the circumferential direction. Gaps are thus left between adjacent vanes for airflow to flow through the gaps. The air ducts of the volute in the prior art are generally smooth air ducts, the flow rate of which is basically constant, and the noise is relatively large.

实用新型内容Utility model content

本申请为克服现有技术中的上述缺陷,提供了一种带有增压翅片的涡轮及包含该涡轮的油烟机,不仅能够增大涡轮的压力和抽吸力,而且还能够降低涡轮的噪音。In order to overcome the above-mentioned defects in the prior art, the present application provides a turbine with supercharging fins and a range hood containing the turbine, which can not only increase the pressure and suction force of the turbine, but also reduce the pressure of the turbine. noise.

根据本申请的一种带有增压翅片的涡轮,包括顶圈和底圈,叶片周向排布在所述顶圈和所述底圈之间,所述叶片包括交替设置的第一叶片和第二叶片,所述第二叶片包括增压翅片。According to the present application, a turbine with supercharger fins comprises a top ring and a bottom ring, blades are circumferentially arranged between the top ring and the bottom ring, and the blades include alternately arranged first blades and a second vane including booster fins.

优选地,所述第二叶片的本体可以与所述第一叶片相同,所述本体的两端分别设置于所述顶圈和所述底圈上,所述增压翅片的高度小于所述本体的高度。所述增压翅片的内侧边可以呈波浪形或锯齿形。所述增压翅片的端部与所述顶圈不接触,并且/或者所述增压翅片的端部与所述底圈不接触。Preferably, the body of the second vane may be the same as that of the first vane, the two ends of the body are respectively arranged on the top ring and the bottom ring, and the height of the booster fin is smaller than that of the The height of the body. The inner sides of the booster fins may be wavy or zigzag. The ends of the booster fins are not in contact with the top ring, and/or the ends of the booster fins are not in contact with the bottom ring.

优选地,所述增压翅片的高度为所述本体的高度的1/3~4/5,并且/或者所述增压翅片的宽度为所述本体的宽度的1/3~4/5。更优选地,所述增压翅片设置在所述本体的中间位置,并与所述本体一体成型。Preferably, the height of the booster fins is 1/3-4/5 of the height of the body, and/or the width of the booster fins is 1/3-4/5 of the width of the body 5. More preferably, the booster fins are arranged in the middle of the body and integrally formed with the body.

本申请的另一方面涉及一种吸油烟机,包括外壳,所述外壳的内部设有涡轮组件,所述涡轮组件包括蜗壳和涡轮,其特征在于,所述涡轮是如上所述的带有增压翅片的涡轮。Another aspect of the present application relates to a range hood, which includes a casing, and a turbine assembly is arranged inside the casing, and the turbine assembly includes a volute and a turbine, and the feature is that the turbine is as described above with Supercharged finned turbo.

优选地,所述涡轮组件还包括与所述涡轮相互装配的涡轮中板,所述涡轮中板设置在所述增压翅片的中间高度位置处。更优选地,所述涡轮中板的中部具有突出的鼓出面。Preferably, the turbine assembly further includes a turbine middle plate assembled with the turbine, and the turbine middle plate is arranged at a middle height position of the supercharging fin. More preferably, the middle part of the turbine middle plate has a protruding bulging surface.

优选地,所述蜗壳包括蜗腔,所述蜗腔与出风口连通,所述蜗壳的两个侧面均分别设有缓冲仓。Preferably, the volute includes a volute, the volute communicates with the air outlet, and two sides of the volute are respectively provided with buffer chambers.

本申请中通过设置增压翅片可以实现涡轮叶片的二次增压,首先通过第二叶片的增压翅片对气流进行增压,然后再通过第二叶片的本体部分和第一叶片进行增压,实验结果显示涡轮的压力和抽吸力可以增大20%左右。另外,通过将增压翅片的内侧边设置为波浪形或锯齿形,可以使其具有湍流器的功效,能够有效降低涡轮转动时的噪音。In this application, the secondary supercharging of the turbine blades can be realized by setting the supercharging fins. First, the airflow is supercharged through the supercharging fins of the second vanes, and then the air is boosted through the body part of the second vanes and the first vanes. The experimental results show that the pressure and suction force of the turbine can be increased by about 20%. In addition, by arranging the inner side of the booster fin in a wavy or zigzag shape, it can function as a turbulator, which can effectively reduce the noise when the turbine rotates.

本申请中通过缓冲仓的设置,有效地增加了蜗壳的轴向尺寸,使得蜗壳变成了一个同时包括轴向蜗壳和径向蜗壳的混合蜗壳,能够有效地缓冲气流、减小噪音、增加风量。In this application, the axial dimension of the volute is effectively increased through the setting of the buffer chamber, so that the volute becomes a mixed volute including both the axial volute and the radial volute, which can effectively buffer the airflow and reduce the Small noise, increased air volume.

附图说明Description of drawings

图1显示了根据本申请的吸油烟机的立体示意图。Fig. 1 shows a schematic perspective view of a range hood according to the present application.

图2显示了涡轮组件的前视立体图。Figure 2 shows a front perspective view of the turbine assembly.

图3显示了涡轮组件的后视立体图。Figure 3 shows a rear perspective view of the turbine assembly.

图4显示了根据本申请的带有增压翅片的涡轮的前视立体图。Figure 4 shows a front perspective view of a turbine with booster fins according to the present application.

图5显示了根据本申请的带有增压翅片的涡轮的后视立体图。Figure 5 shows a rear perspective view of a turbine with booster fins according to the present application.

图6显示了根据本申请的带有增压翅片的第二叶片的示意图。Figure 6 shows a schematic diagram of a second vane with booster fins according to the present application.

图7显示了蜗壳的另一种实施方式的前视立体图。Figure 7 shows a front perspective view of another embodiment of the volute.

图8显示了蜗壳的另一种实施方式的后视立体图。Figure 8 shows a rear perspective view of another embodiment of the volute.

图9显示了蜗壳的另一种实施方式的侧视图。Figure 9 shows a side view of another embodiment of the volute.

具体实施方式Detailed ways

为使本实用新型的目的、技术方案和优点更加清楚明白,下文中将结合附图对本实用新型的实施例进行详细说明。需要说明的是,在不冲突的情况下,本申请中的实施例及实施例中的特征可以相互任意组合。本申请中的方向术语,例如“前后左右”、“上下外内”等均是为了描述的方便,并不构成对保护范围的限定。本领域技术人员知道上述方向之间的简单替换并不脱离本申请的保护范围。In order to make the purpose, technical solutions and advantages of the present utility model clearer, the embodiments of the present utility model will be described in detail below in conjunction with the accompanying drawings. It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined arbitrarily with each other. The directional terms in this application, such as "front, back, left, right", "up, down, outside, inside", etc., are for the convenience of description and do not constitute a limitation on the scope of protection. Those skilled in the art know that simple substitutions between the above directions do not depart from the protection scope of the present application.

如图1所示,其中显示了根据本申请的吸油烟机的立体示意图。如图所示,吸油烟机包括外壳1、操控台2、导流板3和收油盒4,外壳1的内部设有涡轮组件。导流板3设置在外壳的下部,导流板3的外部还可以设有网罩5。As shown in FIG. 1 , it shows a perspective view of a range hood according to the present application. As shown in the figure, the range hood includes a casing 1 , a console 2 , a deflector 3 and an oil collection box 4 , and a turbine assembly is arranged inside the casing 1 . The deflector 3 is arranged at the lower part of the casing, and the outside of the deflector 3 may also be provided with a mesh cover 5 .

如图2和3所示,其中分别显示了涡轮组件的前视立体图和后视立体图。涡轮组件的上部设有出风口6,出风口与排烟通道相连,以将油烟排出油烟机的外部。涡轮组件包括蜗壳11、相互装配的涡轮10和涡轮中板12,蜗壳11和涡轮10之间还可以设有导风圈13。导风圈除了能够导风以外,还可以具有消音、阻止涡流产生等效果。涡轮中板12的中间设有轴孔,旋转电机的电机轴穿过轴孔,旋转电机固定在蜗壳11上,而涡轮10和涡轮中板12通过电机轴固定在旋转电机上。优选地,如图3所示,还可以在涡轮10的背面设置支撑件14,以将涡轮支撑在蜗壳上。如图2和3所示,其中的涡轮叶片为常规的形状,即涡轮的叶片沿周向间隔布置,叶片的截面为弧状结构。As shown in Figures 2 and 3, a front perspective view and a rear perspective view of the turbine assembly are shown, respectively. The upper part of the turbine assembly is provided with an air outlet 6, and the air outlet is connected with the smoke exhaust channel to discharge the oil fume to the outside of the range hood. The turbine assembly includes a volute 11 , a mutually assembled turbine 10 and a turbine middle plate 12 , and a wind guide ring 13 may also be provided between the volute 11 and the turbine 10 . In addition to being able to guide the wind, the wind guide ring can also have effects such as noise reduction and prevention of eddy current generation. The center of the turbine middle plate 12 is provided with a shaft hole, the motor shaft of the rotating motor passes through the shaft hole, the rotating motor is fixed on the volute 11, and the turbine 10 and the turbine middle plate 12 are fixed on the rotating motor through the motor shaft. Preferably, as shown in FIG. 3 , a support 14 may also be provided on the back of the turbine 10 to support the turbine on the volute. As shown in Figures 2 and 3, the turbine blades are in a conventional shape, that is, the blades of the turbine are arranged at intervals in the circumferential direction, and the cross-section of the blades is an arc-shaped structure.

如图4和5所示,其中显示了根据本申请的带有增压翅片的涡轮的前视立体图和后视立体图。如图所示,涡轮包括顶圈15和底圈16,叶片17周向排布在顶圈15和底圈16之间,叶片包括交替设置的第一叶片171和第二叶片170,第二叶片170还包括增压翅片172,即相当于在第一叶片171的基础上增设增压翅片172。如图4和5所示,优选地,涡轮中板12的中部具有突出的鼓出面18,这样可以在涡轮的吸风侧形成更大的风腔,以加大吸力,同时便于安装电机的电机轴。As shown in Figures 4 and 5, there are shown a front perspective view and a rear perspective view of a turbine with booster fins according to the present application. As shown in the figure, the turbine includes a top ring 15 and a bottom ring 16, and blades 17 are circumferentially arranged between the top ring 15 and the bottom ring 16, and the blades include alternately arranged first blades 171 and second blades 170, the second blades 170 also includes a booster fin 172 , which is equivalent to adding a booster fin 172 on the basis of the first vane 171 . As shown in Figures 4 and 5, preferably, the middle part of the turbine middle plate 12 has a protruding bulging surface 18, which can form a larger air cavity on the suction side of the turbine to increase the suction force and facilitate the installation of the motor of the motor axis.

如图6所示,显示了根据本申请的带有增压翅片的第二叶片的示意图。第二叶片170的本体173与第一叶片171相同,截面均为弧状结构。本体173的两端分别设置于顶圈15和底圈16上,增压翅片172的高度小于本体173的高度,增压翅片172的端部与顶圈15不接触,甚至与底圈16也不接触。增压翅片172的高度可以为本体17的高度的1/6~5/6,增压翅片172的宽度可以为本体17的宽度的1/6~5/6;上述比值的优选范围是1/3~4/5,最优值是1/2。As shown in FIG. 6 , a schematic diagram of a second vane with booster fins according to the present application is shown. The body 173 of the second vane 170 is the same as the first vane 171 , and both have an arc-shaped cross section. The two ends of the body 173 are respectively arranged on the top ring 15 and the bottom ring 16. The height of the booster fins 172 is smaller than the height of the body 173. The ends of the booster fins 172 are not in contact with the top ring 15, even the bottom ring 16 No contact either. The height of booster fin 172 can be 1/6~5/6 of the height of body 17, and the width of booster fin 172 can be 1/6~5/6 of the width of body 17; The preferred range of above-mentioned ratio is 1/3~4/5, the optimal value is 1/2.

涡轮中板可以设置在增压翅片172的中间高度位置处。增压翅片172可以设置在本体17的中间位置,并与本体173一体成型。优选地,涡轮旋转时,第一叶片171的内圆周轮廓线的半径可以为15cm,增压翅片172的内圆周轮廓线的半径可以为14cm,也即增压翅片172的宽度可以是1cm。增压翅片172的内侧边呈波浪形或锯齿形。The turbine midplate may be disposed at a mid-height position of the booster fins 172 . The booster fins 172 can be disposed in the middle of the body 17 and integrally formed with the body 173 . Preferably, when the turbine rotates, the radius of the inner circumference outline of the first blade 171 can be 15cm, and the radius of the inner circumference outline of the booster fin 172 can be 14cm, that is, the width of the booster fin 172 can be 1cm . The inner sides of the booster fins 172 are wavy or zigzag.

通过设置增压翅片可以实现涡轮叶片的二次增压,即首先通过第二叶片的增压翅片对气流进行增压,然后再通过第二叶片的本体部分和第一叶片进行增压,实验结果显示涡轮的压力和抽吸力可以增大20%左右。另外,通过将增压翅片的内侧边设置为波浪形或锯齿形,可以使其具有湍流器的功效,能够有效降低涡轮转动时的噪音。The secondary supercharging of the turbine blades can be achieved by setting the supercharging fins, that is, the airflow is firstly supercharged through the supercharging fins of the second vane, and then supercharged through the body part of the second vane and the first vane, Experimental results show that the pressure and suction force of the turbine can be increased by about 20%. In addition, by arranging the inner side of the booster fin in a wavy or zigzag shape, it can function as a turbulator, which can effectively reduce the noise when the turbine rotates.

如图7-9所示,其中显示了蜗壳的另一种实施方式的前视立体图和后视立体图。如图所示,蜗壳包括蜗腔113,蜗腔113与出风口连通,蜗壳的两个侧面均分别设有缓冲仓。如图7-9所示,缓冲仓包括第一缓冲仓111和第二缓冲仓112,第一缓冲仓111和第二缓冲仓112的大小不等,第一缓冲仓111和第二缓冲仓112均突出蜗壳的外表面。优选地,在同一侧面上,第一缓冲仓111和第二缓冲仓112可以沿环向相对布置;在不同侧面上,两个第一缓冲仓对应设置,两个第二缓冲仓也对应设置。优选地,鼓风仓的高度可以是8-12mm,优选为9mm,鼓风仓的高度与相应位置处蜗壳的宽度之比可以是0.01-0.5。As shown in Figures 7-9, front and rear perspective views of another embodiment of a volute are shown. As shown in the figure, the volute includes a volute cavity 113, which communicates with the air outlet, and two sides of the volute are respectively provided with buffer chambers. As shown in Figures 7-9, the buffer bin includes a first buffer bin 111 and a second buffer bin 112, the first buffer bin 111 and the second buffer bin 112 have different sizes, the first buffer bin 111 and the second buffer bin 112 Both protrude from the outer surface of the volute. Preferably, on the same side, the first buffer bins 111 and the second buffer bins 112 may be circumferentially oppositely arranged; on different sides, the two first buffer bins are correspondingly arranged, and the two second buffer bins are also correspondingly arranged. Preferably, the height of the blast chamber can be 8-12mm, preferably 9mm, and the ratio of the height of the blast chamber to the width of the volute at the corresponding position can be 0.01-0.5.

该缓冲仓有效地增加了蜗壳的轴向尺寸,使得该蜗壳变成了一个同时包括轴向蜗壳和径向蜗壳的混合蜗壳,能够有效地缓冲气流、减小噪音、增加风量。实验结果显示,如此设置缓冲仓以后,蜗壳内的风量可以增加1立方米/分钟,噪音可以降低1分贝。The buffer chamber effectively increases the axial dimension of the volute, so that the volute becomes a mixed volute including both the axial volute and the radial volute, which can effectively buffer the airflow, reduce noise and increase the air volume . Experimental results show that after setting up the buffer chamber in this way, the air volume in the volute can be increased by 1 cubic meter per minute, and the noise can be reduced by 1 decibel.

虽然本实用新型所揭露的实施方式如上,但所述的内容只是为了便于理解本实用新型而采用的实施方式,并非用以限定本实用新型。任何本实用新型所属技术领域内的技术人员,在不脱离本实用新型所揭露的精神和范围的前提下,可以在实施的形式上及细节上作任何的修改与变化,但本实用新型的专利保护范围,仍须以所附的权利要求书所界定的范围为准。Although the embodiments disclosed in the present utility model are as above, the content described is only an embodiment adopted for the convenience of understanding the present utility model, and is not intended to limit the present utility model. Anyone skilled in the technical field to which the utility model belongs can make any modifications and changes in the form and details of the implementation without departing from the spirit and scope disclosed in the utility model, but the patent of the utility model The scope of protection must still be based on the scope defined in the appended claims.

Claims (10)

1.一种带有增压翅片的涡轮,包括顶圈和底圈,叶片周向排布在所述顶圈和所述底圈之间,其特征在于,所述叶片包括交替设置的第一叶片和第二叶片,所述第二叶片包括增压翅片。1. A turbine with booster fins, comprising a top ring and a bottom ring, the blades are circumferentially arranged between the top ring and the bottom ring, and it is characterized in that the blades include alternately arranged first A vane and a second vane, the second vane includes booster fins. 2.根据权利要求1所述的带有增压翅片的涡轮,其特征在于,所述第二叶片的本体与所述第一叶片相同,所述本体的两端分别设置于所述顶圈和所述底圈上,所述增压翅片的高度小于所述本体的高度。2. The turbine with booster fins according to claim 1, wherein the body of the second blade is the same as that of the first blade, and the two ends of the body are respectively arranged on the top ring And on the bottom ring, the height of the booster fins is smaller than the height of the body. 3.根据权利要求1所述的带有增压翅片的涡轮,其特征在于,所述增压翅片的内侧边呈波浪形或锯齿形。3. The turbine with booster fins according to claim 1, characterized in that, the inner sides of the booster fins are wavy or zigzag. 4.根据权利要求1-3中任一项所述的带有增压翅片的涡轮,其特征在于,所述增压翅片的端部与所述顶圈不接触,并且/或者所述增压翅片的端部与所述底圈不接触。4. The turbine with booster fins according to any one of claims 1-3, characterized in that, the ends of the booster fins are not in contact with the top ring, and/or the The ends of the booster fins are not in contact with the bottom ring. 5.根据权利要求2所述的带有增压翅片的涡轮,其特征在于,所述增压翅片的高度为所述本体的高度的1/3~4/5,并且/或者所述增压翅片的宽度为所述本体的宽度的1/3~4/5。5. The turbine with supercharging fins according to claim 2, characterized in that, the height of the supercharging fins is 1/3-4/5 of the height of the body, and/or the The width of the booster fins is 1/3-4/5 of the width of the main body. 6.根据权利要求2所述的带有增压翅片的涡轮,其特征在于,所述增压翅片设置在所述本体的中间位置,并与所述本体一体成型。6 . The turbine with supercharging fins according to claim 2 , wherein the supercharging fins are arranged at a middle position of the body and integrally formed with the body. 7 . 7.一种吸油烟机,包括外壳,所述外壳的内部设有涡轮组件,所述涡轮组件包括蜗壳和涡轮,其特征在于,所述涡轮是根据权利要求1-6中任一项所述的带有增压翅片的涡轮。7. A range hood, comprising a casing, a turbine assembly is provided inside the casing, and the turbine assembly includes a volute and a turbine, characterized in that, the turbine is according to any one of claims 1-6 Turbines with booster fins as described above. 8.根据权利要求7所述的吸油烟机,其特征在于,所述涡轮组件还包括与所述涡轮相互装配的涡轮中板,所述涡轮中板设置在所述增压翅片的中间高度位置处。8. The range hood according to claim 7, wherein the turbine assembly further comprises a turbine middle plate assembled with the turbine, and the turbine middle plate is arranged at the middle height of the booster fins location. 9.根据权利要求8所述的吸油烟机,其特征在于,所述涡轮中板的中部具有突出的鼓出面。9. The range hood according to claim 8, characterized in that, the middle part of the turbine middle plate has a protruding bulging surface. 10.根据权利要求7或8或9所述的吸油烟机,其特征在于,所述蜗壳包括蜗腔,所述蜗腔与出风口连通,所述蜗壳的两个侧面均分别设有缓冲仓。10. The range hood according to claim 7, 8 or 9, wherein the volute includes a volute, the volute communicates with the air outlet, and the two sides of the volute are respectively provided with Buffer warehouse.
CN201820222275.3U 2018-02-08 2018-02-08 A kind of turbine with supercharging fin and the kitchen ventilator comprising the turbine Expired - Fee Related CN207865500U (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108240355A (en) * 2018-02-08 2018-07-03 浙江帅康电气股份有限公司 A kind of spiral case with surge bunker and the kitchen ventilator comprising the spiral case
CN108253488A (en) * 2018-02-08 2018-07-06 浙江帅康电气股份有限公司 A kind of turbine with supercharging fin and the kitchen ventilator comprising the turbine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108240355A (en) * 2018-02-08 2018-07-03 浙江帅康电气股份有限公司 A kind of spiral case with surge bunker and the kitchen ventilator comprising the spiral case
CN108253488A (en) * 2018-02-08 2018-07-06 浙江帅康电气股份有限公司 A kind of turbine with supercharging fin and the kitchen ventilator comprising the turbine
CN108253488B (en) * 2018-02-08 2024-03-29 浙江帅康电气股份有限公司 Turbine with booster fins and range hood comprising turbine
CN108240355B (en) * 2018-02-08 2024-08-13 浙江帅康电气股份有限公司 A volute with a buffer bin and a range hood including the volute

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