CN102562171B - Spherical blade pneumatic motor - Google Patents
Spherical blade pneumatic motor Download PDFInfo
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- CN102562171B CN102562171B CN201110453992.XA CN201110453992A CN102562171B CN 102562171 B CN102562171 B CN 102562171B CN 201110453992 A CN201110453992 A CN 201110453992A CN 102562171 B CN102562171 B CN 102562171B
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- 238000009826 distribution Methods 0.000 claims abstract description 33
- 229910000831 Steel Inorganic materials 0.000 claims description 24
- 239000010959 steel Substances 0.000 claims description 24
- 238000007789 sealing Methods 0.000 abstract description 9
- 238000010586 diagram Methods 0.000 description 10
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
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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
Technical field
The present invention relates to a kind of pneumatic motor, particularly relate to a kind of spherical blade pneumatic motor.
Background technique
Existing blade pneumatic motor structure is a rotor eccentricity and is placed in cylinder block, blade radial or be placed in rotor with rotor radius is angled, and during work, blade throws away under the effect of spring or air pressure, forms Seal cage with cylinder block.This form pneumatic vane motor is owing to being seal by a Line of contact between blade and cylinder block, and therefore sealability is poor, and output torque is lower, very large friction is produced between blade and rotor and cylinder block when adding rotation, cause pneumatic vane motor overall wear fast, the life-span is short, and efficiency is low.In addition, in order to ensure that blade safety can pass in and out in rotor during rotation, rotor must have suitable diameter, and the volume that is bound to like this is large, and specific power is low.
Summary of the invention
The object of the invention is for the deficiencies in the prior art, a kind of spherical blade pneumatic motor is provided.Large, whole sealing place of specific power of the present invention is face sealing, and not easy to wear.
In order to achieve the above object, the technical solution used in the present invention is as follows: a kind of spherical blade formula pneumatic motor, comprising: housing, rotor, two blades, two Stamping Steel Ribbons, two distribution cones and two cushion blocks; Rotor is positioned at center, housing is positioned at outside, two distribution cones lay respectively in two ends of rotor conical hollow face, two blades lay respectively at the both sides of rotor, and be placed in housing diagonal angle hollow ring in, with rotor at an angle, the ratio being just cut to body height and circular diameter at the bottom of housing of this angle; The frustum cone side that a plane of blade and distribution are bored fits, Stamping Steel Ribbon is between rotor and blade, a plane of its plane side and rotor is fitted, then fit with the cylinder E1 of blade in cylinder side, cushion block be positioned at housing diagonal angle hollow ring, just in time fill up the vacancy formed by blade, rotor and Stamping Steel Ribbon.
Described blade is enclosed by two plane A1, B1 and two cylinders C1, E1 and forms; Wherein, the cylinder that cylinder C1 is center is centre of sphere O1, radius is identical with the radius of the cylinder E4 of the hollow ring of housing, cylinder E1 is center is centre of sphere O1, radius is 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 is equal with the hollow ring width of housing; The length of O1K1 is the half of rotor thickness and the height sum of Stamping Steel Ribbon;
the cylinder that being a center on the upside of described Stamping Steel Ribbon is centre of sphere O1, radius is equal with the cylinder E1 radius of blade, downside is a plane, the perpendicular distance of centre of sphere O1 and this underside plan is the half of rotor thickness, the cylinder that cylinder G1 is center is O1, radius is equal with the cylinder P2 radius of rotor, the sphere that sphere F1 is the centre of sphere is O1, radius is equal with the sphere F4 radius of housing, plane H1 is parallel with I1, and the width (i.e. the distance of plane H1 and I1) of Stamping Steel Ribbon is equal with vane thickness; Blade and Stamping Steel Ribbon are axisymmetric;
one flat plate in the middle of described rotor, in the middle of dull and stereotyped, two waist places are two identical director circle platforms, one of them director circle platform bottom surface is face B2, the cloudy cylndrical surface P2 that in the middle of to be center be upper bottom surface and dull and stereotyped connecting part O2 radius and Stamping Steel Ribbon, the radius of cylinder G1 is identical, director circle platform cone angle is identical with the cone angle of cloudy round platform H2, bottom surface A2 with B2 of two director circle platforms is parallel disks, two dull and stereotyped planar I 2 are parallel with J2, large sphere outside the left and right of sphere E2 and F2 to be the centre of sphere be O2, G2 with H2 is two identical cloudy round platform surface, one of them cloudy round platform upper and lower two ends, are disk B2 respectively and take K2L2 as the disc of diameter, 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, whole rotor is not only symmetrical about center O2, also be axisymmetric,
Described distribution cone is a round platform, the radius of cloudy upper and lower two bottom surfaces of round platform is equal with rotor respectively for the radius of end face A3 and bottom surface B3, highly also the height of round platform cloudy with rotor is equal, the spatial position of two distribution cones is to determine as follows: after guarantee assembles, corresponding parallel plane C4's two distribution cone frustum cone sides or D4 fits with the hollow ring of corresponding housing respectively, the conical surface of some D3 to E3 is deflation area, point D3 was the horizontal axis in the center of circle and the intersection point of bottom surface B3, point E3 position be when rotor 2 as shown in Figure 5 paper position forward to as shown in figure 16 perpendicular to paper position time, the intersection point of rotor 2 left side plan and end circle, the conical surface of some D3 to G3 is air inlet face, the conical surface of D3 to G3 is less than 90 degree.
Described housing is the parallel dolioform sphere cutting out two spherical crowns in two, thickness is equal with the width K2M2 of rotor, end face A4 and bottom surface B4 are the parallel disks that two radiuses are equal, sphere F4 take O4 as the centre of sphere, the sphere that radius is equal with the radius of large sphere E2 and F2 in outside about rotor, the diagonal angle of housing sphere is a hollow ring, two side C4 with D4 of hollow ring are parallel planar circulars, the cylinder E4 of hollow ring is the cylinder of central shaft by O4, is positioned on the diagonal of housing; Whole housing is symmetrical about billiard table center O4;
Described cushion block is one section of annulus, its outer side surface A5 is the cylinder that radius is equal with the cylinder E4 external diameter of housing hollow ring, inner side surface B5 is the sphere that radius is equal with housing sphere F4 radius, two waist C5 and D5 are the cylinders that radius is equal with the radius of blade bottom surface cylinder E1, and the thickness of cushion block is identical with vane thickness; Cushion block shape is axisymmetric.
Pressurized gas are from the air inlet face input of the some D3 to G3 of distribution cone (5), and low-pressure gas exports from the deflation area of the some D3 to E3 of distribution cone (5), and pneumatic motor output torque is to load.
The invention has the beneficial effects as follows:
1) all sealings place are face sealing;
2) volume is little, and moment of torsion is large, and efficiency is high;
3) specific power is large;
4) compact structure, processing is relatively easy;
5) cost is lower, and the life-span is long.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described.
Fig. 1 is blade shape schematic diagram of the present invention
Fig. 2 is the left view of Fig. 1;
Fig. 3 is gasket structure schematic diagram of the present invention;
Fig. 4 be in Fig. 3 Q1 to schematic diagram;
Fig. 5 is rotor structure schematic diagram 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 of the present inventionly joins oily wimble structure schematic diagram;
Fig. 9 is that the P of Fig. 8 is to schematic diagram
Figure 10 is shell construction schematic diagram 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 overall structure schematic diagram of the present invention;
Figure 14 is that the K of Figure 13 is to schematic diagram;
Figure 15 is the N-N sectional view of Figure 13;
Figure 16 is running principle schematic diagram of the present invention;
Figure 17 is the U-U sectional view of Figure 13;
Figure 18 is working procedure principle schematic of the present invention;
Figure 19 is the V-V sectional view of Figure 16;
Figure 20 is working procedure principle schematic of the present invention;
In figure: housing 1, rotor 2, blade 3, Stamping Steel Ribbon 4, distribution cone 5, cushion block 6.
Embodiment
As shown in figure 16, spherical blade formula pneumatic motor of the present invention comprises housing 1, rotor 2, two blades 3, two Stamping Steel Ribbons 4, two distribution cones 5 and two cushion blocks 6.Rotor 2 is positioned at center, housing 1 is positioned at outside, two distribution cones 5 lay respectively in conical hollow face, rotor 2 two ends, two blades 3 lay respectively at the both sides of rotor 2, and be placed in housing 1 diagonal angle hollow ring (i.e. guiding groove) in, with rotor 2 at an angle, this angle be just cut to housing 1 height and the ratio of housing 1 end circular diameter.The frustum cone side that a plane of blade 3 and distribution bore 5 fits, Stamping Steel Ribbon 4 is between rotor 2 and blade 3, a plane of its plane side and rotor 2 is fitted, then fit with the cylinder E1 of blade 3 in cylinder side, cushion block 6 be positioned at housing 1 diagonal angle hollow ring, just in time fill up the vacancy formed by blade 3, rotor 2 and Stamping Steel Ribbon 4.
Fig. 1 and the shape that Figure 2 shows that blade 3 of the present invention.Blade 3 is enclosed by two plane A1, B1 and two cylinders C1, E1 and forms, wherein, the cylinder that cylinder C1 is center is centre of sphere O1, radius is identical with the radius of the cylinder E4 of the hollow ring of housing 1, cylinder E1 is center is centre of sphere O1, radius is 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 is equal 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 the shape that Figure 4 shows that Stamping Steel Ribbon 4 of the present invention.As shown in Figure 4, the cylinder that being a center on the upside of Stamping Steel Ribbon 4 is centre of sphere O1, radius is equal with blade 3 cylinder E1 radius, downside is a plane, the perpendicular distance of centre of sphere O1 and this underside plan is the half of Fig. 6 rotor 2 thickness, the cylinder that cylinder G1 is center is O1, radius is equal with Fig. 5 rotor 2 cylinder P2 radius, the sphere that sphere F1 is the centre of sphere is O1, radius is equal with Figure 11 housing 1 sphere F4 radius, plane H1 is parallel with I1, and width (i.e. the distance of plane H1 and I1) is equal with the thickness of blade 3.Blade 3 and Stamping Steel Ribbon 4 are axisymmetric.
Fig. 5, Fig. 6 and Figure 7 shows that the shape of rotor 2 of the present invention.One flat plate in the middle of rotor 2, in the middle of dull and stereotyped, two waist places are two identical director circle platforms, one of them director circle platform is gone to the bottom as B2, upper base and dull and stereotyped connecting part are centers is the cloudy cylndrical surface P2 that O2 radius is identical with Stamping Steel Ribbon 4 middle G1 radius, director circle platform cone angle is identical with the cone angle of cloudy round platform H2, A2 with B2 is parallel disk, I2 with J2 is parallel plate level, large sphere outside the left and right of E2 and F2 to be the centre of sphere be O2, G2 with H2 is two identical cloudy round platform surface, one of them cloudy round platform upper and lower two ends, are disk B2 respectively and take K2L2 as the disc of diameter, 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, whole rotor 2 is not only symmetrical about center O2, also be axisymmetric.
Fig. 8 and the shape that Figure 9 shows that distribution of the present invention cone 5.Distribution cone 5 is round platforms, the radius of end face A3 and bottom surface B3 is equal with the radius of two bottom surfaces up and down of the cloudy round platform of rotor 2 respectively, highly also equal with the height of the cloudy round platform of rotor 2, the spatial position of two distributions cones 5 is with following and determine: ensure to assemble two distributions afterwards and bore 5 frustum cone sides and fit with corresponding parallel plane C4 or D4 of the hollow ring of corresponding housing 1 respectively, the conical surface of some D3 to E3 is deflation area, point D3 was the horizontal axis in the center of circle and the intersection point of bottom surface B3, point E3 position be when rotor 2 as shown in Figure 5 paper position forward to as shown in figure 16 perpendicular to paper position time, the intersection point of rotor 2 left side plan and end circle, the conical surface of some D3 to G3 is air inlet face, the conical surface of D3 to G3 is less than 90 degree.
Figure 10, Figure 11 and Figure 12 shows that the shape of housing 1 of the present invention.Housing 1 is the parallel dolioform sphere cutting out two spherical crowns in two, thickness is equal with the width K2M2 of rotor 2, end face A4 and bottom surface B4 are the parallel disks that radius is equal, sphere F4 take O4 as the centre of sphere, the sphere that radius is equal with the radius of large sphere E2 and F2 in rotor about 2 outside, the diagonal angle of housing 1 sphere is a hollow ring, two side C4 with D4 of hollow ring are parallel planar circulars, E4 is the cylinder of central shaft by O4, be positioned on the diagonal of housing, the spatial position of the two plane C4 that hollow ring is parallel and D4 is with following and determine: guarantee assembles rear C4 and D4 two plane and two distributions and bores 5 frustum cone sides and fit respectively.Whole housing 1 is symmetrical about billiard table center O4.
The shape of cushion block 6 has been shown in Figure 15.Cushion block 6 is one section of annulus, its outer side surface A5 is the cylinder that radius is equal with housing 1 hollow ring E4 external diameter, inner side surface B5 is the sphere that radius is equal with housing 1 sphere F4 radius, two waist C5 and D5 are the cylinders that radius is equal 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 shape is axisymmetric.
As shown in figure 16, after ball-type pneumatic vane motor of the present invention assembles, center O1, O2, O4 of each parts overlap.
Operation working principle of the present invention is as follows:
As Figure 18, in one end of pneumatic motor, rotor 2, blade 3, Stamping Steel Ribbon 4, air cavity is divided into three respective independently Seal cage Q1, Q2 and Q3 by distribution cone 5 and housing 1.In one end of rotor 2, when rotor 2 is in air inlet initial position (as Figure 13 or 7a), high pressure air enters air cavity Q1 from the air inlet face that distribution is bored, as Figure 18, at this moment air cavity Q3 is filled with high pressure air, and air cavity Q2 is then low pressure gas, the pressure reduction that three air cavitys are formed, rotor produces moment of torsion, rotor is rotated counterclockwise, then promote blade and be rotated counterclockwise.When rotor is rotated counterclockwise, the deflation area that the low pressure gas in air cavity Q2 is bored by distribution is discharged.When high pressure air continues to enter air cavity Q1 from the air inlet face of distribution cone, rotor continues to be rotated counterclockwise.When rotor forwards Figure 19 position to, and when continuing to be rotated counterclockwise, air cavity Q3 becomes low pressure exhaust chamber then from high pressure admission chamber, and high pressure air then continues to enter air cavity Q1, and air cavity Q2 is still low pressure exhaust chamber.The moment of torsion that draught head produces continues drive rotor and is rotated counterclockwise, as Figure 20.At this moment Q1 is high pressure admission chamber, Q2 and Q3 is low pressure exhaust chamber.When rotor rotates counterclockwise Figure 17 position, the low pressure gas in exhaust cavity Q2 drains, and Q1 is still high pressure admission chamber, and Q3 is still low pressure exhaust chamber, and at this moment high pressure air enters new high pressure admission chamber from the air inlet face of distribution cone again, and drive rotor continues to be rotated counterclockwise.When rotor rotates to Figure 19 position, oil pocket Q1 becomes low pressure exhaust chamber then from high pressure admission chamber, and at this moment Q3 is still low pressure exhaust chamber, and high pressure air continues to enter new high pressure admission chamber, and drive rotor continues to be rotated counterclockwise.So go round and begin again, drive rotor is constantly rotated counterclockwise.At the other end of pneumatic motor, situation is also identical with this one end.
Above-described embodiment is used for explaining and the present invention is described, instead of limits this aspect, and in the protection domain of spirit of the present invention and claim, any amendment make this aspect and change, all fall into protection scope of the present invention.
Claims (1)
1. a spherical blade formula pneumatic motor, is characterized in that, it comprises housing (1), rotor (2), two blades (3), two Stamping Steel Ribbons (4), two distribution cones (5) and two cushion blocks (6); Rotor (2) is positioned at housing (1) center, housing (1) is positioned at outside, two distributions cone (5) lay respectively in conical hollow face, rotor (2) two ends, two blades (3) lay respectively at the both sides of rotor (2), and in the hollow ring being placed in housing (1) diagonal angle and guiding groove, with rotor (2) at an angle, this angle be just cut to housing (1) height and the ratio of housing (1) end circular diameter; The frustum cone side that (5) are bored in a plane of blade (3) and distribution fits, Stamping Steel Ribbon (4) is positioned between rotor (2) and blade (3), a plane of its plane side and rotor (2) is fitted, then fit with the cylinder E1 of blade (3) in cylinder side, cushion block (6) is positioned at the hollow ring at housing (1) diagonal angle, just in time fills up the vacancy formed by blade (3), rotor (2) and Stamping Steel Ribbon (4);
Described blade (3) is enclosed by two plane A1, B1 and two cylinders C1, E1 and forms; Wherein, the cylinder that cylinder C1 is center is centre of sphere O1, radius is identical with the radius of the cylinder E4 of the hollow ring of housing (1), cylinder E1 is center is centre of sphere O1, radius is 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) is equal with the hollow ring width of housing (1); The length of O1K1 is the half of rotor (2) thickness and the height sum of Stamping Steel Ribbon;
Described Stamping Steel Ribbon (4) upside is a center is centre of sphere O1, the cylinder that radius is equal with the cylinder E1 radius of blade (3), downside is a plane, the perpendicular distance of centre of sphere O1 and this underside plan is the half of rotor (2) thickness, cylinder G1 is center is centre of sphere O1, the cylinder that radius is equal with the cylinder P2 radius of rotor (2), sphere F1 is the centre of sphere is O1, the sphere that radius is equal with the sphere F4 radius of housing (1), plane H1 is parallel with I1, the distance of plane H1 and I1 is the width of Stamping Steel Ribbon (4), the width of Stamping Steel Ribbon (4) is equal with the thickness of blade (3), blade (3) and Stamping Steel Ribbon (4) are axisymmetric,
Described rotor is one flat plate in the middle of (2), in the middle of dull and stereotyped, two waist places are two identical director circle platforms, one of them director circle platform bottom surface is face B2, upper bottom surface and dull and stereotyped connecting part are centers is centre of sphere O2, the cloudy cylndrical surface P2 that radius is identical with the radius of cylinder G1 in the middle of Stamping Steel Ribbon (4), director circle platform cone angle is identical with the cone angle of cloudy round platform, bottom surface A2 with B2 of two director circle platforms is parallel disks, two dull and stereotyped planar I 2 are parallel with J2, large sphere outside the left and right of sphere E2 and F2 to be the centre of sphere be O2, G2 with H2 is two identical cloudy round platform surface, one of them cloudy round platform upper and lower two ends, are disk B2 respectively and take K2L2 as the disc of diameter, the distance of two parallel plane I2 and J2 is the thickness of rotor (2), the length of straigh line of K2M2 is the width of rotor (2), K2 is the intersection point of the orthographic projection of sphere E2 and the orthographic projection of cloudy round platform, M2 is the intersection point of the orthographic projection of sphere E2 and the orthographic projection of cloudy round platform G2, L2 is the intersection point of the orthographic projection of sphere F2 and the orthographic projection of cloudy round platform, whole rotor (2) is not only symmetrical about centre of sphere O2, is also axisymmetric,
Described distribution cone (5) is a round platform, the radius of end face A3 and bottom surface B3 is equal with the radius of upper and lower two bottom surfaces of rotor (2) cloudy round platform respectively, highly also equal with the height of rotor (2) cloudy round platform, the spatial position of two distributions cone (5) is to determine as follows: after guarantee assembles, two distribution cone (5) frustum cone sides fit with corresponding parallel plane C4 or D4 of the hollow ring of corresponding housing (1) respectively, the conical surface of some D3 to E3 is 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 is when rotor 2 is perpendicular to paper position, the intersection point of rotor 2 left side plan and end circle, the conical surface of some D3 to G3 is air inlet face, the conical surface of D3 to G3 is less than 90 degree,
Described housing (1) is the parallel dolioform sphere cutting out two spherical crowns in two, thickness is equal with the width K2M2 of rotor (2), end face A4 and bottom surface B4 are the parallel disks that two radiuses are equal, sphere F4 take O4 as the centre of sphere, the sphere that radius is equal with the radius of large sphere E2 and F2 in outside, rotor (2) left and right, the diagonal angle of housing (1) sphere is a hollow ring, two side C4 with D4 of hollow ring are parallel planar circulars, the cylinder E4 of hollow ring is the cylinder of central shaft by centre of sphere O4, is positioned on the diagonal of housing; Whole housing (1) is symmetrical about centre of sphere O4;
Described centre of sphere O1, centre of sphere O2, centre of sphere O4 all with housing (1) center superposition;
Described cushion block (6) is one section of annulus, its outer side surface A5 is the cylinder that radius is equal with the radius of the cylinder E4 outer side surface of housing (1) hollow ring, inner side surface B5 is the sphere that radius is equal with housing (1) sphere F4 radius, and two waist C5 and D5 are the cylinders that radius is equal with the radius of blade (3) bottom surface cylinder E1; Distance between two faces of cushion block (6) except outer side surface A5, inner side surface B5, two waist C5 and D5 is the thickness of cushion block (6), and the thickness of cushion block (6) is identical with blade (3) thickness; Cushion block (6) shape is axisymmetric;
Pressurized gas are from the air inlet face input of the some D3 to G3 of distribution cone (5), and low-pressure gas exports from the deflation area of the some D3 to E3 of distribution cone (5), and pneumatic motor output torque is to load.
Priority Applications (1)
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CN201110453992.XA CN102562171B (en) | 2011-12-30 | 2011-12-30 | Spherical blade pneumatic motor |
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CN201110453992.XA CN102562171B (en) | 2011-12-30 | 2011-12-30 | Spherical blade pneumatic motor |
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CN102562171B true CN102562171B (en) | 2015-04-29 |
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CN201110453992.XA Expired - Fee Related CN102562171B (en) | 2011-12-30 | 2011-12-30 | Spherical blade pneumatic motor |
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CN103883356B (en) * | 2013-12-16 | 2017-02-22 | 浙江大学 | Blade pneumatic motor |
Citations (5)
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 |
-
2011
- 2011-12-30 CN CN201110453992.XA patent/CN102562171B/en not_active Expired - Fee Related
Patent Citations (5)
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 |
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