GB2116634A - Rotary positive-displacement fluid-machines - Google Patents

Rotary positive-displacement fluid-machines Download PDF

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Publication number
GB2116634A
GB2116634A GB08305332A GB8305332A GB2116634A GB 2116634 A GB2116634 A GB 2116634A GB 08305332 A GB08305332 A GB 08305332A GB 8305332 A GB8305332 A GB 8305332A GB 2116634 A GB2116634 A GB 2116634A
Authority
GB
United Kingdom
Prior art keywords
chamber
rotors
compressor
support structure
shaft
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.)
Withdrawn
Application number
GB08305332A
Other versions
GB8305332D0 (en
Inventor
Pier Luigi Scapecchi
Giorgio Gatti
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.)
Fiat Auto SpA
Original Assignee
Fiat Auto SpA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fiat Auto SpA filed Critical Fiat Auto SpA
Publication of GB8305332D0 publication Critical patent/GB8305332D0/en
Publication of GB2116634A publication Critical patent/GB2116634A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • F04C27/008Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids for other than working fluid, i.e. the sealing arrangements are not between working chambers of the machine
    • F04C27/009Shaft sealings specially adapted for pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/002Sealings comprising at least two sealings in succession
    • F16J15/004Sealings comprising at least two sealings in succession forming of recuperation chamber for the leaking fluid

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Supercharger (AREA)

Abstract

In a Roots-type compressor the shafts 8, 9 of the rotors are supported by "rolling" bearings 10 and a lipped sealing-gland 14 associated with each bearing separates the bearing lubricating environment from an annular chamber 15, which is adjacent the rotor chamber 7 and substantially isolated therefrom by a labyrinth seal 16. The annular chamber communicates with the atmosphere through a hole (18), Fig.2 (not shown), so as to prevent the lip of the sealing gland from being subjected to excessive loads owing to negative or positive pressures transmitted from the rotor chamber past the labyrinth seal. <IMAGE>

Description

SPECIFICATION Rotary volumetric compressor of the Roots type The present invention relates to a rotary volumetric compressor of the Roots type, comprising a support structure, two rotors mounted rotatably in a chamber within the support structure, and a pair of shafts connected to the two rotors and having their ends mounted rotatably in the support structure by means of rolling bearings, in which a lipped sealing gland is provided at each end of the shafts to separate the lubricating environment of the bearing from a respective annular chamber which is adjacent the chamber of the two rotors and is isolated therefrom by a labyrinth seal.
The object of the present invention is to prevent the lips of the sealing glands from being subjected to excessive loads (which would reduce the effectiveness and/or the lifetime of the glands), as a result of the pressures or pressure drops which occur in the rotor chamber during operation of the compressor.
In orderto achieve this object, the invention provides a compressor of the aforesaid type, characterised in that the annular chamber adjacent each lipped sealing gland communicates with a respective hole formed through the support structure to the exterior.
The present invention will now be described with reference to the appended drawings, provided purely by way of non-limiting example, in which: Figure lisa partially sectioned view of a com pressor according to the present invention, and Figure 2 is a section taken on the line ll-ll of Figure 1.
In the drawings, there is shown a rotary volumetric compressor of the Roots type, generally indicated 1, usable, for example, for supercharging an internal combustion engine.
The compressor 1 comprises a support structure 2 including an externally-finned casing 3 closed at one end by a cover 4 and at the opposite end by a plate 5 and a cover 6.
The casing 3 has an internal chamber 7 housing the two rotors (not visible in the drawings) of the compressor.
The two rotors of the compressor are connected for rotation with two shafts 8,9 the ends of which are mounted rotatably within the plate 5 and the cover 4, respectively, by means of rolling bearings 10.
The shaft 8 has one end 8a projecting from the cover 6, onto which is keyed a gear wheel 11 for connection by a cogged belt to the driving shaft or cam shaft of the engine with which the compressor is associated.
The drive is transmitted from the shaft 8 to the shaft 9 through the meshing of two gear wheels 12, 13 connected for rotation with the shafts.
With each rolling bearing 10 is associated a lipped sealing gland 14 which separates the lubricating environment of the respective bearing from an annular chamber 15 adjacent the chamber 7 of the two rotors.
Each annular chamber 15 is isolated from the chamber 7 of the rotors by a double labyrinth seal 16.
In the case of the two sealing glands 14 mounted in the plate 5, each double labyrinth seal 16 is formed between the outer surface of a tubular spacer 17 (interposed coaxially of the respective shaft between the bearing and the rotor) and the surface of the hole in the plate 5 in which the spacer 17 is mounted. In the case of the sealing glands 14 mounted in the cover 4, however, each labyrinth seal 16 is formed between the outer surface of the respective shaft and the surface of the hole in the cover 4 in which the shaft is mounted.
In order to prevent the pressures or pressure drops existing in the rotor chamber 7 of the com pressorfrom being transmitted through the labyrinth seal 16 to the annular chambers 15, thereby subjecting the lips of the sealing glands 14 to excessive loads which would render the seals unreliable, each annular chamber 15 (see Figure 2) communicates with a hole 18 formed through the support structure (or, more precisely, the plate 5 or the cover 4) to open onto the outer surface 19 of the compressor.
1. Rotary volumetric compressor of the Roots type, comprising a support structure, two rotors mounted rotatably in a chamber within the support structure, and a pair of shafts connected to the two rotors and having their ends mounted rotatably in the support structure by means of rolling bearings, in which a lipped sealing gland is provided at each end of the shafts to separate the lubricating environment of the bearing from a respective annular chamber which is adjacent the (Ç) chamber of the two rotors and is isolated therefrom by means of a labyrinth seal, characterised in that the annular chamber adjacent each lipped sealing gland communicates with a respective hole formed through the support structure to the exterior.
2. A rotary volumetric compressor as constructed and arranged substantially as hereinbefore described and as shown in the figures of the accompanying drawing.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (2)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Rotary volumetric compressor of the Roots type The present invention relates to a rotary volumetric compressor of the Roots type, comprising a support structure, two rotors mounted rotatably in a chamber within the support structure, and a pair of shafts connected to the two rotors and having their ends mounted rotatably in the support structure by means of rolling bearings, in which a lipped sealing gland is provided at each end of the shafts to separate the lubricating environment of the bearing from a respective annular chamber which is adjacent the chamber of the two rotors and is isolated therefrom by a labyrinth seal. The object of the present invention is to prevent the lips of the sealing glands from being subjected to excessive loads (which would reduce the effectiveness and/or the lifetime of the glands), as a result of the pressures or pressure drops which occur in the rotor chamber during operation of the compressor. In orderto achieve this object, the invention provides a compressor of the aforesaid type, characterised in that the annular chamber adjacent each lipped sealing gland communicates with a respective hole formed through the support structure to the exterior. The present invention will now be described with reference to the appended drawings, provided purely by way of non-limiting example, in which: Figure lisa partially sectioned view of a com pressor according to the present invention, and Figure 2 is a section taken on the line ll-ll of Figure 1. In the drawings, there is shown a rotary volumetric compressor of the Roots type, generally indicated 1, usable, for example, for supercharging an internal combustion engine. The compressor 1 comprises a support structure 2 including an externally-finned casing 3 closed at one end by a cover 4 and at the opposite end by a plate 5 and a cover 6. The casing 3 has an internal chamber 7 housing the two rotors (not visible in the drawings) of the compressor. The two rotors of the compressor are connected for rotation with two shafts 8,9 the ends of which are mounted rotatably within the plate 5 and the cover 4, respectively, by means of rolling bearings 10. The shaft 8 has one end 8a projecting from the cover 6, onto which is keyed a gear wheel 11 for connection by a cogged belt to the driving shaft or cam shaft of the engine with which the compressor is associated. The drive is transmitted from the shaft 8 to the shaft 9 through the meshing of two gear wheels 12, 13 connected for rotation with the shafts. With each rolling bearing 10 is associated a lipped sealing gland 14 which separates the lubricating environment of the respective bearing from an annular chamber 15 adjacent the chamber 7 of the two rotors. Each annular chamber 15 is isolated from the chamber 7 of the rotors by a double labyrinth seal 16. In the case of the two sealing glands 14 mounted in the plate 5, each double labyrinth seal 16 is formed between the outer surface of a tubular spacer 17 (interposed coaxially of the respective shaft between the bearing and the rotor) and the surface of the hole in the plate 5 in which the spacer 17 is mounted. In the case of the sealing glands 14 mounted in the cover 4, however, each labyrinth seal 16 is formed between the outer surface of the respective shaft and the surface of the hole in the cover 4 in which the shaft is mounted. In order to prevent the pressures or pressure drops existing in the rotor chamber 7 of the com pressorfrom being transmitted through the labyrinth seal 16 to the annular chambers 15, thereby subjecting the lips of the sealing glands 14 to excessive loads which would render the seals unreliable, each annular chamber 15 (see Figure 2) communicates with a hole 18 formed through the support structure (or, more precisely, the plate 5 or the cover 4) to open onto the outer surface 19 of the compressor. CLAIMS
1. Rotary volumetric compressor of the Roots type, comprising a support structure, two rotors mounted rotatably in a chamber within the support structure, and a pair of shafts connected to the two rotors and having their ends mounted rotatably in the support structure by means of rolling bearings, in which a lipped sealing gland is provided at each end of the shafts to separate the lubricating environment of the bearing from a respective annular chamber which is adjacent the (Ç) chamber of the two rotors and is isolated therefrom by means of a labyrinth seal, characterised in that the annular chamber adjacent each lipped sealing gland communicates with a respective hole formed through the support structure to the exterior.
2. A rotary volumetric compressor as constructed and arranged substantially as hereinbefore described and as shown in the figures of the accompanying drawing.
GB08305332A 1982-03-10 1983-02-25 Rotary positive-displacement fluid-machines Withdrawn GB2116634A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT67296/82A IT1155126B (en) 1982-03-10 1982-03-10 ROOTS TYPE ROTARY VOLUMETRIC COMPRESSOR

Publications (2)

Publication Number Publication Date
GB8305332D0 GB8305332D0 (en) 1983-03-30
GB2116634A true GB2116634A (en) 1983-09-28

Family

ID=11301234

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08305332A Withdrawn GB2116634A (en) 1982-03-10 1983-02-25 Rotary positive-displacement fluid-machines

Country Status (4)

Country Link
DE (2) DE3308363A1 (en)
FR (1) FR2523223A1 (en)
GB (1) GB2116634A (en)
IT (1) IT1155126B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4813857A (en) * 1986-03-31 1989-03-21 Aisin Seiki Kabushiki Kaisha Roots blower
EP0320956A2 (en) * 1987-12-18 1989-06-21 Hitachi, Ltd. Screw type vacuum pump
FR2638788A1 (en) * 1988-11-07 1990-05-11 Cit Alcatel MULTI-STAGE ROOTS TYPE VACUUM PUMP
GB2247047A (en) * 1990-07-17 1992-02-19 Bombas Stork S A Shaft sealing in lobe rotor pump
FR2774133A1 (en) * 1998-01-28 1999-07-30 Luk Fahrzeug Hydraulik Pump for hydraulic oil
EP0959251A1 (en) * 1998-05-18 1999-11-24 SGI-PROZESS-TECHNIK GmbH Rotary gear compressor and method for its operation
US6659227B2 (en) 2001-05-08 2003-12-09 Kabushiki Kaisha Toyota Jidoshokki Oil leak prevention structure for vacuum pump
CN104100524A (en) * 2014-07-31 2014-10-15 山东省章丘鼓风机股份有限公司 Roots blower with combined sealing structure

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3619645A1 (en) * 1986-05-08 1987-11-12 Wankel Gmbh Bearing arrangement for a rotary piston ventilator with an external axis
DE3725902A1 (en) * 1987-08-05 1989-02-16 Bayer Ag MIXTURES OF CHLOROPRENE POLYMERS AND THEIR PREPARATION

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB559226A (en) * 1942-08-07 1944-02-09 Douglas Rudolf Pobjoy Improvements in and relating to rotary pumps
GB559729A (en) * 1942-09-14 1944-03-02 Frederick George Horstmann Improvements in and relating to rotary pumps

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2128928A5 (en) * 1971-03-09 1972-10-27 Commissariat Energie Atomique
FR2214337A5 (en) * 1973-01-11 1974-08-09 Hydroperfect Int
GB1484994A (en) * 1973-09-03 1977-09-08 Svenska Rotor Maskiner Ab Shaft seal system for screw compressors

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB559226A (en) * 1942-08-07 1944-02-09 Douglas Rudolf Pobjoy Improvements in and relating to rotary pumps
GB559729A (en) * 1942-09-14 1944-03-02 Frederick George Horstmann Improvements in and relating to rotary pumps

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4813857A (en) * 1986-03-31 1989-03-21 Aisin Seiki Kabushiki Kaisha Roots blower
US4984974A (en) * 1987-12-18 1991-01-15 Hitachi, Ltd. Screw type vacuum pump with introduced inert gas
EP0320956A2 (en) * 1987-12-18 1989-06-21 Hitachi, Ltd. Screw type vacuum pump
EP0320956A3 (en) * 1987-12-18 1990-02-21 Hitachi, Ltd. Screw type vacuum pump
US4990069A (en) * 1988-11-07 1991-02-05 Societe Anonyme Dite: Alcatel Cit Multi-stage roots vacuum pump with sealing module
EP0368122A1 (en) * 1988-11-07 1990-05-16 Alcatel Cit Multistage Roots vacuum pump
FR2638788A1 (en) * 1988-11-07 1990-05-11 Cit Alcatel MULTI-STAGE ROOTS TYPE VACUUM PUMP
GB2247047A (en) * 1990-07-17 1992-02-19 Bombas Stork S A Shaft sealing in lobe rotor pump
GB2247047B (en) * 1990-07-17 1994-05-04 Bombas Stork S A Lobe rotor pump
FR2774133A1 (en) * 1998-01-28 1999-07-30 Luk Fahrzeug Hydraulik Pump for hydraulic oil
EP0959251A1 (en) * 1998-05-18 1999-11-24 SGI-PROZESS-TECHNIK GmbH Rotary gear compressor and method for its operation
US6659227B2 (en) 2001-05-08 2003-12-09 Kabushiki Kaisha Toyota Jidoshokki Oil leak prevention structure for vacuum pump
CN104100524A (en) * 2014-07-31 2014-10-15 山东省章丘鼓风机股份有限公司 Roots blower with combined sealing structure

Also Published As

Publication number Publication date
FR2523223A1 (en) 1983-09-16
DE8306813U1 (en) 1985-01-17
IT1155126B (en) 1987-01-21
IT8267296A0 (en) 1982-03-10
GB8305332D0 (en) 1983-03-30
DE3308363A1 (en) 1983-09-29

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)