CA3020210C - Regulation aerodynamique de pales d'helice, de soufflante et d'eolienne avec des alesages et/ou une coupe et/ou un crantage - Google Patents
Regulation aerodynamique de pales d'helice, de soufflante et d'eolienne avec des alesages et/ou une coupe et/ou un crantage Download PDFInfo
- Publication number
- CA3020210C CA3020210C CA3020210A CA3020210A CA3020210C CA 3020210 C CA3020210 C CA 3020210C CA 3020210 A CA3020210 A CA 3020210A CA 3020210 A CA3020210 A CA 3020210A CA 3020210 C CA3020210 C CA 3020210C
- Authority
- CA
- Canada
- Prior art keywords
- blade
- notch
- blades
- airscrew
- tip
- 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.)
- Active
Links
- 230000000694 effects Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor
- F03D1/06—Rotors
- F03D1/0608—Rotors characterised by their aerodynamic shape
- F03D1/0633—Rotors characterised by their aerodynamic shape of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/18—Aerodynamic features
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05B2240/307—Blade tip, e.g. winglets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/182—Two-dimensional patterned crenellated, notched
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Wind Motors (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Une pale dhélice, une soufflante et une éolienne davion axial de faible charge caractérisées par le rapport daspect des pales faible; à proximité de lensemble des extrémités de pale, mais dans une distance appropriée, sont formées dans la pointe de chaque pale, qui sétend entre un côté pression et un côté aspiration, et un canal menant à lencoche formée à travers le corps de la pale entre les côtés. La distance entre lencoche et la pointe de la pale modifie le diamètre des pales de 1,2 % à 1,67 %, le long de la longueur de lencoche. Pendant lexploitation, lair sécoulant à travers cette ouverture élimine la turbulence formée à lextrémité des pales. Les vibrations en résonance survenant sur les pales et les éoliennes sont également réduites, ce qui étend la durée de vie des pales.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA3020210A CA3020210C (fr) | 2018-10-10 | 2018-10-10 | Regulation aerodynamique de pales d'helice, de soufflante et d'eolienne avec des alesages et/ou une coupe et/ou un crantage |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA3020210A CA3020210C (fr) | 2018-10-10 | 2018-10-10 | Regulation aerodynamique de pales d'helice, de soufflante et d'eolienne avec des alesages et/ou une coupe et/ou un crantage |
Publications (2)
Publication Number | Publication Date |
---|---|
CA3020210A1 CA3020210A1 (fr) | 2020-04-10 |
CA3020210C true CA3020210C (fr) | 2021-08-17 |
Family
ID=70155994
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA3020210A Active CA3020210C (fr) | 2018-10-10 | 2018-10-10 | Regulation aerodynamique de pales d'helice, de soufflante et d'eolienne avec des alesages et/ou une coupe et/ou un crantage |
Country Status (1)
Country | Link |
---|---|
CA (1) | CA3020210C (fr) |
-
2018
- 2018-10-10 CA CA3020210A patent/CA3020210C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
CA3020210A1 (fr) | 2020-04-10 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5131604A (en) | Helicopter antitorque device | |
US9932960B2 (en) | Rotor blade of a wind turbine | |
RU2007148890A (ru) | Лопасть несущего винта для высокоскоростного винтокрылого летательного аппарата | |
WO2019210110A1 (fr) | Système d'hélice ultra-silencieux | |
US10625847B2 (en) | Split winglet | |
US9340277B2 (en) | Airfoils for use in rotary machines | |
US11795975B2 (en) | Low noise and high efficiency blade for axial fans and rotors and axial fan or rotor comprising said blade | |
US20170073062A1 (en) | Variable Geometry Wingtip | |
JPH0341399B2 (fr) | ||
JPH036039B2 (fr) | ||
US8827201B2 (en) | Rotorcraft structural element for reducing aerodynamic drag | |
CN108750073B (zh) | 一种兼顾亚音速及超音速气动性能的可变机翼前缘 | |
US9475578B2 (en) | Rotary wing aircraft with a tail shroud | |
CA3060758C (fr) | Aeronef a soufflante canalisee rotative | |
CN211364914U (zh) | 旋翼飞行器的桨叶及旋翼飞行器 | |
US10730606B2 (en) | Systems, methods, and apparatuses for airfoil configuration in aircraft | |
US20200198763A9 (en) | Aerodynamic Regulation of Airscrew-, Fan- and Wind Turbine Blades with Bores and/or Cutting and/or Notching | |
US6899525B2 (en) | Blade and wing configuration | |
AU2018101230A4 (en) | Aerodynamic Regulation of Airscrew-, Fan- and Wind Turbine Blades with Bores and/or Cutting and/or Notching | |
CA3020210C (fr) | Regulation aerodynamique de pales d'helice, de soufflante et d'eolienne avec des alesages et/ou une coupe et/ou un crantage | |
JP6856930B2 (ja) | ロータ、ドローン及びヘリコプタ | |
WO2017145563A1 (fr) | Pale de rotor, drone et hélicoptère | |
Bocci | A new series of aerofoil sections suitable for aircraft propellers | |
US20050061921A1 (en) | Aerodynamic tip protuberances for tip vortex intensity reduction | |
CN111075760A (zh) | 流体翼 |