CN201729269U - Efficiency increasing propeller - Google Patents

Efficiency increasing propeller Download PDF

Info

Publication number
CN201729269U
CN201729269U CN2010201905361U CN201020190536U CN201729269U CN 201729269 U CN201729269 U CN 201729269U CN 2010201905361 U CN2010201905361 U CN 2010201905361U CN 201020190536 U CN201020190536 U CN 201020190536U CN 201729269 U CN201729269 U CN 201729269U
Authority
CN
China
Prior art keywords
paddle
outer ring
utility
model
outer shroud
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
Application number
CN2010201905361U
Other languages
Chinese (zh)
Inventor
李淑萍
许高珩
李若
周荣堂
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang Aerospace University
Original Assignee
Shenyang Aerospace University
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shenyang Aerospace University filed Critical Shenyang Aerospace University
Priority to CN2010201905361U priority Critical patent/CN201729269U/en
Application granted granted Critical
Publication of CN201729269U publication Critical patent/CN201729269U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The utility model relates to an efficiency increasing propeller, comprising a paddle and an outer ring. The outer ring is fixed at the outer side of the paddle, and integral design and manufacturing are adopted for the outer ring and the paddle. The utility model can provide more lifting force under the same rotate speed. The whole paddle and the outer ring are made of reinforcing carbon fiber material, and the paddle and the outer ring are integrally designed and manufactured, thereby the utility model has light weight and good toughness.

Description

Enhanced propeller
Technical field: the utility model relates to a kind of properller, and especially a kind of enhanced propeller is mainly used on the piston engine of light-small aircraft.
Background technology: present driving engine screw propeller is when rotating speed improves, and the outside of blade at first reaches velocity of sound, produces drag due to shock wave, and the efficient that has influenced screw propeller improves.
The utility model content: at above-mentioned the deficiencies in the prior art, the utility model provides a kind of enhanced propeller.
For achieving the above object, the technical solution adopted in the utility model is: enhanced propeller, comprise blade and outer shroud, and outer shroud is fixed on the outside of blade, and both adopt the integrated design manufacturing.
The utility model provides more lift under identical rotating speed.Entire blade and outer shroud adopt the enhanced carbon fiber material, make blade and outer shroud integrated design manufacturing, and be in light weight, good toughness.
Description of drawings:
Fig. 1 is a structural representation of the present utility model
Fig. 2 is the cross-sectional view of outer shroud.
The specific embodiment:
As depicted in figs. 1 and 2: enhanced propeller, comprise blade 2 and outer shroud 1, outer shroud 1 is fixed on the outside of blade 2, and both adopt the integrated design manufacturing.The cross section of outer shroud 1 is an aerofoil profile, thereby makes the fluid on its upper and lower surface produce the asymmetry that flows, and the upper surface flow velocity increases, and pressure reduces; The lower surface flow velocity reduces, and pressure increases, and obtains lift.The leading edge of aerofoil profile (being a wide side) is connected with blade 2, and trailing edge (being a narrow side) connects very firm in the outside like this.

Claims (2)

1. enhanced propeller comprises blade, it is characterized in that: also comprise the outer shroud that is fixed on the blade outside, the cross section of outer shroud is an aerofoil profile, and the leading edge of aerofoil profile is connected with blade, and trailing edge is in the outside.
2. enhanced propeller as claimed in claim 1 is characterized in that: described paddle and outer shroud adopt the integrated design manufacturing.
CN2010201905361U 2010-05-14 2010-05-14 Efficiency increasing propeller Expired - Fee Related CN201729269U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010201905361U CN201729269U (en) 2010-05-14 2010-05-14 Efficiency increasing propeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010201905361U CN201729269U (en) 2010-05-14 2010-05-14 Efficiency increasing propeller

Publications (1)

Publication Number Publication Date
CN201729269U true CN201729269U (en) 2011-02-02

Family

ID=43520426

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010201905361U Expired - Fee Related CN201729269U (en) 2010-05-14 2010-05-14 Efficiency increasing propeller

Country Status (1)

Country Link
CN (1) CN201729269U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101823557A (en) * 2010-05-14 2010-09-08 沈阳航空航天大学 Enhanced propeller

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101823557A (en) * 2010-05-14 2010-09-08 沈阳航空航天大学 Enhanced propeller

Similar Documents

Publication Publication Date Title
CN202023688U (en) Wind turbine blade with blunt trailing edge
CN102991658B (en) Bionic propeller of ship
CN203666968U (en) Negative dihedral aerofoil winglet structure
CN103629044B (en) A kind of leaf and root structure of Blades For Horizontal Axis Wind
CN203584893U (en) Noise-reduction energy-saving fan
CN205613368U (en) High -efficient axial compressor type variable cross section paddle subassembly for agitator
CN204591795U (en) The bionical sawtooth blade structure of a kind of multilayer
CN201729269U (en) Efficiency increasing propeller
CN201090504Y (en) Single-stage single absorption centrifugal pump impeller with circulation tank
CN201874882U (en) Fan blade
CN103895850B (en) A kind of combined energy-saving bracing strut device
CN210483953U (en) Blade tip fusion winglet of large-scale offshore wind turbine and wind turbine
CN101892945A (en) Wind turbine blade
CN106477025A (en) A kind of small-sized electrically driven (operated) aircraft power propulsion system
CN101823557A (en) Enhanced propeller
CN202065241U (en) First-stage blade of air compressor with hub diameter of phi 762
CN210949262U (en) Novel plate type axial flow fan impeller
CN209581849U (en) A kind of porous media rear propeller blade
CN202520651U (en) Cooling tower draught fan wing-shaped vane
CN202016565U (en) Structure for improving output efficiency and reducing noise of spiral propeller
CN201198842Y (en) High lifting force and low noise airfoil blade
CN205770151U (en) A kind of unmanned plane rotor
CN203627082U (en) Blade root structure of horizontal shaft wind turbine blade
CN209553500U (en) Anti- low induced drag lifting airscrew under a kind of wing tip sweepback
CN104696158A (en) Lift type blade airfoil for vertical-axis wind turbine generator system

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110202

Termination date: 20130514