US2975963A - Rotor device - Google Patents

Rotor device Download PDF

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Publication number
US2975963A
US2975963A US795534A US79553459A US2975963A US 2975963 A US2975963 A US 2975963A US 795534 A US795534 A US 795534A US 79553459 A US79553459 A US 79553459A US 2975963 A US2975963 A US 2975963A
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United States
Prior art keywords
rotor
section
male
female
sections
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.)
Expired - Lifetime
Application number
US795534A
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English (en)
Inventor
Nilsson Hans Robert
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.)
Svenska Rotor Maskiner AB
Original Assignee
Svenska Rotor Maskiner AB
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.)
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Publication date
Application filed by Svenska Rotor Maskiner AB filed Critical Svenska Rotor Maskiner AB
Application granted granted Critical
Publication of US2975963A publication Critical patent/US2975963A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
    • F04C23/001—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids of similar working principle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type

Definitions

  • the present invention relates to a rotor device operating with at least two pressure stages and provided with male and female rotors, each one consisting of male and female sections corresponding to the number of stages.
  • the male rotors are provided with helical convex lands and intermediate grooves and the female rotors are provided with helical concave lands and intermediate grooves.
  • This rotor device is particularly intended for compression or expansion of gaseous media in several stages.
  • a characteristic feature of the present invention is that the cross section of the male rotor sections show a common basic profile and that likewise the cross sections of the female rotor sections show a common basic profile. Furthermore, the lands of the female sections are, in a lower pressure stage, provided with addendum portions outside the profile of the lands of the female section in the next higher pressure stage, the grooves of the corresponding male section being provided with recesses or dedendums in their bottoms corresponding to these addendum portions in order to obtain a suction volume corresponding to the gas pressure.
  • the female section of the second stage i.e. the stage with higher pressure
  • the male section shows a basic profile without bottom recesses or dedendums.
  • Another characteristic feature of the invention is that the addendum portions of the female section are located outside the pitch circle of the female section and that the recesses in the grooves of the male section corresponding to these addendum portions are located inside the pitch .circle of the male section.
  • the invention is further characterized in that in each rotor the sections show the same pitch diameter.
  • respective rotor consists of integral rotor sections so that each rotor can be journalled only at its outer ends while the sections of said rotor are mutually sealed.
  • the male rotor is fourthreaded and has a wrap angle for its lands in respective stage below 360. In the low pressure stage, such wrap angle can be lying within the limits 275-325 and preferably be maximum 300". In the high pressure stage such wrap angle can be lying within the limits l50-l90 and preferably be minimum 170.
  • the ratio or relation between rotor length and rotor diameter is in the low pressure stage preferably lying be tween 1.1 and 1.4 and in the high pressure stage between 0.6 and 0.8 and preferably said relation can be about 1.25 and 0.7 in respective stage.
  • the land profiles of the male sections respectively the groove profiles of the female sections are formed by corresponding equal circular arcs in the two stages and that the addendum por- 2,975,963 Patented Mar. 21, 1961 ice.
  • tions of the side section and the recesses of the male section show profiles likewise formed by circular arcs.
  • a further characteristic feature of the invention is that the male and female rotors run with a clearance against each other, which clearance at full meshing between male land and female groove preferably is 0.08-0.1'1 mm. in both the low pressure section and the high pressure sectiori and that the rotors have a common synchronising gear for their rotor sections.
  • Fig. 1 sows a vertical central longitudinal section through a compressor designed according to the invention.
  • Fig. 2 shows the compressor rotors in a horizontal longitudinal section through the compressor in Fig. 1.
  • Fig. 3 shows a transverse section through the rotors in the high pressure side taken on the line '3-3 in Fig. 1.
  • Fig. 4 shows transverse section through the low pressure rotors taken on the line 4-4 in Fig. 1.
  • Fig. 1 shows a two stage compressor.
  • This compressor has a housing consisting of a 'low pressure end 10, an upper shell 12, a lower shell 14 and a high pressure end 16.
  • a low-pressure inlet 18 is arranged in the low pressure end 10 and in the lower shell 14.
  • an intermediate pressure outlet 20 is arranged in the upper shell 12
  • an intermediate pressure inlet 22 is arranged in the lower shell 14
  • a high pressure outlet 24 is arranged in the upper shell 12 and in the high pressure end 16.
  • the upper and lower shells 12 and 14 encircles two working chambers each consisting of two intersecting cylindrical borings in which are arranged a male rotor 26 and a female rotor 28.
  • the high pressure section 32 of the male rotor 26 comprises four helical convex lands 42 located mainly outside the pitch circle of the male rotor44 and the intermediate grooves 46.
  • the high pressure section 36 of the female rotor 28 comprises six helical concave lands located mainly inside the pitch circle 50 of the female rotor and the intermediate grooves 52.
  • the low pressure section of the male rotor 26 comprises likewise four helical concex lands 54 located mainly outside the pitch circle 44 of the male rotor and the intermediate grooves 56 of which each one, however, is provided with a recess 58 inside the pitch circle 44.
  • the low pressure section 34 of the female rotor 28 comprises six helical, substantially concave lands 60 located mainly inside the pitch circle 50 of the female rotor and provided with addendum portions '62 outside the pitch circle 50 and the intermediate grooves 64.
  • the cross sections of the male rotor 26 in the low pressure section 30 and the high pressure section 32 are identical except for the recesses 58 in the groove bottoms in the low pressure section.
  • the cross sections of the female rotor 28 in the low pressure section 34 and the high pressure section 36 are identical except for the addendum portions 62 on the rotor lands in the low pressure section.
  • the pitch angle is the same on both sections of the same rotor.
  • the male rotor is furthermore designed in such a way that in the low pressure section the wrap angle for each land is about 300 and the ratio between section length and section diameter is about 1.25 and in the high pressure section the wrap angle for each land is about 170 and the ratio between section length and section diameter is about 0.7.
  • the rotors are designed with land profiles even in the addendum portions and recesses substantially consisting of circular arcs which are equal on the male and the female rotors, except for a little difierence for providing a clearance of 0.080.11 mm. between the rotors in the low pressure section as well as in the high pressure'section, in order to prevent direct meshing between these and therefrom arising risk for seizing.
  • the male rotor is direct driven from a motor shaft
  • the female rotor in a manner known per se for compressors of the present type, is driven by the male rotor by means of an additional synchronizing gearing.
  • the compressor operates in the following manner.
  • Low pressure gas is suctioned-in through the low pressure inlet 18 and is being compressed to an intermediate pressure in the low pressure section 30, 34 and is blown out through the intermediate pressure outlet 20.
  • the gas is thereupon suctioned-in through the intermediate pressure inlet 22 in the high pressure section 32, 36 and is therein further compressed to high pressure gas before it is blown out through the high pressure outlet 24.
  • the size of the addendum portions 52 and the recesses 58 preferably is dimensioned in such a way that the two compressor stages operate with the same weight quantity of gas per time unit, so that no special accumulating vessel between the two pressure stages is necessary.
  • a builtup with an intermediate cooler between the two pressure stages may be advantageous in other forms of constructions. However, consideration must then be taken to such cooling-down at the dimensioning of the addendum portions and the recesses.
  • Rotor device operating with at least two pressure stages and provided with male and female rotors each one comprising male and female sections corresponding to the number of stages, the male sections being provided with helical convex lands and intermediate grooves and the female sections with helical concave lands and intermediate grooves, the cross sections of the male sections having a common basic profile and the cross sections of the female sections having a common basic profile, and in a lower pressure stage the lands of the female section being provided with addendum portions outside the profile of the lands of the adjacent female section, the grooves of the corresponding male section being provided with recesses in their bottoms corresponding to these addendum portions, similar sections of each pressure stage having the same land angle.
  • Rotor device having two stages, female section of the second higher pressure stage having a profile with lands substantially on its pitch circle and the male section having a profile with grooves adjacent the inside of its pitch circle.
  • Rotor device according to claim 1 the sections of each rotor having the same pitch diameter.
  • Rotor device each rotor comprising integral rotor sections.
  • Rotor device the male and female rotors run with a clearance therebetween, which clearance at full meshing between male lands and female grooves preferably is 0.08-0.11 mm. in both the high pressure and low pressure sections, and that the said rotors have a common synchronizing gear for their rotor sections.
  • a rotor device according to claim 1 the wrap angle for the lands of the low pressure stage of the male rotor lying within the limits 275-325, the wrap angle for the lands of the high pressure stage of the male rotor lying within the limits ISO-, the ratio between rotor length and rotor diameter in the low pressure stage lying between 1.1 and 1.4 and in the high pressure stage between 0.6 and 0.8.
  • a rotor device according to claim 1, the male sections having the same external diameter.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
US795534A 1958-02-27 1959-02-25 Rotor device Expired - Lifetime US2975963A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE193958 1958-02-27

Publications (1)

Publication Number Publication Date
US2975963A true US2975963A (en) 1961-03-21

Family

ID=20259105

Family Applications (1)

Application Number Title Priority Date Filing Date
US795534A Expired - Lifetime US2975963A (en) 1958-02-27 1959-02-25 Rotor device

Country Status (8)

Country Link
US (1) US2975963A (de)
AT (1) AT211945B (de)
BE (1) BE576046A (de)
CH (1) CH375474A (de)
DE (1) DE1109704B (de)
DK (1) DK98144C (de)
FR (1) FR1224330A (de)
GB (1) GB851262A (de)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3265293A (en) * 1959-09-08 1966-08-09 Svenska Rotor Maskiner Ab Vacuum pump of the screw rotor type and method for operating the same
US3265292A (en) * 1965-01-13 1966-08-09 Svenska Rotor Maskiner Ab Screw rotor machine
US3279682A (en) * 1963-02-23 1966-10-18 Howden James & Co Ltd Screw air compressors
US3283996A (en) * 1963-09-12 1966-11-08 Svenska Rotor Maskiner Ab Screw rotor machine for elastic working fluid
US3307777A (en) * 1963-12-23 1967-03-07 Svenska Rotor Maskiner Ab Screw rotor machine with an elastic working fluid
US3405604A (en) * 1965-05-14 1968-10-15 Lysholm Alf Method of driving a screw engine power unit and a power unit to be driven according to such method
US3577742A (en) * 1969-06-13 1971-05-04 Vilter Manufacturing Corp Refrigeration system having a screw compressor with an auxiliary high pressure suction inlet
US3807911A (en) * 1971-08-02 1974-04-30 Davey Compressor Co Multiple lead screw compressor
US4068984A (en) * 1974-12-03 1978-01-17 H & H Licensing Corporation Multi-stage screw-compressor with different tooth profiles
US4776779A (en) * 1984-03-21 1988-10-11 Wassan Pty Ltd. Fluid motor or pump
US4792294A (en) * 1986-04-11 1988-12-20 Mowli John C Two-stage screw auger pumping apparatus
US4944657A (en) * 1989-03-01 1990-07-31 Mowli John C Two-stage pumping apparatus with low shear first stage
US5267837A (en) * 1992-09-23 1993-12-07 Mowli John C Two-stage pumping apparatus with non-meshing first stage augers
US6257195B1 (en) 2000-02-14 2001-07-10 Arthur Vanmoor Internal combustion engine with substantially continuous fuel feed and power output
US6666666B1 (en) * 2002-05-28 2003-12-23 Denis Gilbert Multi-chamber positive displacement fluid device
US20090288648A1 (en) * 2008-05-21 2009-11-26 Gm Global Technology Operations, Inc. Superchargers with dual integral rotors
US20140283797A1 (en) * 2011-09-30 2014-09-25 Eaton Corporation Supercharger assembly with two rotor sets
US9534531B2 (en) 2011-09-30 2017-01-03 Eaton Corporation Supercharger assembly for regeneration of throttling losses and method of control
CN106704179A (zh) * 2017-03-09 2017-05-24 上海格什特螺杆科技有限公司 一种新型直连双螺杆压缩机
US9751411B2 (en) 2012-03-29 2017-09-05 Eaton Corporation Variable speed hybrid electric supercharger assembly and method of control of vehicle having same
US9856781B2 (en) 2011-09-30 2018-01-02 Eaton Corporation Supercharger assembly with independent superchargers and motor/generator
US10934951B2 (en) 2013-03-12 2021-03-02 Eaton Intelligent Power Limited Adaptive state of charge regulation and control of variable speed hybrid electric supercharger assembly for efficient vehicle operation
US11149732B2 (en) 2017-11-02 2021-10-19 Carrier Corporation Opposed screw compressor having non-interference system

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005005347A1 (de) * 2005-01-31 2006-10-26 Kayser, Albrecht, Dipl.-Ing. Rotorprofile für trockene Schraubenverdichter

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2659239A (en) * 1949-10-07 1953-11-17 Jarvis C Marble Independent synchronization
US2714857A (en) * 1951-09-04 1955-08-09 Roper Corp Geo D Gear pump

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1317370A (en) * 1918-04-15 1919-09-30 William S Holdaway Pump.
GB384355A (en) * 1931-08-05 1932-12-08 Frederick Charles Greenfield Improvements in and relating to rotary machines for the compression and propulsion of
DE723315C (de) * 1940-02-20 1942-08-03 Franz Burghauser Dipl Ing Hochdruckschraubenpumpe
DE903500C (de) * 1949-10-07 1954-02-08 Svenska Rotor Maskiner Ab Einrichtung zur Synchronisierung von Maschinenlaeufern
DE934605C (de) * 1952-04-19 1955-10-27 Svenska Rotor Maskiner Ab Drehkolbenmaschine

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2659239A (en) * 1949-10-07 1953-11-17 Jarvis C Marble Independent synchronization
US2714857A (en) * 1951-09-04 1955-08-09 Roper Corp Geo D Gear pump

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3265293A (en) * 1959-09-08 1966-08-09 Svenska Rotor Maskiner Ab Vacuum pump of the screw rotor type and method for operating the same
US3279682A (en) * 1963-02-23 1966-10-18 Howden James & Co Ltd Screw air compressors
US3283996A (en) * 1963-09-12 1966-11-08 Svenska Rotor Maskiner Ab Screw rotor machine for elastic working fluid
US3307777A (en) * 1963-12-23 1967-03-07 Svenska Rotor Maskiner Ab Screw rotor machine with an elastic working fluid
US3265292A (en) * 1965-01-13 1966-08-09 Svenska Rotor Maskiner Ab Screw rotor machine
US3405604A (en) * 1965-05-14 1968-10-15 Lysholm Alf Method of driving a screw engine power unit and a power unit to be driven according to such method
US3577742A (en) * 1969-06-13 1971-05-04 Vilter Manufacturing Corp Refrigeration system having a screw compressor with an auxiliary high pressure suction inlet
US3807911A (en) * 1971-08-02 1974-04-30 Davey Compressor Co Multiple lead screw compressor
US4068984A (en) * 1974-12-03 1978-01-17 H & H Licensing Corporation Multi-stage screw-compressor with different tooth profiles
US4776779A (en) * 1984-03-21 1988-10-11 Wassan Pty Ltd. Fluid motor or pump
US4792294A (en) * 1986-04-11 1988-12-20 Mowli John C Two-stage screw auger pumping apparatus
US4944657A (en) * 1989-03-01 1990-07-31 Mowli John C Two-stage pumping apparatus with low shear first stage
US5267837A (en) * 1992-09-23 1993-12-07 Mowli John C Two-stage pumping apparatus with non-meshing first stage augers
US6530365B2 (en) 1999-05-18 2003-03-11 Arthur Vanmoor Fluid displacement pump with backpressure stop
US6257195B1 (en) 2000-02-14 2001-07-10 Arthur Vanmoor Internal combustion engine with substantially continuous fuel feed and power output
US6666666B1 (en) * 2002-05-28 2003-12-23 Denis Gilbert Multi-chamber positive displacement fluid device
US20090288648A1 (en) * 2008-05-21 2009-11-26 Gm Global Technology Operations, Inc. Superchargers with dual integral rotors
US20140283797A1 (en) * 2011-09-30 2014-09-25 Eaton Corporation Supercharger assembly with two rotor sets
US9534531B2 (en) 2011-09-30 2017-01-03 Eaton Corporation Supercharger assembly for regeneration of throttling losses and method of control
US9534532B2 (en) * 2011-09-30 2017-01-03 Eaton Corporation Supercharger assembly with two rotor sets
US9856781B2 (en) 2011-09-30 2018-01-02 Eaton Corporation Supercharger assembly with independent superchargers and motor/generator
US9751411B2 (en) 2012-03-29 2017-09-05 Eaton Corporation Variable speed hybrid electric supercharger assembly and method of control of vehicle having same
US10934951B2 (en) 2013-03-12 2021-03-02 Eaton Intelligent Power Limited Adaptive state of charge regulation and control of variable speed hybrid electric supercharger assembly for efficient vehicle operation
CN106704179A (zh) * 2017-03-09 2017-05-24 上海格什特螺杆科技有限公司 一种新型直连双螺杆压缩机
US11149732B2 (en) 2017-11-02 2021-10-19 Carrier Corporation Opposed screw compressor having non-interference system

Also Published As

Publication number Publication date
CH375474A (de) 1964-02-29
DE1109704B (de) 1961-06-29
FR1224330A (fr) 1960-06-23
DK98144C (da) 1964-03-02
BE576046A (fr) 1959-06-15
AT211945B (de) 1960-11-10
GB851262A (en) 1960-10-12

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