CN103835768B - A kind of steam turbine - Google Patents

A kind of steam turbine Download PDF

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Publication number
CN103835768B
CN103835768B CN201210479001.XA CN201210479001A CN103835768B CN 103835768 B CN103835768 B CN 103835768B CN 201210479001 A CN201210479001 A CN 201210479001A CN 103835768 B CN103835768 B CN 103835768B
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Prior art keywords
duct
rotating disc
cylinder body
boom plate
annulus
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CN103835768A (en
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袁丽君
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QUANJIAO DONGRUN ELECTRONICS TECHNOLOGY Co.,Ltd.
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Wuhu Wen Qing Mechanical Equipment Design Co Ltd
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Abstract

The present invention relates to a kind of steam turbines, its structure includes: annulus duct cylinder body (GT), duct boom plate (XB), rotating disc (P), couple rotor (C), injection apparatus (PS), steam exhaust device (PZ), wherein annulus duct cylinder body (GT) is the stationary housing for having annular cavity, its axial plane cross-sectional view is circle, duct boom plate (XB) is located in the cavity of annulus duct cylinder body (GT), it is distributed along arc-shaped surface, it is coupled as one with annulus duct cylinder body (GT), annulus duct cylinder body (GT) is provided with cylinder body annular groove along cavity, rotating disc (P) is located in cylinder body annular groove;Couple rotor (C) is mounted on rotating disc (P), in cavity, its radial outer edge is in contact with cavity inner surface, its pivot center is vertical with the pivot center of rotating disc (P), it is tangent with the annulus axis of cavity, coupling slot is provided with along radial direction, duct boom plate (XB) passes through coupling slot, when couple rotor (C) and rotating disc (P) and annulus duct cylinder body (GT) relatively rotate, duct boom plate (XB) and slidably engaging for coupling slot push couple rotor (C) around own rotation axis rotation.

Description

A kind of steam turbine
Technical field
The present invention relates to a kind of steam turbines.
Background technique
Steam turbine according to the present invention can be widely applied to the national warp such as engineering machinery, power generation, ship of automobile industry Ji field.
The existing steam turbine being widely used is gas turbine form, knot especially for use in the steam turbine on ship Structure is complex huge, and the dynamic efficiency of steam turbine especially generally used now does not all reach ideal level, and Energy conservation and environmental protection today requires under very urgent situation, and automobile industry more needs efficient with inflating medium such as steam, pressure Contracting air-liquid gas etc. is the power device in energy source.
The invention proposes a kind of design schemes of completely new steam turbine, have structure simple, reliable for operation, high-efficient Feature.
About the explanation of nouns in the invention patent narration:
1. axial plane cross-sectional view: the resulting view of cutting in the plane to coincide with pivot center.As shown in Figure 1.
2. surfaces of revolution cross-sectional view: projecting resulting view in perpendicular plane with pivot center.As shown in Figure 2.
3. pivot center: the pivot center of rotor or revolution space.Pivot center O as shown in figure 1.
4. annulus axis: axial plane cross-sectional view is circular said three-dimensional body annulus, the circular axis of circle.As in Figure 1 and Figure 2 Q。
Summary of the invention
The present invention relates to a kind of steam turbine, structure specifically includes that annulus duct cylinder body (GT), duct boom plate (XB), turns Moving plate (P), couple rotor (C), injection apparatus (PS), steam exhaust device (PZ), wherein annulus duct cylinder body (GT), which is one, circle The stationary housing of toroidal cavity, the axial plane section view diagram shape of annulus duct cylinder body (GT) are circle, and duct boom plate (XB) is located at circle In the annular cavity of ring duct cylinder body (GT), the arc-shaped surface along annular cavity is distributed, and is joined with ring duct cylinder body (GT) It becames one, annulus duct cylinder body (GT) is provided with cylinder body annular groove along annular cavity, and rotating disc (P) is located in cylinder body annular groove;
Couple rotor (C) is mounted on rotating disc (P), be located at annular cavity in, the radial outer edge of couple rotor (C) with The inner surface of annular cavity is in contact, and pivot center R is vertical with the pivot center O of rotating disc (P), and and annular cavity Annulus axis Q it is tangent;
Couple rotor (C) is provided with coupling slot along radial direction, and duct boom plate (XB) passes through coupling slot, as couple rotor (C) When relatively rotating with rotating disc (P) and annulus duct cylinder body (GT), duct boom plate (XB) is pushed away with slidably engaging for coupling slot Dynamic couple rotor (C) surrounds own rotation axis R rotation;
Duct boom plate (XB) is distributed along the arc-shaped surface of annular cavity, so that couple rotor (C) is with rotating disc (P) and circle When ring duct cylinder body (GT) is produced relative rotation and revolved with uniform revolving speed, couple rotor (C) is because of coupling slot and duct boom plate (XB) slidably engage and around own rotation axis R rotation in the form of reciprocally swinging;
Using duct boom plate (XB) and the contact position of the side rotating disc (P) as starting point, when rotating disc (P) drives couple rotor (C) when rotating, coupling slot is slidably engaged since start position and duct boom plate (XB), with rotating disc (P) and annulus duct Relative rotation between cylinder body (GT), couple rotor (C) rotation about one week, coupling slot under the thrust of duct boom plate (XB) The position that the duct boom plate (XB) of the other side rotating disc (P) is contacted with rotating disc (P) is reached, with the rotation of rotating disc (P), coupling Rotor (C) opposite direction rotation again under the thrust of duct boom plate (XB) is closed, coupling slot is made to return to duct boom plate again (XB) with the starting point of the contact position of the side rotating disc (P), rotating disc (P) drives couple rotor (C) to rotate one week at this time, coupling It closes rotor (C) rotation and swings an oscillation cycle, duct boom plate (XB) is a closed circular structure;Couple rotor (C) will be justified The arc surface of ring duct cylinder body (GT), rotating disc (P), the space between duct boom plate (XB) three are divided into pressure area and release Area, inflating medium enter the expansion of pressure area and generate pressure promotion couple rotor (C) in annular cavity around rotating disc (P) Center of rotation is rotated to distressed zone, to drive rotating disc (P) output torque.
Injection apparatus (PS) is located at the duct boom plate (XB) of annulus duct cylinder body (GT) to pressure area's jet expansion medium With the pressure area side near rotating disc (P) contact position, steam exhaust device (PZ) is located at the duct string of annulus duct cylinder body (GT) Distressed zone side near plate (XB) and rotating disc (P) contact position.
Duct boom plate (XB) is distributed along the arc-shaped surface of annular cavity, so that couple rotor (C) is with rotating disc (P) and circle Ring duct cylinder body (GT) produces relative rotation and when with uniform rotational speed, and couple rotor (C) is because of coupling slot and duct boom plate (XB) slidably engage and around own rotation axis with sine curve rule carry out reciprocating swing type rotation.
Boom plate ring is installed on duct boom plate (XB).Rotor ring is housed on couple rotor (C).It is located on duct boom plate (XB) Pressure area side near duct boom plate (XB) and rotating disc (P) contact position is equipped with pressing aid wraping plate.
Steam turbine of the present invention is made of multiple coaxial annulus duct cylinder bodies (GT).Injection apparatus (PS) includes by timing The opening and closing of the cam mechanism driving valve of gear control.
Detailed description of the invention
The axial plane cross-sectional view of one of Fig. 1 embodiment of the present invention.
The couple rotor of Fig. 2 embodiment illustrated in fig. 1 of the present invention and the view of rotating disc assembly.
Fig. 3 couple rotor view.
One of Fig. 4 embodiment illustrated in fig. 1 operation principle schematic diagram of the present invention.
The two of Fig. 5 embodiment illustrated in fig. 1 operation principle schematic diagram of the present invention.
The partial view of embodiment of the Fig. 6 equipped with boom plate ring.
The partial view of embodiment of the Fig. 7 equipped with rotor ring.
The partial sectional view of embodiment of the Fig. 8 equipped with pressing aid wraping plate.
Specific embodiment
In the Detailed description of the invention of the invention patent, the structure and size and shape of the components of diagram do not represent actual The structure and size and shape of components do not represent the actual size proportionate relationship between components yet, and diagram is only with concise Mode is explained the embodiment of the present invention.
Fig. 1 shows the axial plane cross-sectional view of one of embodiment of the present invention, it can be seen from the figure that steam turbine of the present invention Structure specifically include that annulus duct cylinder body (GT), duct boom plate (XB), rotating disc (P), couple rotor (C), injection apparatus (PS), the position of steam exhaust device (PZ) and these devices, Fig. 2 show the couple rotor (C) and rotating disc (P) of the present embodiment The view of assembly, Fig. 3 show the view of couple rotor (C).
The cylinder body of annulus duct shown in Fig. 1 (GT) is the stationary housing for having annular cavity K, the axis of annular cavity K Face cross-sectional view is circle, and duct boom plate (XB) is located in annular cavity K, and the arc-shaped surface along annular cavity K is distributed, and with Annulus duct cylinder body (GT) is coupled as one, and annulus duct cylinder body (GT) is provided with cylinder body annular groove, rotating disc along annular cavity K () is located in cylinder body annular groove.
Couple rotor shown in Fig. 1 and Fig. 2 (C) is mounted on rotating disc (P), is located at the circular ring shape of annulus duct cylinder body (GT) In cavity K, the radial outer edge of couple rotor (C) is in contact with the inner surface of annular cavity K, pivot center R and rotating disc (P) pivot center O is vertical, and tangent with the annulus axis Q of annular cavity K.
Shown in Fig. 3, it can be seen that couple rotor (C) is provided with coupling slot along radial direction, and duct boom plate (XB) can be worn Overcoupling slot, when couple rotor (C) and rotating disc (P) and annulus duct cylinder body (GT) relatively rotate, duct boom plate (XB) engage opposite with coupling slot pushes couple rotor (C) around pivot center R rotation, and duct boom plate (XB) is along circular ring shape sky The arc-shaped surface of chamber K is distributed, so that couple rotor (C) produces relative rotation simultaneously with rotating disc (P) and annulus duct cylinder body (GT) When being revolved with even speed, couple rotor (C) surrounds own rotation axis due to slidably engaging because coupling slot and duct boom plate (XB's) Line R rotation in the form of reciprocally swinging.
Using duct boom plate (XB) and the contact position of the side rotating disc (P) as starting point, when rotating disc (P) drives couple rotor (C) when rotating, coupling slot is slidably engaged since start position and duct boom plate (XB), as rotating disc (P) is in annulus duct Rotation in cylinder body (GT), couple rotor (C) rotation about one week under the thrust of duct boom plate (XB), coupling slot, which reaches, to be turned The position that the duct boom plate (XB) of the other side Moving plate (P) is contacted with rotating disc (P), with the rotation of rotating disc (P), couple rotor (C) the reversed rotation again under the action of the thrust of duct boom plate (XB) makes coupling slot return to duct boom plate (XB) again and turn The starting point of the contact position of the side Moving plate (P), at this point, rotating disc (P) drives couple rotor (C) public affairs to circle, couple rotor (C) rotation swings an oscillation cycle, it follows that duct boom plate (XB) is a closed cyclic structure.
Couple rotor (C) will be between the arc surface of annulus duct cylinder body (GT), rotating disc (P), duct boom plate (XB) three Space be divided into pressure area and distressed zone, it is swollen that inflating medium such as steam, combustion gas, compressed gas, liquefied gas etc. enters pressure area The swollen pressure that generates pushes the pivot center O of couple rotor (C) in toroidal cavity K around rotating disc (P) to rotate to distressed zone, from And drive rotating disc (P) output torque.
In order to illustrate the above process, show duct boom plate (XB) in arc surface n~m~e of annular cavity K with Fig. 4 One week plan view is circumferentially unfolded on~m '~n ', the arc surface in space is expanded into a circular plan view, although empty Between arc surface expand into a circular plane and can lack accuracy, but can concisely show its working principle.
Shown in Fig. 4, inner circle 1-2-3-4-5-6-7-8 indicates the arc position adjacent with the side of rotating disc (P) N, outer circle 21-22-23-24-25-26-27-28 indicate the arc position n ' adjacent with the other side of rotating disc (P), From one duct boom plate (XB) successively returns point 1 after point 9,10,11,12,13,14,15 since point 1, by It is a closed ring-type that this, which can be seen that duct boom plate (XB),.In the present embodiment, when couple rotor (C) is with rotating disc (P) It produces relative rotation with annulus duct cylinder body (GT) and when with uniform rotational speed, couple rotor (C) is because of coupling slot and duct string Slidably engaging for plate (XB) and around pivot center R with sine curve rule carry out reciprocating swing type rotation, couple rotor (C) with Rotating disc (P) public affairs circle, the coupling slot of couple rotor (C) then reciprocal rotation two weeks, because the rotation of couple rotor (C) is not With uniform revolving speed rotation but with sine curve rule rotation, therefore, angle 2~9 is less than 90 °, angle 4~11 is greater than 270 °, angle 6~13 be greater than 270 °, angle 8~15 less than 90 °, and angle 3~10,7~14 is about 180 °, can be with from Fig. 4 Seeing, annular cavity K is separated into 2 parts K1 and K2 by duct boom plate (XB), when couple rotor (C) is in point 1, coupling It closes rotor (C) and K2 is separated into two equal spaces, when couple rotor (C) is in point 12, couple rotor (C) is again by K1 Two equal spaces are separated into, during couple rotor (C) revolves around pivot center O, K1 and K2 are sprayed in turn Penetrate expansion and the work of steam discharge.
In order to illustrate the working condition of space K1 and K2 and the curve law of duct boom plate (XB), with Fig. 5 with another kind side Formula illustrates its working principle, although the plan view that the cambered surface in space expands into a rectangle can still lack accuracy, uses Another way signal can concisely show its working principle.
From fig. 5, it is seen that arc-shaped surface of the duct boom plate (XB) with sinusoidal rule in annular cavity K is divided The port of left and right two of cloth, duct boom plate (XB) is linked, and annular cavity K is separated into K1 and K2 by duct boom plate (XB) Two spaces, when couple rotor (C) rotates from left to right as shown, in the position of diagram, the couple rotor (C) of space K1 Leftward space change from small to big for press area, at this point, inflating medium by injection apparatus (PS) spray into and expand against couple rotor (C) It rotates to the right, the right side of the space of the couple rotor (C) of space K1 is distressed zone from large to small, and the medium after expanding is coupled Rotor (C) is pressed through steam exhaust device (PZ) discharge;The pressure area of space K2 and distressed zone are also equally to be alternately present, therefore As it can be seen that the pressure of K1 and K2 two spaces and release have the function of mutually compensating, so that the expansion of steam turbine of the present invention The penetrating and discharge of medium have stability and continuity in total amount.
From Fig. 1 and Fig. 5 as can be seen that injection apparatus (PS) be located at annulus duct cylinder body (GT) duct boom plate (XB) and Pressure area side near rotating disc (P) contact position, steam exhaust device (PZ) are located at the duct boom plate of annulus duct cylinder body (GT) (XB) and the distressed zone side near rotating disc (P) contact position.
Fig. 6 show the local axial plane cross-sectional view of the embodiment on duct boom plate (XB) equipped with boom plate ring, the boom plate of diagram Ring is mounted in boom plate groove, elastic device is housed, to keep boom plate ring and rotating disc between duct boom plate (XB) and boom plate ring (P) contact between, to improve the sealing performance of pressure area.
Fig. 7 show the rotor axial plane partial sectional view of the embodiment on couple rotor (C) equipped with rotor ring, installation side Formula, identical as the piston-engined piston ring of linear reciprocating using principle, this is no longer going to repeat them.
Fig. 8 show the partial sectional view for being equipped with the embodiment of pressing aid wraping plate, and the pressing aid wraping plate of diagram is mounted on duct On boom plate (XB), and it is located at the pressure area side near duct boom plate (XB) and rotating disc (P) contact position, works as couple rotor (C) when rotating from left to right with rotating disc (P), pressing aid wraping plate is pressed into wraping plate slot by the coupling slot of couple rotor (C) makes coupling After conjunction rotor (C) passes through, pressing aid wraping plate is tilted rapidly under the action of the elastic means and is kept in contact with rotating disc (P), Effect is to improve the sealing performance in pressure area.
Steam turbine of the present invention can be made of multiple coaxial annulus duct cylinder bodies (GT), and the coupling of each cylinder body turns Sub (C) mutually staggers and is in the state of angle bisecting, so that each annulus duct cylinder body (GT) is in the stress mutually compensated The torque of state, output is more stable and continuous.
About injection apparatus (PS), the supply system of steam exhaust device (PZ) and inflating medium, control system and sealing dress It sets, lubricating system, supporting system, safety guard etc., those skilled in the art has known, and extensive in this field Using no longer repeating one by one herein.
Above-described embodiment diagrammatically illustrates the present invention, but the above-described embodiment illustrated by way of illustration is not Limitation of the present invention, the present invention are defined by the claims.

Claims (8)

1. a kind of steam turbine, structure specifically includes that annulus duct cylinder body, duct boom plate, rotating disc, couple rotor, injection dress It sets, steam exhaust device, it is characterised in that: the annulus duct cylinder body is the stationary housing for having annular cavity, the annulus The axial plane section view diagram shape of duct cylinder body is circle, and the duct boom plate is located at the annular cavity of the annulus duct cylinder body Interior, the arc-shaped surface along annular cavity is distributed, and is coupled as one with the annulus duct cylinder body, and annulus duct cylinder body is along circle Toroidal cavity is provided with cylinder body annular groove, and the rotating disc is located in the cylinder body annular groove;
The couple rotor is mounted on rotating disc, is located in the annular cavity, the radial outer edge and annulus of couple rotor The inner surface of shape cavity is in contact, and pivot center is vertical with the pivot center of rotating disc, and the annulus axle with annular cavity Line is tangent;
The couple rotor is provided with coupling slot along radial direction, and duct boom plate passes through coupling slot, when couple rotor and rotating disc with When annulus duct cylinder body relatively rotates, duct boom plate and slidably engaging for coupling slot push couple rotor around own rotation Axis rotation;
The duct boom plate is distributed along the arc-shaped surface of the annular cavity, so that couple rotor is with rotating disc and annulus duct Cylinder body produces relative rotation and when with uniform rotational speed, and couple rotor surrounds due to slidably engaging because coupling slot and duct boom plate Own rotation axis rotation in the form of reciprocally swinging;
The duct boom plate and the contact position of rotating disc side are starting point, when rotating disc drives couple rotor rotation, coupling Slot is slidably engaged since start position and duct boom plate, with the relative rotation between rotating disc and annulus duct cylinder body, coupling Rotor rotation about one week under the thrust of duct boom plate is closed, coupling slot reaches duct boom plate and the rotation of the rotating disc other side Disk contact position, with the rotation of rotating disc, couple rotor opposite direction rotation again under the thrust of duct boom plate makes to couple Slot returns to the starting point of the contact position of duct boom plate and rotating disc side again, and rotating disc drives couple rotor rotation at this time One week, couple rotor rotation swung an oscillation cycle, and the duct boom plate is a closed circular structure;The couple rotor Space between the arc surface of annulus duct cylinder body, rotating disc, duct boom plate three is divided into pressure area and distressed zone, expansion Medium enters the expansion of pressure area and generates the center of rotation that pressure pushes couple rotor to surround rotating disc in the annular cavity It is rotated to distressed zone, to drive rotating disc output torque.
2. steam turbine according to claim 1, it is characterised in that: the injection apparatus to pressure area's jet expansion medium, And the pressure area side near the duct boom plate and rotating disc contact position of annulus duct cylinder body, the steam exhaust device are located at The duct boom plate of annulus duct cylinder body and the distressed zone side near rotating disc contact position.
3. steam turbine according to claim 1, it is characterised in that: circular arc of the duct boom plate along the annular cavity Surface distribution, so that couple rotor produces relative rotation with rotating disc and annulus duct cylinder body and when with uniform rotational speed, coupling Conjunction rotor is surrounded own rotation axis because of coupling slot and slidably engaging for duct boom plate and is carried out with sine curve rule toward physical pendulum Dynamic formula rotation.
4. steam turbine according to claim 1, it is characterised in that: be equipped with boom plate ring on the duct boom plate.
5. steam turbine according to claim 1, it is characterised in that: rotor ring is housed on the couple rotor.
6. steam turbine according to claim 1, it is characterised in that: be located at duct boom plate and rotating disc on the duct boom plate Pressure area side near contact position is equipped with pressing aid wraping plate.
7. steam turbine according to claim 1, it is characterised in that: the steam turbine is by multiple coaxial annulus duct cylinder body groups At.
8. steam turbine according to claim 1 or claim 7, it is characterised in that: the injection apparatus includes being controlled by timing gears Cam mechanism driving valve opening and closing.
CN201210479001.XA 2012-11-22 2012-11-22 A kind of steam turbine Active CN103835768B (en)

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Application Number Priority Date Filing Date Title
CN201210479001.XA CN103835768B (en) 2012-11-22 2012-11-22 A kind of steam turbine

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Application Number Priority Date Filing Date Title
CN201210479001.XA CN103835768B (en) 2012-11-22 2012-11-22 A kind of steam turbine

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CN103835768A CN103835768A (en) 2014-06-04
CN103835768B true CN103835768B (en) 2019-01-11

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Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2528317B2 (en) * 1987-06-09 1996-08-28 洋一 山崎 Pure fluid type variable capacity turbocharger
CN1056435C (en) * 1996-04-18 2000-09-13 沈泉贵 Vaneless steam turbine
EP2522808A1 (en) * 2011-05-10 2012-11-14 Aella SA Turbo-engine, particularly internal combustion engine
CN202325699U (en) * 2011-09-28 2012-07-11 江顺天 Moving vane-type steam turbine
CN102661195A (en) * 2012-04-20 2012-09-12 袁丽君 Circumferential rotation type piston engine

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Effective date of registration: 20181123

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