Double screw rotor assembly with electrically controlled clearance adjustment means

Information

  • Patent Grant
  • 6257839
  • Patent Number
    6,257,839
  • Date Filed
    Thursday, June 8, 2000
    24 years ago
  • Date Issued
    Tuesday, July 10, 2001
    23 years ago
Abstract
A double screw rotor assembly includes two screw rotors meshed in a bushing inside a casing. The threads of the screw rotors have a constant pitch, and define with the bushing a plurality of air chambers in the pitch. The volumes of the air chambers reduce gradually from the inlet toward the outlet due to reduced tooth height so that the outer diameter defined by the tooth tip of the thread of each screw rotor has the shape of an invertedly disposed cone. An electric driving device is controlled to move the bushing axially in the casing relative to the screw rotors in adjusting the clearance between the inside wall of the bushing and the tooth tip of the thread of each screw rotor, so as to minimize the consumption of starting power and facilitate stable running of the screw rotors, Further, a O-ring is provided at the top wall of the busing and pressed on the casing to keep an airtight status, so as to improve the working efficiency.
Description




BACKGROUND OF THE INVENTION




The present invention relates to fluid machinery for controlling a fluid pressure, and more particularly to a double screw rotor assembly that can reduce starting power, start electric current, or adjust operating power. The double screw rotor assembly of the invention can be used in vacuum pumps, air compressors, water or oil pumps, or other fluid media.





FIG. 1

shows a double screw rotor assembly manufactured by KASHIYAMA INDUSTRIES, LTD., and designed for use in a vacuum pump. This structure of double screw rotor comprises two screw rotors


81


and


82


meshed together. Because the screw rotors


81


and


82


have a constant pitch P′ and constant height of tooth H′, the volume of air chamber


810


or


820


does not change while air is transferred from the inlet to the output end


80


, a high pressure difference occurs, thereby causing a reverse flow of air, high noises, and waste of energy.




U.S. Pat. No. 5,667,370 discloses another structure of double screw rotor assembly. According to this design, as illustrated in

FIG. 2

, the meshed screw rotors


83


and


84


have same height of tooth H″, and the pitch is gradually reduced in direction from the input side toward the output side


801


(P


1


>P


2


). Because of P


1


>P


2


, the volume of air chamber


830


or


840


is reduced during transmission, and the pressure in these chambers would be increased gradually. Therefore, when the air chambers were compressed and transmitted to the output end


801


, less pressure difference occurs, the reverse flow of air would be reduced and so as to the high noise. However, because of different pitches and pressure angles are defined at different rotor sections, the fabrication process of the screw rotors


83


and


84


are complicated, resulting in a high manufacturing cost.





FIG. 3

shows still another structure of double screw rotor assembly, which was filed to USPTO for a patent by the present applicant under application Ser. No. 09/372,674. According to this design, two screw rotors are meshed together and mounted in a compression chamber inside a casing, each comprising a spiral thread around the periphery. The thread has a height H made gradually reduced from the input side toward the output side


90


. The threads of the screw rotors define a constant pitch P in order to be manufactured easily. The volumes of the air chambers


910


and


920


reduce gradually from the input side toward the output side, so the pressure can be increased gradually during transmission of air, the consumption of operation power and noise can be reduced. Because a constant pitch P is provided and the height H is made gradually reduced from the input side toward the output side


90


, the outer diameter D has the shape of an invertedly disposed cone, and the inner diameter d has the shape of a regular cone.




According to the aforesaid second and third prior art designs, much starting power is required when starting the double screw rotor assembly. As illustrated in

FIG. 3

, the pressure (i.e. the atmospheric pressure) in all air chambers


910


and


920


, pressure Pi at the input side, and pressure P


0


at the output side, at the initial stage are the same. Because the volumes of the air chambers


910


and


920


are gradually reduced during rotary motion of the screw rotors, the pressure Pmax near the output side surpasses the pressure P


0


(=the atmospheric pressure) at the output side when starting the double screw rotor assembly. Therefore, much more power and electric current are required to drive the rotors


91


and


92


to conquer the flow pressure of all air chambers


910


and


920


. A certain period of time after starting, the flow pressure at the input side


901


is gradually reduced (for example, being drawn into a vacuum state), causing the flow pressure in the air chambers


910


and


920


near the input side


901


to be gradually reduced, and hence the electric power consumed is gradually reduced to the level of the rated working power. Because high working power is required when starting the double screw rotor assembly, high current, noise and vibration occur at the initial state when starting the screw rotors, resulting in an unstable operation.





FIG. 4

shows another prior art design constructed according to U.S. Pat. No. 5,533,887. According to this design, a movable case is sliding in a fixed case, however the spring at the top of the movable case is not adjustable, and the presence of the gap


22


C which is left between the movable case and the fixed case for enabling the movable case to slide in the fixed case which may cause air leakage directly from the high pressure area to the low pressure area, thereby causing a low working efficiency. Further, if the process gas condensed in the gap between movable and fixed cases, the movable case maybe jammed at some position, and the bypass mechanism failed.




In view of the drawbacks of the aforesaid prior art designs, there is a strong demand for a high performance double screw rotor assembly that requires low starting power, and can be conveniently adjusted to fit different manufacturing requirement.




SUMMARY OF THE INVENTION




The present invention has been accomplished to provide a double screw rotor assembly, which eliminates the aforesaid drawbacks. It is one object of the present invention to provide a double screw rotor assembly, which reduces starting power and starting current by adjusting its internal pressure difference, allows the user to adjust operating power for a stable operation, and can be freely adjusted to change the clearance between the rotors and the casing subject to different manufacturing requirements. It is another object of the present invention to provide a double screw rotor assembly, which prevent a leakage to achieve a high performance. According to one aspect of the present invention, the double screw rotor assembly comprises a casing having a receiving chamber; an inlet and an outlet; a bushing axially movably mounted in the receiving chamber inside the casing, the bushing having an inside wall defining a receiving chamber, and an outside wall fitting with the inside wall of the casing; guide means provided to guide axial movement of the bushing relative to the casing; two screw rotors meshed together and mounted in the receiving chamber inside the bushing; and an electric driving means controller to move the bushing axially in the casing relative to the screw rotors to adjust inside pressure in the bushing. According to another aspect of the present invention, the electric driving means comprises at least one rack fixedly mounted in the bushing, and a driving gear meshed with the at least one rack and rotated by, for example, a motor or other electric driving apparatus to move the at least one rack. Chain transmission means, belt transmission means, electromagnetic induction type transmission means may be used instead of the gear and rack transmission mechanism. According to still another aspect of the present invention, the double screw rotor assembly further comprises an O-ring mounted on the top wall of the busing and facing the casing. The O-ring can be made of rubber or any suitable equivalent material. According to still another aspect of the present invention, the double screw rotor assembly further comprises control means controlling the operation of the electric driving means, the control means comprising pressure sensor means, temperature sensor means, wattmeter, or voltmeter which detects the pressure or temperature in the receiving chamber near the outlet, or the value of electric current or voltage at the motor, for enabling the control means to control the electric driving means in moving the bushing subject to the value detected by the pressure sensor means. According to still another aspect of the present invention, the guide means comprises at least one sliding groove formed on the outside wall of the bushing, and at least one guide rib respectively formed integral with the inside wall of the casing and coupled to the at least one sliding groove on the bushing. The sliding groove and the guide rib can be made having any of a variety of designs that facilitate stable movement of the bushing relative to the casing. Further, the outer diameter of the thread of each screw rotor can be made linearly, non-linearly reduced from the inlet to the output, having a convex or concave profile.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a sectional view of a double screw rotor assembly according to the prior art.





FIG. 2

is a sectional view of another structure of double screw rotor assembly according to the prior art.





FIG. 3

is a sectional view of still another structure of double screw rotor assembly according to the prior art.





FIG. 4

is a sectional view of still another structure of double screw rotor assembly according to the prior art.





FIG. 5

is a bottom view of a double screw rotor assembly after removal of the bottom cover according to the present invention.





FIG. 6

is a sectional view AA of the double screw rotor assembly shown in FIG.


5


.





FIG. 7

is a sectional view of the present invention showing the initial stage of the double screw rotor assembly when started.





FIG. 8

is an enlarged view in section of a part of the present invention showing the initial stage of the double screw rotor assembly when started.





FIG. 9

is an enlarged view in section of a part of the present invention, showing the status of the double screw rotor assembly a certain period of time after starting.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




Referring to

FIGS. 5 and 6

, a double screw rotor assembly used in a vacuum pump in accordance with the present invention is shown comprised of a casing


1


, a bushing


2


, two screw rotors


3


and


4


, and an electric driving device


5


.




The casing


1


comprises a top cover


11


, a peripheral shell


12


, and a bottom cover


13


. The top cover


11


has an inlet


111


connected to a container to be drawn into a vacuum status. The peripheral shell


12


comprises an inside wall


121


defining a receiving chamber


10


. The bottom cover


13


comprises an outlet


131


disposed in communication with the atmosphere.




The bushing


2


has a loop-like, or more specifically, double loop-like cross section mounted in the receiving chamber


10


inside the casing


1


, comprising an inside wall


21


, a receiving chamber


20


defined within the inside wall


21


, a top wall


23


, a rubber O-ring


24


around the top wall


23


, and an outside wall


22


fitting the inside wall


121


of the peripheral shell


12


of the casing


1


. Further, guide means


7


is provided for enabling the bushing


2


to be moved axially relative to the casing


1


. The guide means


7


comprises two longitudinal sliding grooves


71


and


72


respectively formed on the outside wall


22


at two opposite sides, and two longitudinal guide ribs


73


and


74


respectively bilaterally formed integral with the inside wall


121


of the peripheral shell


12


of the casing


1


and coupled to the longitudinal sliding grooves


71


and


72


.




The two screw rotors


3


and


4


are meshed together, and mounted inside the receiving chamber


20


in the bushing


2


. Each screw rotor


3


or


4


comprises a spiral thread


30


or


40


raised around the periphery (Alternatively, the screw rotors


3


and


4


can be made having two or more threads). The tooth tip


31


and


41


of the threads


30


and


40


of the screw rotors


3


and


4


are respectively spirally extended, defining a respective outer diameter D


1


and D


2


and meshed with each other. As illustrated, the threads


30


and


40


have a constant pitch, and the outer diameter D


1


or D


2


reduces gradually and linearly from the inlet


111


toward the outlet


131


.




The thread


30


or


40


defines with the inside wall


21


of the bushing


2


a plurality of air chambers


35


or


45


in the respective pitch, i.e., the root of tooth


34


or


44


, the side walls


32


and


33


, or,


42


and


43


, and the inside wall


21


of the bushing


2


define a plurality of air chambers


35


or


45


. As illustrated, the outer diameters D


1


and D


2


that are formed of the tooth tip


31


and


41


of the threads


30


and


40


of the screw rotors


3


and


4


fit the inside wall


21


of the bushing


2


, therefore the inside wall


21


of the bushing


2


is tapered linearly. Each thread


30


or


40


has two side walls


32


and


33


, or,


42


and


43


. The root of tooth


34


or


44


defines an inner diameter d


1


or d


2


having the shape of a regular cone. Because the tooth height H


1


or H


2


gradually reduces in direction from the inlet


111


toward the outlet


131


, the volumes of the air chambers


35


or


45


were gradually reduced in direction from the inlet


111


toward the outlet


131


.




The aforesaid electric driving device


5


is comprised of two racks


51


and


52


, a driving gear


53


meshed with the racks


51


and


52


, and a motor


54


controlled to turn the driving gear


53


. Upon rotary motion of the driving gear


53


, the bushing


2


is moved with the racks


51


and


52


axially relative to the screw rotors


3


and


4


. By means of the effect of the guide means


7


, the axial movement of the bushing


2


is accurate and stable.




Referring to

FIG. 7

, when starting the double screw rotor assembly, the flow pressure in the air chambers


35


and


45


between the inlet


111


and the outlet


131


is equal to the atmosphere at the beginning. At this stage, the motor


54


is operated to move the bushing


2


slightly axially downwards. The O-ring


24


at the top wall


23


of the bushing


2


is released from pressure, enabling gas to leak from the lower high pressure area to the upper low pressure area via gap between the outside wall


22


and top wall


23


of the bushing


2


. As illustrated in

FIG. 8

, because the outer diameter D


2


of the screw rotor


4


has the shape of an invertedly disposed cone, minor downward displacement of the bushing


2


causes the clearance t between the inside wall


21


and the tooth tip


41


to be relatively larger, enabling air to leak from the air chamber


45


of relatively higher pressure to the air chamber


45


′ of relatively lower pressure via the clearance t. This design prevents simultaneous compression of the air chambers


45


and


45


′ in the same time when the air chambers


45


and


45


′ are at the atmosphere, and therefore it is not necessary to start the double screw rotor assembly with high power and high electric current.




Referring to

FIG. 9

, a certain period of time after starting, the flow pressure around the inlet


111


is gradually reduced, and the pressure of the air chambers


45


and


45


′ is relatively reduced, and the motor


54


is then driven to move the bushing


2


axially upwards and make the gap between the inside wall


21


of the bushing


2


and the tooth tip


41


smaller, and the O-ring


24


at the top wall


23


of the bushing


2


is compressed and maintained in the sealing status (see FIG.


7


), preventing gas leakage from the high pressure side to the receiving chamber


20


via the outside wall


22


and top wall


23


of the bushing


2


, and therefore the working efficiency is greatly improved.




The application of the present invention is not limited to the starting stage. The invention can also be applied to control the stability of the operating power during running of the double screw rotor assembly, or used for safety control or adjusting the clearance between the rotors and the casing subject to different manufacturing requirements. For example, a control device


6


may be added to the double screw rotor assembly (see FIG.


5


). The control device


6


comprises a pressure sensor


61


(or temperature sensor) disposed inside the receiving chamber


10


near the outlet


131


to detect the pressure (or temperature) of air in the high-pressure area. When the detected pressure (or temperature) surpasses a predetermined value, the control device


6


immediately outputs a signal to the motor


54


, causing the motor


54


to move the bushing


2


slightly axially downwards (see FIG.


7


), therefore the electric current and voltage would be stable, preventing an excessively high operating power. When an overpressure or overheat unexpectedly occurs, the bushing


2


can be rapidly axially moved downwards to prevent an accident.




It is to be understood that the drawings are designed for purposes of illustration only, and are not intended for use as a definition of the limits and scope of the invention disclosed.



Claims
  • 1. A double screw rotor assembly comprising:a casing, said casing comprising an inside wall defining a receiving chamber, an inlet and an outlet respectively disposed in communication with the receiving chamber of said casing; a bushing mounted in the receiving chamber inside said casing and moved axially along the inside wall of said casing, said bushing comprising an inside wall defining a receiving chamber, and an outside wall fitting the inside wall of said casing; an O-ring mounted on a top wall of said bushing and disposed between said bushing and said casing to seal the gap between said bushing and said casing; guide means to guide movement of said bushing in axial direction relative to said casing; two screw rotors meshed together and mounted in the receiving chamber inside said bushing; an electric driving means controlled to move said bushing axially in said casing relative to said screw rotors; and control means to control the operation of said electric driving means, said control means comprising pressure sensor means which detects the pressure in the receiving chamber near said outlet, for enabling said control means to control said electric driving means in moving said bushing subject to the pressure value detected by said pressure sensor means.
  • 2. The double screw rotor assembly of claim 1 wherein said guide means comprises at least one sliding groove formed on the outside wall of said bushing, and at least one guide rib respectively formed integral with the inside wall of said casing and coupled to the at least one sliding groove on said bushing.
  • 3. The double screw rotor assembly of claim 1 wherein said casing is comprised of a peripheral shell, a top cover, and a bottom cover.
  • 4. The double screw rotor assembly of claim 1 wherein said bushing has a double loop-like cross section.
  • 5. The double screw rotor assembly of claim 1 wherein said electric driving means comprises at least one rack fixedly mounted in said bushing, and a driving gear meshed with said at least one rack and rotated to move said at least one rack.
  • 6. The double screw rotor assembly of claim 5 wherein said electric driving means further comprises a motor controlled to turn said driving gear.
  • 7. The double screw rotor assembly of claim 1 wherein said screw rotors each comprise at least one spiral thread.
  • 8. The double screw rotor assembly of claim 7 wherein said at least one spiral thread of each of said screw rotors each has a root of tooth and side walls that define with the inside wall of said bushing at least one air chamber, and the air chambers defined between said screw rotors and the inside wall of said bushing have a volume gradually reduced from said inlet toward said outlet.
  • 9. The double screw rotor assembly of claim 7 wherein said at least one spiral thread of each of said screw rotors has a constant pitch, and the tooth tip of said at least one spiral thread of each of said screw rotors defines an outer diameter having the shape of an invertedly disposed cone.
  • 10. The double screw rotor assembly of claim 9 wherein said outer diameter gradually linearly reduces from said inlet toward said outlet.
Priority Claims (1)
Number Date Country Kind
089201921 Feb 2000 TW
US Referenced Citations (2)
Number Name Date Kind
1323459 Dorr Dec 1919
3605188 McCormick et al. Sep 1971
Foreign Referenced Citations (1)
Number Date Country
384355 Dec 1932 GB