CN102562171A - Spherical blade pneumatic motor - Google Patents

Spherical blade pneumatic motor Download PDF

Info

Publication number
CN102562171A
CN102562171A CN201110453992XA CN201110453992A CN102562171A CN 102562171 A CN102562171 A CN 102562171A CN 201110453992X A CN201110453992X A CN 201110453992XA CN 201110453992 A CN201110453992 A CN 201110453992A CN 102562171 A CN102562171 A CN 102562171A
Authority
CN
China
Prior art keywords
rotor
cylinder
sphere
radius
housing
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.)
Granted
Application number
CN201110453992XA
Other languages
Chinese (zh)
Other versions
CN102562171B (en
Inventor
陈行
金波
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.)
Zhejiang University ZJU
Original Assignee
Zhejiang University ZJU
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 Zhejiang University ZJU filed Critical Zhejiang University ZJU
Priority to CN201110453992.XA priority Critical patent/CN102562171B/en
Publication of CN102562171A publication Critical patent/CN102562171A/en
Application granted granted Critical
Publication of CN102562171B publication Critical patent/CN102562171B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Hydraulic Motors (AREA)
  • Rotary Pumps (AREA)

Abstract

The invention discloses a spherical blade pneumatic motor. The motor comprises a shell, a rotor, two blades, two sealing strips, two air distribution cones and two cushion blocks; the rotor is positioned in the center, the shell is positioned on the outer part, the two air distribution cones are respectively positioned in hollow conical surfaces of two ends of the rotor, the two blades are respectively positioned on two sides of the rotor and arranged in a diagonal hollow ring of the shell and form an angle with the rotor, and the tangent of the angle is the ratio of the height of the shell to the diameter of the bottom circle of the shell; and one plane of the blade is attached to the circular lateral surface of each air distribution cone, the sealing strips are positioned between the rotor and the blades, the plane side of the sealing strips is attached to one plane of the rotor, the cylindrical surface side of the sealing strips is attached to the cylindrical surface E1 of the blades, and the cushion blocks are positioned in the diagonal hollow ring of the shell and just fill the vacancy formed by the blades, the rotor and the sealing strips. All sealed positions of the motor are in face seal; and the motor has the advantages of large output torque, high pressure, high efficiency, high specific power, compact structure, low cost and long service life, and is relatively easy to machine.

Description

A kind of spherical blade pneumatic motor
Technical field
The present invention relates to a kind of pneumatic motor, relate in particular to a kind of spherical blade pneumatic motor.
Background technique
Existing pneumatic vane motor structure is a rotor eccentricity and places in the cylinder block, blade radial or place in the rotor with rotor radius is angled, and blade throws away under the effect of spring or air pressure during work, forms Seal cage with cylinder block.This form-blade formula pneumatic motor is owing to be to lean on a Line of contact sealing between blade and the cylinder block, so sealability is relatively poor, and output torque is lower; Produce very big friction when adding rotation between blade and rotor and cylinder block; Cause the pneumatic vane motor overall wear fast, the life-span is short, and efficient is low.In addition, in order to guarantee that blade can safety pass in and out in rotor, rotor must have suitable diameter during rotation, and the volume that is bound to like this is big, and specific power is low.
Summary of the invention
The objective of the invention is deficiency, a kind of spherical blade pneumatic motor is provided to existing technology.Specific power of the present invention is big, all sealing part is face seal, and not easy to wear.
In order to achieve the above object, the technological scheme of the present invention's employing is following: a kind of spherical pneumatic vane motor comprises: housing, rotor, two blades, two Stamping Steel Ribbons, two distributions awls and two cushion blocks; Rotor is positioned at the center; Housing is positioned at the outside; Two distributions awl lays respectively in the two ends of rotor conical hollow face, and two blades lay respectively at the both sides of rotor, and be placed in the housing diagonal angle hollow ring in; With rotor at an angle, the ratio that just is cut to housing height and circular diameter at the bottom of the housing of this angle; The frustum cone side of plane of blade and distribution awl fits; Stamping Steel Ribbon is between rotor and blade; Fit in a plane of its plane one side and rotor; Cylinder one side is then fitted with the cylinder E1 of blade, cushion block be positioned at the housing diagonal angle hollow ring, just in time fill up the vacancy that forms by blade, rotor and Stamping Steel Ribbon.
Said blade is surrounded by two plane A1, B1 and two cylinder C1, E1 and forms; Wherein, cylinder C1 is that the center is centre of sphere O1, radius and the identical cylinder of radius of the cylinder E4 of the hollow ring of housing, and cylinder E1 is that the center is that centre of sphere O1, radius are the cylinder of O1K1, and some K1 was the vertical axis of symmetry of centre of sphere O1 and the intersection point of cylinder E1; Two plane A1 are parallel with B1, connect cylinder C1 and E1; The distance of two parallel plane A1 and B1 is the thickness of blade, and the thickness of blade equates with the hollow ring width of housing; The length of O1K1 is the height sum of the half the and Stamping Steel Ribbon of rotor thickness;
Said Stamping Steel Ribbon upside is that a center is the cylinder that centre of sphere O1, radius equate with the cylinder E1 radius of blade; Downside is a plane; The perpendicular distance of centre of sphere O1 and this time side plane is the half the of rotor thickness, and cylinder G1 is that the center is the cylinder that O1, radius equate with the cylinder P2 radius of rotor, and sphere F1 is that the centre of sphere is the sphere that O1, radius equate with the sphere F4 radius of housing; Plane H1 is parallel with I1, and the width of Stamping Steel Ribbon (being the distance of plane H1 and I1) equates with vane thickness; Blade and Stamping Steel Ribbon are axisymmetric;
Be one flat plate in the middle of the said rotor, dull and stereotyped middle two waist places are two identical director circle platforms, and one of them director circle platform bottom surface is face B2; Upper bottom surface is that the center is the identical cloudy cylndrical surface P2 of radius of O2 radius and the middle cylinder G1 of Stamping Steel Ribbon with dull and stereotyped connecting part, and director circle platform cone angle is identical with the cone angle of cloudy round platform H2, and the bottom surface A2 of two director circle platforms is parallel disk with B2; Two dull and stereotyped planar I 2 are parallel with J2; The sphere E2 and the F2 centre of sphere are the big sphere in the outside about O2, and G2 and H2 are two identical cloudy round platform part sides, and two ends were respectively disk B2 and were the disc of diameter with K2L2 about one of them cloudy round platform; The distance of two parallel plane I2 and J2 is the thickness of rotor; The length of straigh line of K2M2 is the width of rotor, and whole rotor also is an axisymmetric not only about center O 2 symmetries;
Said distribution awl is a round platform; The radius of end face A3 and bottom surface B3 respectively with the cloudy round platform of rotor up and down the radius of two bottom surfaces equate; Highly also the height with the cloudy round platform of rotor equates, the spatial position that two distributions are bored is to decide as follows: after guaranteeing to assemble, the corresponding parallel plane C4 of hollow ring or the D4's two distributions awl frustum cone side of housing fit respectively with accordingly; The conical surface of point D3 to E3 is a deflation area; Point D3 was the horizontal axis in the center of circle and the intersection point of bottom surface B3, the position of some E3 be when rotor 2 forward to by paper shown in Figure 5 position shown in figure 16 during perpendicular to the paper position, the intersection point that justify at the rotor plane, 2 left side and the end; The conical surface of point D3 to G3 is an air inlet face, and the conical surface of D3 to G3 is less than 90 degree.
Said housing is the dolioform sphere that two spherical crowns are fallen at parallel section of two; Thickness equates with the width K2M2 of rotor; End face A4 and bottom surface B4 are the parallel disks that two radiuses equate, sphere F4 is to be the centre of sphere with O4, the outside sphere that equates of the radius of sphere E2 and F2 greatly about radius and rotor; The diagonal angle of housing sphere is a hollow ring; Two side C4 of hollow ring are parallel planar circulars with D4, and the cylinder E4 of hollow ring is the cylinder of central shaft through O4, is positioned on the diagonal of housing; Whole housing is about billiard table center O 4 symmetries;
Said cushion block is one section annulus; Its outer side surface A5 is the cylinder that radius equates with the cylinder E4 external diameter of housing hollow ring; Inner side surface B5 is the sphere that radius equates with housing sphere F4 radius; Two waist C5 and D5 are the cylinders that radius equates with the radius of blade bottom surface cylinder E1, and the thickness of cushion block is identical with vane thickness; Cushion block is shaped as axisymmetric.
Pressurized gas are from the air inlet face input of the some D3 to G3 of distribution awl (5), and low-pressure gas is from the deflation area output of the some D3 to E3 of distribution awl (5), and the pneumatic motor output torque is to load.
The invention has the beneficial effects as follows:
1) all sealing part are face seal;
2) volume is little, and moment of torsion is big, and efficient is high;
3) specific power is big;
4) compact structure, processing is relatively easy;
5) cost is lower, and the life-span is long.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the present invention is described further.
Fig. 1 is a blade shape schematic representation of the present invention
Fig. 2 is the left view of Fig. 1;
Fig. 3 is a gasket structure schematic representation of the present invention;
Fig. 4 be among Fig. 3 Q1 to schematic representation;
Fig. 5 is a rotor structure schematic representation of the present invention;
Fig. 6 is the W-W sectional view of Fig. 5;
Fig. 7 is the T-T sectional view of Fig. 5;
Fig. 8 is the oily wimble structure schematic representation of joining of the present invention;
Fig. 9 is that the P of Fig. 8 is to schematic representation
Figure 10 is a shell construction schematic representation of the present invention;
Figure 11 is the sectional view of housing;
Figure 12 is the M-M sectional view of Figure 11;
Figure 13 is an overall structure schematic representation of the present invention;
Figure 14 is that the K of Figure 13 is to schematic representation;
Figure 15 is the N-N sectional view of Figure 13;
Figure 16 is a running principle schematic representation of the present invention;
Figure 17 is the U-U sectional view of Figure 13;
Figure 18 is a working procedure principle schematic of the present invention;
Figure 19 is the V-V sectional view of Figure 16;
Figure 20 is a working procedure principle schematic of the present invention;
Among the figure: housing 1, rotor 2, blade 3, Stamping Steel Ribbon 4, distribution awl 5, cushion block 6.
Embodiment
Shown in figure 16, the spherical pneumatic vane motor of the present invention comprises housing 1, rotor 2, two blades 3, two Stamping Steel Ribbons 4, two 5 and two cushion blocks 6 of distribution awl.Rotor 2 is positioned at the center; Housing 1 is positioned at the outside; Two distributions awl 5 lays respectively in the rotor 2 two ends conical hollow faces, and two blades 3 lay respectively at the both sides of rotor 2, and be placed in housing 1 diagonal angle hollow ring (being guiding groove) in; With rotor 2 at an angle, the ratio that just is cut to housing 1 height and 1 end of housing circular diameter of this angle.The frustum cone side of plane of blade 3 and distribution awl 5 fits; Stamping Steel Ribbon 4 is between rotor 2 and blade 3; Fit in a plane of its plane one side and rotor 2; Cylinder one side is then fitted with the cylinder E1 of blade 3, cushion block 6 be positioned at housing 1 diagonal angle hollow ring, just in time fill up the vacancy that forms by blade 3, rotor 2 and Stamping Steel Ribbon 4.
Illustrated in figures 1 and 2 is the shape of blade 3 of the present invention.Blade 3 is surrounded by two plane A1, B1 and two cylinder C1, E1 and forms; Wherein, Cylinder C1 is that the center is centre of sphere O1, radius and the identical cylinder of radius of the cylinder E4 of the hollow ring of housing 1; Cylinder E1 is that the center is that centre of sphere O1, radius are the cylinder of O1K1, and some K1 was the vertical axis of symmetry of centre of sphere O1 and the intersection point of cylinder E1.Two plane A1 are parallel with B1, connect cylinder C1 and E1.The distance of two parallel plane A1 and B1 is blade 3 thickness, and blade 3 thickness equate with the hollow ring width of Figure 11 housing 1.The length of O1K1 is the height sum of a half-sum Stamping Steel Ribbon of Fig. 6 rotor 2 thickness.
Fig. 3 and shown in Figure 4 be the shape of Stamping Steel Ribbon 4 of the present invention.As shown in Figure 4; Stamping Steel Ribbon 4 upsides are that a center is the cylinder that centre of sphere O1, radius equate with blade 3 cylinder E1 radiuses; Downside is a plane; The perpendicular distance of centre of sphere O1 and this time side plane is the half the of Fig. 6 rotor 2 thickness, and cylinder G1 is that the center is the cylinder that O1, radius equate with Fig. 5 rotor 2 cylinder P2 radiuses, and sphere F1 is that the centre of sphere is the sphere that O1, radius equate with Figure 11 housing 1 sphere F4 radius; Plane H1 is parallel with I1, and width (being the distance of plane H1 and I1) equates with the thickness of blade 3.Blade 3 is axisymmetric with Stamping Steel Ribbon 4.
Fig. 5, Fig. 6 and shown in Figure 7 be the shape of rotor 2 of the present invention.Be one flat plate in the middle of the rotor 2, dull and stereotyped middle two waist places are two identical director circle platforms, and one of them director circle platform is gone to the bottom and is B2; Upper base is that the center is O2 radius and the identical cloudy cylndrical surface P2 of Stamping Steel Ribbon 4 middle G1 radiuses with dull and stereotyped connecting part, and director circle platform cone angle is identical with the cone angle of cloudy round platform H2, and A2 is parallel disk with B2; I2 is parallel plate level with J2; The E2 and the F2 centre of sphere are the big sphere in the outside about O2, and G2 and H2 are two identical cloudy round platform part sides, and two ends were respectively disk B2 and were the disc of diameter with K2L2 about one of them cloudy round platform; The distance of two parallel plane I2 and J2 is rotor 2 thickness; The length of straigh line of K2M2 is the width of rotor 2, and whole rotor 2 also is an axisymmetric not only about center O 2 symmetries.
Fig. 8 and shown in Figure 9 be the shape of distribution of the present invention awl 5.Distribution awl 5 is round platforms; The radius of end face A3 and bottom surface B3 equates with the radius of two bottom surfaces up and down of rotor 2 cloudy round platforms respectively; Highly also the height with rotor 2 cloudy round platforms equates; The spatial position of two distributions awl 5 is with following and decide: guarantee to assemble back two distributions and bore 5 frustum cone sides and fit with the corresponding parallel plane C4 of hollow ring or the D4 of corresponding housing 1 respectively, the conical surface of some D3 to E3 is a deflation area, and putting D3 was the horizontal axis in the center of circle and the intersection point of bottom surface B3; The position of point E3 is to be forwarded to shown in figure 16 during perpendicular to the paper position by paper shown in Figure 5 position when rotor 2; The intersection point of rotor plane, 2 left side and end circle, the conical surface of some D3 to G3 is an air inlet face, the conical surface of D3 to G3 is less than 90 degree.
Figure 10, Figure 11 and shown in Figure 12 be the shape of housing 1 of the present invention.Housing 1 is the dolioform sphere that two spherical crowns are fallen at parallel section of two; Thickness equates that with the width K2M2 of rotor 2 end face A4 is the parallel disk that radius equates with bottom surface B4, and sphere F4 is to be the centre of sphere with O4; The sphere that radius equates with the radius of big sphere E2 in rotor about 2 outsides and F2; The diagonal angle of housing 1 sphere is a hollow ring, and two side C4 of hollow ring are parallel planar circulars with D4, and E4 is the cylinder of central shaft through O4; Be positioned on the diagonal of housing, two plane C4 that hollow ring is parallel and the spatial position of D4 are with following and decide: guarantee to assemble afterwards C4 and D4 two planes and two distributions and bore 5 frustum cone sides and fit respectively.Whole housing 1 is about billiard table center O 4 symmetries.
The shape of cushion block 6 has been shown among Figure 15.Cushion block 6 is one section annulus; Its outer side surface A5 is the cylinder that radius equates with housing 1 hollow ring E4 external diameter; Inner side surface B5 is the sphere that radius equates with housing 1 sphere F4 radius; Two waist C5 and D5 are the cylinders that radius equates with the radius of blade 3 bottom surface cylinder E1, and the thickness of cushion block 6 is identical with blade 3 thickness.Cushion block 6 is shaped as axisymmetric.
Shown in figure 16, after ball-type pneumatic vane motor of the present invention assembled, the center O 1 of each parts, O2, O4 overlapped.
Operation working principle of the present invention is following:
Like Figure 18, at an end of pneumatic motor, rotor 2, blade 3, Stamping Steel Ribbon 4, distribution awl 5 and housing 1 are divided into three independently Seal cage Q1, Q2 and Q3 separately with air cavity.At an end of rotor 2, when rotor 2 was in air inlet initial position (like Figure 13 or 7a), high pressure air got into air cavity Q1 from the air inlet face of distribution awl; Like Figure 18, at this moment air cavity Q3 has been full of high pressure air, and air cavity Q2 then is a low pressure gas; Three pressure reduction that air cavity forms; On rotor, produce moment of torsion, rotor is rotated counterclockwise, promote blade then and be rotated counterclockwise.When rotor was rotated counterclockwise, the low pressure gas in the air cavity Q2 was discharged through the deflation area of distribution awl.When high pressure air continues when the air inlet face of distribution awl gets into air cavity Q1, rotor continues to be rotated counterclockwise.When rotor forwards Figure 19 position to, and when continuing to be rotated counterclockwise, air cavity Q3 becomes the low pressure exhaust chamber then from the high pressure admission chamber, and high pressure air then continues to get into air cavity Q1, and air cavity Q2 still is the low pressure exhaust chamber.The moment of torsion that draught head produces continues to promote rotor and is rotated counterclockwise, like Figure 20.At this moment Q1 is the high pressure admission chamber, and Q2 and Q3 are the low pressure exhaust chamber.When rotor rotated counterclockwise Figure 17 position, the low pressure gas in the exhaust cavity Q2 drained, and Q1 still is the high pressure admission chamber, and Q3 still is the low pressure exhaust chamber, and at this moment high pressure air gets into new high pressure admission chamber from the air inlet face of distribution awl again, promoted rotor and continued to be rotated counterclockwise.When rotor rotated to Figure 19 position, oil pocket Q1 became the low pressure exhaust chamber then from the high pressure admission chamber, and at this moment Q3 still is the low pressure exhaust chamber, and high pressure air continues to get into new high pressure admission chamber, promoted rotor and continued to be rotated counterclockwise.So go round and begin again, promote rotor and constantly be rotated counterclockwise.At the other end of pneumatic motor, situation is also identical with this end.
The foregoing description is used for the present invention that explains, rather than this aspect is limited, and in the protection domain of spirit of the present invention and claim, any modification and change to make this aspect all fall into protection scope of the present invention.

Claims (2)

1. a spherical pneumatic vane motor is characterized in that, it comprises housing (1), rotor (2), two blades (3), two Stamping Steel Ribbons (4), two distribution awls (5) and two cushion blocks (6) etc.; Rotor (2) is positioned at the center; Housing (1) is positioned at the outside; Two distributions awls (5) lay respectively in the conical hollow face of rotor (2) two ends, and two blades (3) lay respectively at the both sides of rotor (2), and be placed in housing (1) diagonal angle hollow ring (being guiding groove) in; With rotor (2) at an angle, the ratio that just is cut to housing (1) height and housing (1) end circular diameter of this angle; The frustum cone side of plane of blade (3) and distribution awl (5) fits; Stamping Steel Ribbon (4) is positioned between rotor (2) and the blade (3); Fit in a plane of its plane one side and rotor (2); Cylinder one side is then fitted with the cylinder E1 of blade (3), cushion block (6) be positioned at housing (1) diagonal angle hollow ring, just in time fill up the vacancy that forms by blade (3), rotor (2) and Stamping Steel Ribbon (4).
2. according to the said spherical pneumatic vane motor of claim 1, it is characterized in that said blade (3) is surrounded by two plane A1, B1 and two cylinder C1, E1 and forms; Wherein, cylinder C1 is that the center is centre of sphere O1, radius and the identical cylinder of radius of the cylinder E4 of the hollow ring of housing (1), and cylinder E1 is that the center is that centre of sphere O1, radius are the cylinder of O1K1, and some K1 was the vertical axis of symmetry of centre of sphere O1 and the intersection point of cylinder E1; Two plane A1 are parallel with B1, connect cylinder C1 and E1; The distance of two parallel plane A1 and B1 is the thickness of blade (3), and the thickness of blade (3) equates with the hollow ring width of housing (1); The length of O1K1 is the height sum of the half the and Stamping Steel Ribbon of rotor (2) thickness;
Said Stamping Steel Ribbon (4) upside is that a center is the cylinder that centre of sphere O1, radius equate with the cylinder E1 radius of blade (3); Downside is a plane; The perpendicular distance of centre of sphere O1 and this time side plane is the half the of rotor (2) thickness; Cylinder G1 is that the center is the cylinder that O1, radius equate with the cylinder P2 radius of rotor (2); Sphere F1 is that the centre of sphere is the sphere that O1, radius equate with the sphere F4 radius of housing (1), and plane H1 is parallel with I1, and the width of Stamping Steel Ribbon (4) (being the distance of plane H1 and I1) equates with blade (3) thickness; Blade (3) and Stamping Steel Ribbon (4) are axisymmetric;
Said rotor is an one flat plate in the middle of (2); Two waist places are two identical director circle platforms in the middle of dull and stereotyped, and one of them director circle platform bottom surface is face B2, and upper bottom surface is that the center is the identical cloudy cylndrical surface P2 of radius of O2 radius and the middle cylinder G1 of Stamping Steel Ribbon (4) with dull and stereotyped connecting part; Director circle platform cone angle is identical with the cone angle of cloudy round platform H2; The bottom surface A2 and the B2 of two director circle platforms is parallel disks, and two dull and stereotyped planar I 2 are parallel with J2, and the sphere E2 and the F2 centre of sphere are the big sphere in the outside about O2; G2 and H2 are two identical cloudy round platform part sides; One of them cloudy round platform up and down was disk B2 and was the disc of diameter with K2L2 that the distance of two parallel plane I2 and J2 was the thickness of rotor (2) respectively in two ends, and the length of straigh line of K2M2 is the width of rotor (2); Whole rotor (2) also is an axisymmetric not only about center O 2 symmetries;
Said distribution awl (5) is a round platform; The radius of end face A3 and bottom surface B3 respectively and the cloudy round platform of rotor (2) up and down the radius of two bottom surfaces equate; Highly also the height with the cloudy round platform of rotor (2) equates, two distributions are bored the spatial position of (5) to decide as follows: after guaranteeing to assemble, the corresponding parallel plane C4 of hollow ring or the D4's two distributions awl (5) frustum cone side of housing (1) fit respectively with accordingly; The conical surface of point D3 to E3 is a deflation area; Point D3 was the horizontal axis in the center of circle and the intersection point of bottom surface B3, and the position of some E3 is when rotor 2 during perpendicular to the paper position, the intersection point that justify at the rotor plane, 2 left side and the end; The conical surface of point D3 to G3 is an air inlet face, and the conical surface of D3 to G3 is less than 90 degree;
Said housing (1) is the dolioform sphere that two spherical crowns are fallen at parallel section of two; Thickness equates with the width K2M2 of rotor (2); End face A4 and bottom surface B4 are the parallel disks that two radiuses equate, sphere F4 is to be the centre of sphere with O4, the outside sphere that equates of the radius of sphere E2 and F2 greatly about radius and rotor (2); The diagonal angle of housing (1) sphere is a hollow ring; Two side C4 of hollow ring are parallel planar circulars with D4, and the cylinder E4 of hollow ring is the cylinder of central shaft through O4, is positioned on the diagonal of housing; Whole housing (1) is about billiard table center O 4 symmetries;
Said cushion block (6) is one section annulus; Its outer side surface A5 is the cylinder that radius equates with the cylinder E4 external diameter of housing (1) hollow ring; Inner side surface B5 is the sphere that radius equates with housing (1) sphere F4 radius; Two waist C5 and D5 are the cylinders that radius equates with the radius of blade (3) bottom surface cylinder E1, and the thickness of cushion block (6) is identical with blade (3) thickness; Cushion block (6) is shaped as axisymmetric;
Pressurized gas are from the air inlet face input of the some D3 to G3 of distribution awl (5), and low-pressure gas is from the deflation area output of the some D3 to E3 of distribution awl (5), and the pneumatic motor output torque is to load.
CN201110453992.XA 2011-12-30 2011-12-30 Spherical blade pneumatic motor Expired - Fee Related CN102562171B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110453992.XA CN102562171B (en) 2011-12-30 2011-12-30 Spherical blade pneumatic motor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110453992.XA CN102562171B (en) 2011-12-30 2011-12-30 Spherical blade pneumatic motor

Publications (2)

Publication Number Publication Date
CN102562171A true CN102562171A (en) 2012-07-11
CN102562171B CN102562171B (en) 2015-04-29

Family

ID=46408603

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110453992.XA Expired - Fee Related CN102562171B (en) 2011-12-30 2011-12-30 Spherical blade pneumatic motor

Country Status (1)

Country Link
CN (1) CN102562171B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103883356A (en) * 2013-12-16 2014-06-25 浙江大学 Blade pneumatic motor

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0124325A1 (en) * 1983-04-21 1984-11-07 The Garrett Corporation Composite compressor wheel for radial compressors
CN101344085A (en) * 2008-07-30 2009-01-14 郑良才 Vane compressor or vacuum pump
CN101418770A (en) * 2008-12-11 2009-04-29 宁波华液机器制造有限公司 High performance hydraulic motor
CN101418772A (en) * 2008-12-11 2009-04-29 宁波华液机器制造有限公司 Spherical hydraulic motor
CN101418773B (en) * 2008-12-11 2010-12-08 宁波华液机器制造有限公司 High performance spherical hydraulic motor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0124325A1 (en) * 1983-04-21 1984-11-07 The Garrett Corporation Composite compressor wheel for radial compressors
CN101344085A (en) * 2008-07-30 2009-01-14 郑良才 Vane compressor or vacuum pump
CN101418770A (en) * 2008-12-11 2009-04-29 宁波华液机器制造有限公司 High performance hydraulic motor
CN101418772A (en) * 2008-12-11 2009-04-29 宁波华液机器制造有限公司 Spherical hydraulic motor
CN101418773B (en) * 2008-12-11 2010-12-08 宁波华液机器制造有限公司 High performance spherical hydraulic motor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103883356A (en) * 2013-12-16 2014-06-25 浙江大学 Blade pneumatic motor

Also Published As

Publication number Publication date
CN102562171B (en) 2015-04-29

Similar Documents

Publication Publication Date Title
CN101418772A (en) Spherical hydraulic motor
CN101344085A (en) Vane compressor or vacuum pump
CN101338752A (en) Compressor or vacuum pump
CN103670902A (en) Vane type hydraulic motor
CN101418773B (en) High performance spherical hydraulic motor
CN101368565A (en) Cylindrical vane compressor or vacuum pump
CN101418770A (en) High performance hydraulic motor
CN102562581B (en) Spherical vane type hydraulic pump
CN101418771A (en) High performance hydraulic motor
CN101418792A (en) High performance spherical hydraulic pump
CN103671098A (en) Multiple-blade compressor
CN102562167A (en) Shell air distribution type columnar blade pneumatic motor
CN102562171A (en) Spherical blade pneumatic motor
CN102536803B (en) Shell oil distribution type cylindrical blade hydraulic pump
CN102606217B (en) Pneumatic motor with cylindrical blades
CN102536804A (en) Cylindrical vane hydraulic pump
CN102852791B (en) Housing gas distribution-type cylindrical vane compressor
CN102536816A (en) Spherical blade compressor
CN103670901A (en) Multiple-blade hydraulic motor
CN102562580A (en) Spherical vane hydraulic pump with oil discharging on shell
CN103883356A (en) Blade pneumatic motor
CN102536625A (en) Cylindrical vane hydraulic motor
CN102536624A (en) Spherical-vane hydraulic motor
CN102619568A (en) Shell distribution type pneumatic motor with spherical blades
CN103671095A (en) Multiple-blade hydraulic pump

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150429

Termination date: 20181230

CF01 Termination of patent right due to non-payment of annual fee