CN104443359A - Translation propeller - Google Patents
Translation propeller Download PDFInfo
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- CN104443359A CN104443359A CN201410769585.3A CN201410769585A CN104443359A CN 104443359 A CN104443359 A CN 104443359A CN 201410769585 A CN201410769585 A CN 201410769585A CN 104443359 A CN104443359 A CN 104443359A
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- blade
- main shaft
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- leaf
- arm axle
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Abstract
The invention discloses a translation propeller, and belongs to the technical field of aviation. The translation propeller comprises a main shaft, a center gear, two or three or four rotating vanes, wherein the rotating vanes are evenly distributed on the periphery of the center gear; the main shaft is horizontally arranged in a longitudinal manner, and is connected with the center gear fixed on a bracket through a bearing; each rotating vane comprises an arm shaft, a vane shaft, a blade, an entocentric gear, an arm shaft sleeve, a telecentric gear and a vane gear; each blade has elasticity; the vane shafts are fixedly connected with the arm shafts vertically; the rear ends of the vane shafts are connected with the vane gears through the bearings; the vane gears and the blades are fixedly connected at the centers of the front edges of the blades; the arm shaft sleeves are arranged on the peripheries of the arm shafts through the bearings in a sleeving manner; the telecentric gears are meshed with the vane gears; the transmission ratio is 1 to 1; the rear end of the main shaft is fixedly connected with the arm shafts of all rotating vanes vertically; the transmission ratios of the center gear to all the entocentric gears are all 1 to 1; the blades are horizontally arranged; the main shaft continuously rotates under the drive of power; the vanes alternately beat downwards and upwards; and the efficiency for generating lift and the thrust is relatively high.
Description
Technical field
A kind of translation class screw propeller, belongs to technical field of aerospace, particularly relates to a kind of translation class screw propeller.
Background technology
Traditional aircraft screw propeller plane of rotation can only produce pulling force or thrust when laterally vertically arranging, can not produce lift; Blade is curved surface, and the curvature at different radii place and section are not identical, and processing and manufacturing difficulty is large.
Summary of the invention
The object of the invention is the above-mentioned deficiency overcoming existing aircraft screw propeller, invent the translation class screw propeller that a kind of blade construction simply can produce lift and thrust or pulling force simultaneously.
A kind of translation class screw propeller, the rotating vane that the structure that to comprise main shaft, sun gear different with the setting angle of two, three of being evenly distributed on around sun gear or four only blade is identical.Main shaft vertical equity is arranged, the stage casing of main shaft is connected in the centre hole of sun gear by bearing and sun gear, and main shaft can flexible rotating in the centre hole of sun gear.Sun gear is fixedly mounted on support.The front end of main shaft is connected with power.Each rotating vane comprises arm axle, rachis, blade, nearly heart gear, arm axle sleeve pipe, heart gear far away and leaf-teeth wheel.The plane configuration of blade is rectangular, and blade inlet edge is more abundant, and trailing edge is thinner, and blade is nonrigid, has elasticity.The aerofoil profile of blade is flat pattern under the recessed or epirelief of epirelief, and different length positions aerofoil profile is identical.
The interrelation of the component in same rotating vane is: the rachis front end that be fixed on rachis vertical with arm axle, and rachis vertical equity is arranged, rachis and arm axle and main shaft are in same plane.The rear end of rachis is taken turns by bearing and leaf-teeth and is connected in centre hole that leaf-teeth take turns, and leaf-teeth wheel can around rachis flexible rotating.Leaf-teeth wheel and blade are fixed on the center place of the leading edge of blade.During quiescence, rachis and blade are in same level.Arm axle sleeve pipe is contained in around arm axle stage casing by bearing carrier ring, arm axle can in arm axle sleeve pipe flexible rotating.Nearly heart gear and heart gear far away are fixed on the two ends of arm axle sleeve pipe respectively.Heart gear far away and leaf gears meshing, its transmitting ratio is 1: 1.
The rear end of main shaft is vertical with the arm axle of all rotating vanes to be connected.The nearly heart gear of all rotating vanes all engages with sun gear, and the transmitting ratio of sun gear and all nearly heart gears is all 1: 1.Sun gear and all nearly heart gears, heart gear far away and leaf-teeth wheel all adopt finishing bevel gear cuter.When assembling this translation class screw propeller, guarantee that vaned reference position is level attitude, and the convex surface of blade upward, like this, because sun gear maintains static, and the transmitting ratio that sun gear and all leaf-teeth are taken turns is 1: 1, the blade that arbitrary leaf is walked around to this rotating vane during any position all can be in horizontality.
The principle of work of this translation class screw propeller is: arranged by the main shaft vertical equity of this translation class screw propeller, upward, forward, the front end of main shaft, is connected power backwards to the leading edge of blade to the convex surface of blade by trailing edge, and the frame of support and propulsion source is connected.See from back to front, power driven main shaft clickwise, because sun gear is fixing, and the transmitting ratio that sun gear and leaf-teeth are taken turns is 1: 1, blade can conter clockwise rotation under the drive taken turns at corresponding leaf-teeth while main shaft revolution, on the right side of longitudinal vertical guide crossing main shaft, clap under blade, its leading edge keeps horizontality, and the displacement of clapping under length direction and the identical chord positions of cross blade is identical, realizes flat bat downwards; In the left side of longitudinal vertical guide of mistake main shaft, blade arsis, its leading edge also keeps horizontality, and the displacement along length direction and cross blade identical chord positions arsis is also identical, realizes upwards flat bat.Main shaft rotates continuously under the driving of power, each blade alternate carries out lower bat and arsis, because blade is nonrigid, there is certain elasticity, in the midway of lower bat, the trailing edge of blade want delayed leading edge some, arsis midway trailing edge also can delayed leading edge some, because the aerofoil profile of blade is flat pattern under epirelief concave shape or epirelief, their lower bats can produce larger lift upwards and less thrust forward; Compared with lower bat, during arsis, the degree of their the delayed leading edge of trailing edge is larger, larger thrust forward and less lift upwards can be produced during arsis or do not produce lift, the size producing lift is relevant with the speed that such screw propeller moves ahead, and front line speed is faster, and the lift of generation is larger.Blade substantially laterally can not produce horizontal component of force in the process of flapping motion, and the efficiency producing lift and thrust is higher.
The blade of equal section easily makes.This invention class screw propeller is used on aircraft in pairs, can be aircraft and provide lift and thrust in the middle part of the trailing edge that symmetry is arranged on the left and right wing of aircraft.Power inputs from the front end of their main shaft, and their support should be fixedly mounted on wing.Two class propeller turning directions are contrary, can offset rotating torque.
Accompanying drawing explanation
Schematic rear view when Fig. 1 is the rotation of a kind of translation class of the present invention screw propeller, dotted line represents that rotating vane is in different positions; Fig. 2 is the schematic top plan view of a kind of translation class of the present invention screw propeller two blade when being in same level position.
In figure, 1-main shaft; 2-sun gear; 3-left-hand rotation leaf; 4-right-hand rotation leaf; 5-support; 6-rotating vane hand of rotation indicates.
Belong to the component of left-hand rotation leaf 3: 31-arm axle, 32-rachis, 33-blade, the leading edge of 331-blade, the trailing edge of 332-blade, the nearly heart gear of 34-, 35-arm axle sleeve pipe, 36-heart gear far away, 37-leaf-teeth are taken turns.
Belong to the component of right-hand rotation leaf 4: 41-arm axle, 42-rachis, 43-blade, the leading edge of 431-blade, the trailing edge of 432-blade, the nearly heart gear of 44-, 45-arm axle sleeve pipe, 46-heart gear far away, 47-leaf-teeth are taken turns.
Detailed description of the invention
Below in conjunction with accompanying drawing 1 ~ 2 couple of the present invention casehistory in addition.
A kind of translation class screw propeller, the rotating vane that the structure that to comprise main shaft 1, sun gear 2 different with the setting angle of two, three of being evenly distributed on around sun gear 2 or four only blade is identical.The rotating vane of the present embodiment is two, i.e. left-hand rotation leaf 3 and right-hand rotation leaf 4, and left-hand rotation leaf 3 and right-hand rotation leaf 4 are mutually 180 ° of symmetric offset spread in the both sides of main shaft 1.Main shaft 1 vertical equity is arranged, the stage casing of main shaft 1 is connected in the centre hole of sun gear 2 by bearing and sun gear 2, and main shaft 1 can flexible rotating in the centre hole of sun gear 2.Sun gear 2 is fixedly mounted on support 5.The front end of main shaft 1 is connected with power.
The concrete structure of right-hand rotation leaf 4 is: it comprises arm axle 41, rachis 42, blade 43, nearly heart gear 44, arm axle sleeve pipe 45, heart gear 46 far away and leaf-teeth wheel 47.The plane configuration of blade 43 is rectangular, and blade inlet edge 431 is more abundant, and trailing edge 432 is thinner, and blade 43 is nonrigid, has elasticity.The aerofoil profile of blade 43 is flat pattern under the recessed or epirelief of epirelief, and different length positions aerofoil profile is identical.Rachis 42 front end that be fixed on rachis 42 vertical with arm axle 41, rachis 42 horizontal arrangement.The rear end of rachis 42 is taken turns 47 by bearing and leaf-teeth and is connected in leaf-teeth and takes turns in the centre hole of 47, and leaf-teeth wheel 47 can around rachis 42 flexible rotating.Leaf-teeth wheel 47 and blade 43 are fixed on the center place of the leading edge 431 of blade 43.During quiescence, rachis 42 and blade 43 are in same level.Arm axle sleeve pipe 45 is contained in around arm axle 41 stage casing by bearing carrier ring, arm axle 41 can in arm axle sleeve pipe 45 flexible rotating.Nearly heart gear 44 and heart gear 46 far away are fixed on the two ends of arm axle sleeve pipe 45 respectively.Heart gear 46 far away and leaf-teeth are taken turns 47 and are engaged, and its transmitting ratio is 1: 1.
The rear end of main shaft 1 is connected with the arm axle 41 of right-hand rotation leaf 4 is all vertical with the arm axle 31 of left-hand rotation leaf 3.The arm axle 31 of main shaft 1, left-hand rotation leaf 3, the arm axle 41 of right-hand rotation leaf 4, the rachis 32 of left-hand rotation leaf 3 and the rachis 42 5 of right-hand rotation leaf 4 are in same plane.The nearly heart gear 34 of left-hand rotation leaf 3 and the nearly heart gear 44 of right-hand rotation leaf 4 all engage with sun gear 2, and the transmitting ratio of sun gear 2 and two nearly heart gears is all 1: 1.Sun gear 2, two nearly heart gears, two heart gears far away and two leaf-teeth wheels all adopt finishing bevel gear cuter.When assembling this translation class screw propeller, guarantee that vaned reference position is level attitude, and the convex surface of blade upward, like this, because sun gear 2 maintains static, and the transmitting ratio that sun gear 2 and two leaf-teeth are taken turns is all 1: 1, the blade that arbitrary leaf is walked around to this rotating vane during any position all can be in horizontality.
The principle of work of this translation class screw propeller is: arranged by main shaft 1 vertical equity of this translation class screw propeller, and upward, forward, the front end of main shaft 1, is connected power backwards to the leading edge of two blades to the convex surface of two blades by trailing edge, and support 5 is connected with the frame of propulsion source.See from back to front, power driven main shaft 1 clickwise, because sun gear 2 is fixing, and can conter clockwise rotation under the drive that the transmitting ratio that sun gear 2 and two leaf-teeth are taken turns is all 1: 1, two blades takes turns at corresponding leaf-teeth while revolving round the sun around main shaft 1, on the right side of longitudinal vertical guide crossing main shaft 1, clap under blade, its leading edge keeps horizontality, and the displacement of clapping under length direction and the identical chord positions of cross blade is identical, realizes flat bat downwards; In the left side of longitudinal vertical guide of mistake main shaft 1, blade arsis, its leading edge also keeps horizontality, and the displacement along length direction and cross blade identical chord positions arsis is also identical, realizes upwards flat bat.Main shaft 1 rotates continuously under the driving of power, each blade alternate carries out lower bat and arsis, because blade is nonrigid, there is certain elasticity, in the midway of lower bat, the trailing edge of blade want delayed leading edge some, arsis midway trailing edge also can delayed leading edge some, because the aerofoil profile of blade is flat pattern under epirelief concave shape or epirelief, their lower bats can produce larger lift upwards and less thrust forward; Compared with lower bat, during arsis, the degree of their the delayed leading edge of trailing edge is larger, larger thrust forward and less lift upwards can be produced during arsis or do not produce lift, the size producing lift is relevant with the speed that such screw propeller moves ahead, and front line speed is faster, and the lift of generation is larger.Two blades substantially laterally can not produce horizontal component of force in the process of flapping motion, and the efficiency producing lift and thrust is higher.
This invention class screw propeller is used on aircraft in pairs, can be aircraft and provide lift and thrust in the middle part of the trailing edge that symmetry is arranged on the left and right wing of aircraft.Power inputs from the front end of their main shaft, and their support is fixedly mounted on wing.Two class propeller turning directions are contrary, can offset rotating torque.
Claims (3)
1. a translation class screw propeller, is characterized in that: comprise main shaft (1), sun gear (2) and be evenly distributed on the identical rotating vane of the different structure of the setting angle of sun gear (2) around two, three or four only blade; Main shaft (1) vertical equity is arranged, the stage casing of main shaft (1) is connected in the centre hole of sun gear (2) by bearing and sun gear (2), and main shaft (1) is energy flexible rotating in the centre hole of sun gear (2); Sun gear (2) is fixedly mounted on support (5); The front end of main shaft (1) is connected with power;
Each rotating vane comprises arm axle, rachis, blade, nearly heart gear, arm axle sleeve pipe, heart gear far away and leaf-teeth wheel; The plane configuration of blade is rectangular, and blade inlet edge is more abundant, and trailing edge is thinner, and blade is nonrigid, has elasticity; The aerofoil profile of blade is flat pattern under the recessed or epirelief of epirelief;
The interrelation of the component in same rotating vane is: the rachis front end that be fixed on rachis vertical with arm axle, and rachis vertical equity is arranged, rachis and arm axle and main shaft (1) are in same plane; The rear end of rachis is taken turns by bearing and leaf-teeth and is connected in centre hole that leaf-teeth take turns, and leaf-teeth wheel can around rachis flexible rotating; Leaf-teeth wheel and blade are fixed on the center place of the leading edge of blade; During quiescence, rachis and blade are in same level; Arm axle sleeve pipe is contained in around arm axle stage casing by bearing carrier ring, arm axle can in arm axle sleeve pipe flexible rotating; Nearly heart gear and heart gear far away are fixed on the two ends of arm axle sleeve pipe respectively; Heart gear far away and leaf gears meshing, its transmitting ratio is 1: 1;
The rear end of main shaft (1) is vertical with the arm axle of all rotating vanes to be connected; The nearly heart gear of all rotating vanes all engages with sun gear (2), and sun gear (2) is all 1: 1 with the transmitting ratio of all nearly heart gears; Vaned reference position is level attitude, and their convex surface upward; During use, support (5) is connected with the frame of propulsion source.
2. a kind of translation class screw propeller according to claim 1, is characterized in that: institute's vaned different length positions aerofoil profile is identical.
3. a kind of translation class screw propeller according to claim 1, is characterized in that: sun gear (2) and all nearly heart gears, heart gear far away and leaf-teeth wheel all adopt finishing bevel gear cuter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410769585.3A CN104443359B (en) | 2014-12-15 | 2014-12-15 | A kind of translation class screw propeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410769585.3A CN104443359B (en) | 2014-12-15 | 2014-12-15 | A kind of translation class screw propeller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104443359A true CN104443359A (en) | 2015-03-25 |
| CN104443359B CN104443359B (en) | 2016-04-06 |
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ID=52890282
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410769585.3A Expired - Fee Related CN104443359B (en) | 2014-12-15 | 2014-12-15 | A kind of translation class screw propeller |
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| Country | Link |
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| CN (1) | CN104443359B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2095830U (en) * | 1991-04-22 | 1992-02-12 | 林永克 | Air propeller |
| CN101342943A (en) * | 2008-08-15 | 2009-01-14 | 张鞍平 | Method for acquiring fluid differential pressure propelling force and blades thereof |
| US20130181458A1 (en) * | 2010-09-22 | 2013-07-18 | Saphon Energy Ltd | System for converting wind energy |
| CN204310035U (en) * | 2014-12-15 | 2015-05-06 | 佛山市神风航空科技有限公司 | A kind of translation class screw propeller |
-
2014
- 2014-12-15 CN CN201410769585.3A patent/CN104443359B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2095830U (en) * | 1991-04-22 | 1992-02-12 | 林永克 | Air propeller |
| CN101342943A (en) * | 2008-08-15 | 2009-01-14 | 张鞍平 | Method for acquiring fluid differential pressure propelling force and blades thereof |
| US20130181458A1 (en) * | 2010-09-22 | 2013-07-18 | Saphon Energy Ltd | System for converting wind energy |
| CN204310035U (en) * | 2014-12-15 | 2015-05-06 | 佛山市神风航空科技有限公司 | A kind of translation class screw propeller |
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| Publication number | Publication date |
|---|---|
| CN104443359B (en) | 2016-04-06 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information |
Inventor after: Hao Jinian Inventor before: Wang Zhicheng |
|
| CB03 | Change of inventor or designer information | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170901 Address after: 075000 Zhangjiakou City, Hebei Province town of Wanquan County kongjiazhuang Quanxing Road East 11 No. 2 Building 3 unit 301 room Foshan city streets Gaoming District No. 78 Jiangwan Road, room 402 Fu Wan Patentee after: Hao Jinian Address before: Foshan City, Guangdong province 528500 city streets Gaoming District No. 78 Jiangwan Road, room 402 Fu Wan Patentee before: Shenfeng science and technology of aviation Co., Ltd of Foshan City |
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| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160406 Termination date: 20171215 |
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| CF01 | Termination of patent right due to non-payment of annual fee |