CN211259124U - Ultra-silent structure flabellum - Google Patents
Ultra-silent structure flabellum Download PDFInfo
- Publication number
- CN211259124U CN211259124U CN201921926979.XU CN201921926979U CN211259124U CN 211259124 U CN211259124 U CN 211259124U CN 201921926979 U CN201921926979 U CN 201921926979U CN 211259124 U CN211259124 U CN 211259124U
- Authority
- CN
- China
- Prior art keywords
- blade
- vortexes
- vortex
- reverse
- noise
- Prior art date
- 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.)
- Expired - Fee Related
Links
- 241000883990 Flabellum Species 0.000 title claims abstract description 8
- 244000126211 Hericium coralloides Species 0.000 claims abstract description 8
- 239000002131 composite material Substances 0.000 claims description 4
- 239000002657 fibrous material Substances 0.000 claims description 4
- 239000007769 metal material Substances 0.000 claims description 4
- 239000004033 plastic Substances 0.000 claims description 4
- 239000000835 fiber Substances 0.000 claims description 2
- 230000003116 impacting effect Effects 0.000 abstract description 4
- 238000000926 separation method Methods 0.000 abstract description 3
- 241001415849 Strigiformes Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000001968 nicotinic acid Nutrition 0.000 description 1
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model discloses a super-silent structure flabellum, including the blade, its characterized in that: the front edge and the rear edge of each blade are provided with comb tooth structures; the upper surface and the lower surface of the blade are covered with a convex structure. The front edge comb teeth can uniformly divide and break high-frequency vortexes generated by the front edge of the blade impacting air into smaller lower-frequency vortexes, and can generate reverse vortexes and transmit the reverse vortexes to a boundary layer on the surface of the blade, so that the separation of the boundary layer is weakened, and the vortex shedding noise is reduced; the raised structure on the surface of the blade can increase the thickness and stability of the boundary layer of the blade, and form a layer of air film on the surface of the blade, thereby preventing high-speed air flow from directly rubbing the blade to generate friction noise and better transmitting reverse vortex generated by front-edge comb teeth; the rear edge comb teeth can effectively level turbulence and vortex after the high-speed airflow is separated from the blades and the transmitted reverse vortex, so that the airflow wake of the blades is smooth, and finally, the noise is comprehensively reduced.
Description
Technical Field
The utility model relates to a flabellum technical field especially relates to a super-silent structure flabellum.
Background
Fan blade structures such as fans and propellers are widely used in many aspects of human life and work, including fans, air conditioners, airplanes, helicopters, steam turbines and the like, but due to the problem of blade design, noise which is difficult to ignore is generated when the blades rotate at high speed, and the human health is damaged to different degrees after the blades are in the environment for a long time.
When the fan or the propeller rotates at high speed, the noise generated by the blades mainly comes from three aspects: first, the pressure of the air impacting the leading edge of the blade; second, the friction force between the surface of the blade and the air; and thirdly, the air is discretely collided at the trailing edge of the blade through the vortex generated by the blade. A large number of bionics studies on owls show that noise can be reduced comprehensively by improving the blade design.
However, most of the current fan blade noise reduction designs are realized by only reducing the rotating speed of the blades, and other noise reduction modes are not emphasized or considered a little.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problems of the prior art, and the object of the utility model is to provide a super-silent structure fan blade, which can greatly reduce the noise generated when a fan or a propeller rotates at high speed and weaken the air impulse of the fan blade structure.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an ultra-silent structure flabellum, includes the blade, its characterized in that: the front edge and the rear edge of each blade are provided with comb tooth structures; the upper surface and the lower surface of the blade are covered with a convex structure.
The comb tooth structure is one or more of comb teeth, saw teeth, rows of spikes, brushes and wings.
The raised structure is one or more of short thorns, seta, fluff, fibers and scales.
The convex structure inclines forwards or backwards.
The comb tooth structure is made of one or more of plastic, fiber, metal and composite material.
The protruding structure is made of one or more of plastic, fiber, metal and composite material.
Due to the adoption of the scheme, the beneficial effects of the utility model are that:
the front edge comb teeth can uniformly divide and break high-frequency vortexes generated by the front edge of the blade impacting air into smaller lower-frequency vortexes, and can generate reverse vortexes and transmit the reverse vortexes to a boundary layer on the surface of the blade, so that the separation of the boundary layer is weakened, and the vortex shedding noise is reduced; the raised structure on the surface of the blade can increase the thickness and stability of the boundary layer of the blade, and form a layer of air film on the surface of the blade, thereby preventing high-speed air flow from directly rubbing the blade to generate friction noise and better transmitting reverse vortex generated by front-edge comb teeth; the rear edge comb teeth can effectively level turbulence and vortex after the high-speed airflow is separated from the blades and the transmitted reverse vortex, so that the airflow wake of the blades is smooth, and finally, the noise is comprehensively reduced.
Drawings
Fig. 1 is an isometric view of an embodiment of the present invention.
FIG. 2 is an isometric view of a single blade of the embodiment shown in FIG. 1.
In the figure: 1. the blade, 2, the front edge spine, 3, the rear edge comb teeth and 4, the surface burr.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and specific embodiments.
Fig. 1 to 2 show an ultra-silent structure of an unmanned aerial vehicle fan blade, which comprises a blade 1, a front edge spine 2, a rear edge comb tooth 3, and surface burrs 4.
The body of the blade 1, the front edge spine 2, the rear edge comb teeth 3 and the surface burrs 4 are made of ABS material and are integrally injection molded. The flabellum is that axisymmetric two curved surface blades 1 of thickness 1mm constitute, and the front edge of every blade 1 is one row of spine 2 of length 2mm, and the trailing edge is one row of broach 3 of length 15mm, and 1 surface evenly distributed of blade is long 2mm burr 4, and burr 4 all hypsokinesis 60.
When the fan blades rotate at a high speed, after impact air flow impacting the front edges of the blades 1 passes through the front edge spine 2, generated high-frequency vortexes are evenly divided and scattered into smaller low-frequency vortexes, and the front edge spine 2 can generate reverse vortexes and transmit the reverse vortexes to the surface boundary layers of the blades 1, so that the separation of the boundary layers is weakened, and the vortex shedding noise is reduced. The thickness and the stability of the boundary layer of the blade 1 are increased by the layer of burrs 4 covered on the outer surface of the blade 1, a layer of air film is formed on the surface of the blade 1, the high-speed air flow is prevented from directly rubbing with the surface of the blade 1 to generate friction noise, and reverse vortex generated by the front edge sharp burrs 2 can be better transmitted. The rear edge comb teeth 3 can effectively level turbulence and vortex after the high-speed airflow is separated from the blades 1 and transfer the reverse vortex, so that the airflow wake of the blades 1 is smooth, and finally, the noise is comprehensively reduced.
The present invention is not limited by the above embodiments, and the present invention can be modified in various ways without departing from the spirit and scope of the present invention, and these modifications and changes fall into the scope of the present invention.
Claims (6)
1. The utility model provides an ultra-silent structure flabellum, includes the blade, its characterized in that: the front edge and the rear edge of each blade are provided with comb tooth structures; the upper surface and the lower surface of the blade are covered with a convex structure.
2. The fan blade of claim 1, wherein: the comb tooth structure is one or more of comb teeth, saw teeth, rows of spikes, brushes and wings.
3. The fan blade of claim 1, wherein: the raised structure is one or more of short thorns, seta, fluff, fibers and scales.
4. The fan blade of claim 1, wherein: the convex structure inclines forwards or backwards.
5. The fan blade of claim 1, wherein: the comb tooth structure is made of one or more of plastic, fiber, metal and composite material.
6. The fan blade of claim 1, wherein: the protruding structure is made of one or more of plastic, fiber, metal and composite material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921926979.XU CN211259124U (en) | 2019-11-04 | 2019-11-04 | Ultra-silent structure flabellum |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921926979.XU CN211259124U (en) | 2019-11-04 | 2019-11-04 | Ultra-silent structure flabellum |
Publications (1)
Publication Number | Publication Date |
---|---|
CN211259124U true CN211259124U (en) | 2020-08-14 |
Family
ID=71988127
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201921926979.XU Expired - Fee Related CN211259124U (en) | 2019-11-04 | 2019-11-04 | Ultra-silent structure flabellum |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN211259124U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112848378A (en) * | 2020-12-26 | 2021-05-28 | 吉林大学 | Fiber reinforced composite blade material with bionic structure and preparation method thereof |
-
2019
- 2019-11-04 CN CN201921926979.XU patent/CN211259124U/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112848378A (en) * | 2020-12-26 | 2021-05-28 | 吉林大学 | Fiber reinforced composite blade material with bionic structure and preparation method thereof |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3177524B1 (en) | Wind turbine rotor blade | |
US10012207B2 (en) | Wind turbine blade noise reduction teeth with stiffening rib | |
US10117380B1 (en) | Systems and methods for reducing cutting blade noise | |
US20150233345A1 (en) | Wind turbine blade | |
CN201606315U (en) | Blade-tip clearance vortex flow restraining structure of ducted fan | |
JP2016508094A (en) | Propeller blade for turbomachinery | |
CN104791199B (en) | Blade trailing edge attachments and wind turbine blades | |
CN211259124U (en) | Ultra-silent structure flabellum | |
CN101603514A (en) | Bionic coupling blade of aerogenerator | |
WO2011098807A1 (en) | Apparatus and Method for Aerodynamic Drag Reduction | |
US20040091359A1 (en) | Blade and wing configuration | |
CN205707257U (en) | A kind of propeller reducing stress at blade root and reducing tip whirlpool | |
CN212690450U (en) | Take fan of making an uproar that falls of sawtooth | |
CN106564588B (en) | An unmanned helicopter blade and an unmanned helicopter | |
CN205349855U (en) | Fan blade with piece is strengthened to sectional type metal | |
GB2436861A (en) | Aerofoil | |
JP2012251448A (en) | Configurational form for blade noise reduction for propeller-type wind power generator of 10 m or larger diameter | |
CN112173075A (en) | Aerodynamic profile of helicopter low-noise rotor blade | |
JP4676633B2 (en) | Rotor blade of rotorcraft | |
CN212690449U (en) | Bionic annular noise reduction fan | |
EP2759471B1 (en) | Fluidfoil | |
CN114294264A (en) | Mute fan | |
CN216468434U (en) | High efficiency anti-vibration paddle structure | |
CN106401866B (en) | Blade-shaped wind turbine blades | |
CN206753831U (en) | A kind of noise-reducing blade of wind-driven generator |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200814 Termination date: 20211104 |