US3280754A - Engine - Google Patents
Engine Download PDFInfo
- Publication number
- US3280754A US3280754A US344294A US34429464A US3280754A US 3280754 A US3280754 A US 3280754A US 344294 A US344294 A US 344294A US 34429464 A US34429464 A US 34429464A US 3280754 A US3280754 A US 3280754A
- Authority
- US
- United States
- Prior art keywords
- casing
- transverse end
- chamber
- end walls
- bias
- 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
Links
Images
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
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0003—Sealing arrangements in rotary-piston machines or pumps
- F04C15/0023—Axial sealings for working fluid
- F04C15/0026—Elements specially adapted for sealing of the lateral faces of intermeshing-engagement type machines or pumps, e.g. gear machines or pumps
Definitions
- the meshing gears are located in a working chamber whose opposite ends are closed by transverse end walls that are susbtantially parallel with and lie closely adjacent the side faces of the gears. These faces and walls are intended to define running seals at the opposite sides of the gears, but, since the Walls wear during operation, in time the running clearance increases to such an extent that leakage between the high and low pressure sides of the working chamber becomes intolerable. Because of this, it is common practice to use as one or both of the end walls a removable wear plate which is made of a bearing grade material and which is either deflected or moved into sealing engagement with the side faces of the gears by fluid under pressure.
- the object of this invention is to provide a gear engine incorporating an improved scheme of wear compensation which is less expensive than the removable wear plate approach just mentioned.
- the transverse end walls of the working chamber are defined by surfaces of two separable sections of the engine casing which are made from a bearing grade material.
- One or both of these sections contains an internal bias chamber which is spaced inward from the surface that constitutes a transverse end wall to define a deflectable portion of the casing section.
- the bias chamber is connected with a high pressure space of the engine so that, during operation, the deflectable portion is bowed outward into engagement with the side faces of the gears and maintains an effective seal between the high and low pressure sides of the working chamber.
- bias chamber may be formed at the time the casing section is cast, and since it is inherently sealed because it is contained wholly within the section, this approach to the wear compensation problem is less expensive than the prior approach mentioned earlier because it requires fewer parts and no complicated sealing means for the bias chamber.
- FIG. 1 is an axial sectional view of a gear pump of the externally meshing gear type incorporating the invention.
- FIG. 2 is a sectional view taken on line 22 of FIG. 1 showing the face of the casing cover.
- FIG. 3 is a sectional view taken on line 33 of FIG. 1 showing the face of the casing adapter.
- the improved gear pump comprises a casing having separable cover, housing and adapter sections 11, 12 and 13, respectively, which are aligned by two diametrically opposed locating pins 14 and which are held together by eight bolts 15 that pass through the cover and the housing and are threaded into bores formed in the adapter.
- Elastic rings '16 seal the ice joints between the housing section and the other two sections.
- the cover 11 is provided with inlet and discharge ports 17 and 18, respectively, which communicate with opposite sides of the working chamber enclosed by housing 12, and whose outline is indicated by phantom line 19 in FIG. 3, through shallow chambers 19 and 21, respectively, formed in its front face 22. Extending through the working chamber 19 are a pair of parallel shafts 23 and 24 which are 'journaled in bearings 25 located in cover 11 and adapter 13 and onto which are pressed a pair of meshing gears 26 and 27.
- the adapter 13 contains a cored bias chamber 28 of generally Y-shape having a central leg 28a which extends between the bearings 25 and a pair of branched legs 28b that flare outward in the direction of the inlet or low pressure side of the working chamber 19.
- This bias chamber 28 is spaced inward from the front face 29 of adapter 13 to define an intervening, deflectable adapter portion 31.
- Fluid under pressure is admitted to chamber 28 from the discharge side of the working chamber through a bore 32 that communicates with leg 28a, and this fluid develops a biasing force on deflectable portion 31 that bows it outward into sealing engagement with the side faces of the gears.
- portion 3-1 The magnitude of the deflection of portion 3-1 depends upon its thickness, the shape of and pressure supplied to bias chamber 28, and "the material used in adapter 13. Since portion 31 is flexed during operation, the configuration of chamber 28, and consequently of portion 31, depends upon the allowable fatigue limit of the material from which adapter 13 is made. Inasmuch as the faces 22 and 29 are bearing surfaces, it is essential that cover 11 and adapter 13 be made of bearing grade materials, such as aluminum, bronze or a suitable plastic.
- portion 31 In a typical pump, the deflection of portion 31 is on the order of 0.0006 inch, and, therefore, it is important that the pump be designed initially to have close running clearances between the side faces of the gears and the faces 22 and 29. In cases where a wide variation in initial clearance is expected, the cover may also be provided with a bias chamber 28. However, because of space limitation, this might necessitate locating the inlet and outlet ports 17 and 18 in the housing section 12.
- branched legs 28b of chamber 28 in the illustrated embodiment lie on the inlet or low pressure side of the pump, it will be apparent that they may be I placed on the opposite side. However, since the forces developed on face 29 by the pressure on the discharge side of the pump are much greater than those developed by the pressure on the inlet side, this rearrangement would necessitate using a chamber 28 of larger area in order to obtan tihe same deflection of portion 31. It should also be apparent that a bias chamber 28 could be provided in cover 11 in lieu of adapter 13.
- a gear engine of the type including a casing having separable sections and containing a working chamber whose opposite ends are closed by transverse end walls, one of said transverse end walls being a surface of a first one of the casing sections, and meshing gears located in the working chamber and having side faces substantially parallel with and closely adjacent the transverse end walls, the improvement which comprises (a) a bias chamber defined by a void in the material from which said first casing section is made, said bias chamber being spaced inward from the surface constituting said transverse end wall to define an intervening deflectable portion of said casing material that may be bowed outward into sealing engagement with the side faces of the gears; and
- a gear engine of the type including a casing having separable sections and containing high and low pressure ports and a working chamber whose opposite ends are closed by transverse end walls, one of said transverse end walls being a surface of a first one of the casing sections, a pair of externally meshing gears located in the working chamber and having side faces substantially parallel with and closely adjacent the transverse end walls, spaced parallel shafts carrying the gears and supported in said first and another casing sections, and means connecting the high and low pressure ports with high and low pressure regions, respectively, of the Working chamber located on opposite sides of a plane containing the shaft axes, the improvement which comprises (a) a bias chamber defined by a void in the material from which said first casing section is made, said bias chamber being spaced inward from the surface constituting said transverse end wall to define an intervening deflectable portion of said casing material that may be bowed outward into sealing engagement with the side faces of the gears,
- the bias chamber having a generally Y-shape with the central leg located between the shafts and the two branch legs flaring outward in the direction of one of the low and high pressure regions of the working chamber;
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
- Hydraulic Motors (AREA)
Description
Oct- 2 1966 w. E. MARIETTA ENGINE Filed Feb. 12, 1964 INVENTOR WALTER E. MARIETTA AT TORNEYS United States Patent ENGINE Walter E. Marietta, Kalamazoo, Mich., assignor to The New York Air Brake Company, a corporation of New Jersey Filed Feb. 12, 1964, Ser. No. 344,294 3 Claims. (Cl. 103-126) This invention relates to rotary pumps and motors, hereinafter referred to by the generic term engine, of the gear type.
In engines of this kind, the meshing gears are located in a working chamber whose opposite ends are closed by transverse end walls that are susbtantially parallel with and lie closely adjacent the side faces of the gears. These faces and walls are intended to define running seals at the opposite sides of the gears, but, since the Walls wear during operation, in time the running clearance increases to such an extent that leakage between the high and low pressure sides of the working chamber becomes intolerable. Because of this, it is common practice to use as one or both of the end walls a removable wear plate which is made of a bearing grade material and which is either deflected or moved into sealing engagement with the side faces of the gears by fluid under pressure. Since these plates are continuously biased toward the gears, this scheme automatically compensates for the increase in running clearance resulting from wear. While this approach to the wear problem is effective, it is expensive because it requires additional parts and also because of the rather elaborate means required to seal the pressure chambers at the rear faces of the Wear plates.
The object of this invention is to provide a gear engine incorporating an improved scheme of wear compensation which is less expensive than the removable wear plate approach just mentioned. According to this invention, the transverse end walls of the working chamber are defined by surfaces of two separable sections of the engine casing which are made from a bearing grade material. One or both of these sections contains an internal bias chamber which is spaced inward from the surface that constitutes a transverse end wall to define a deflectable portion of the casing section. The bias chamber is connected with a high pressure space of the engine so that, during operation, the deflectable portion is bowed outward into engagement with the side faces of the gears and maintains an effective seal between the high and low pressure sides of the working chamber. Since the bias chamber may be formed at the time the casing section is cast, and since it is inherently sealed because it is contained wholly within the section, this approach to the wear compensation problem is less expensive than the prior approach mentioned earlier because it requires fewer parts and no complicated sealing means for the bias chamber.
The preferred embodiment of the invention is described herein with reference to the accompanying drawing in which:
FIG. 1 is an axial sectional view of a gear pump of the externally meshing gear type incorporating the invention.
FIG. 2 is a sectional view taken on line 22 of FIG. 1 showing the face of the casing cover.
FIG. 3 is a sectional view taken on line 33 of FIG. 1 showing the face of the casing adapter.
As shown in the drawing, the improved gear pump comprises a casing having separable cover, housing and adapter sections 11, 12 and 13, respectively, which are aligned by two diametrically opposed locating pins 14 and which are held together by eight bolts 15 that pass through the cover and the housing and are threaded into bores formed in the adapter. Elastic rings '16 seal the ice joints between the housing section and the other two sections. The cover 11 is provided with inlet and discharge ports 17 and 18, respectively, which communicate with opposite sides of the working chamber enclosed by housing 12, and whose outline is indicated by phantom line 19 in FIG. 3, through shallow chambers 19 and 21, respectively, formed in its front face 22. Extending through the working chamber 19 are a pair of parallel shafts 23 and 24 which are 'journaled in bearings 25 located in cover 11 and adapter 13 and onto which are pressed a pair of meshing gears 26 and 27.
The adapter 13 contains a cored bias chamber 28 of generally Y-shape having a central leg 28a which extends between the bearings 25 and a pair of branched legs 28b that flare outward in the direction of the inlet or low pressure side of the working chamber 19. This bias chamber 28 is spaced inward from the front face 29 of adapter 13 to define an intervening, deflectable adapter portion 31. Fluid under pressure is admitted to chamber 28 from the discharge side of the working chamber through a bore 32 that communicates with leg 28a, and this fluid develops a biasing force on deflectable portion 31 that bows it outward into sealing engagement with the side faces of the gears. The magnitude of the deflection of portion 3-1 depends upon its thickness, the shape of and pressure supplied to bias chamber 28, and "the material used in adapter 13. Since portion 31 is flexed during operation, the configuration of chamber 28, and consequently of portion 31, depends upon the allowable fatigue limit of the material from which adapter 13 is made. Inasmuch as the faces 22 and 29 are bearing surfaces, it is essential that cover 11 and adapter 13 be made of bearing grade materials, such as aluminum, bronze or a suitable plastic.
In a typical pump, the deflection of portion 31 is on the order of 0.0006 inch, and, therefore, it is important that the pump be designed initially to have close running clearances between the side faces of the gears and the faces 22 and 29. In cases where a wide variation in initial clearance is expected, the cover may also be provided with a bias chamber 28. However, because of space limitation, this might necessitate locating the inlet and outlet ports 17 and 18 in the housing section 12.
Although the branched legs 28b of chamber 28 in the illustrated embodiment lie on the inlet or low pressure side of the pump, it will be apparent that they may be I placed on the opposite side. However, since the forces developed on face 29 by the pressure on the discharge side of the pump are much greater than those developed by the pressure on the inlet side, this rearrangement would necessitate using a chamber 28 of larger area in order to obtan tihe same deflection of portion 31. It should also be apparent that a bias chamber 28 could be provided in cover 11 in lieu of adapter 13.
As stated previously, the drawing and description relate only to the preferred embodiment of the invention. Since changes can be made in the structure of this embodiment without departing from the inventive concept the following claims should provide the sole measure of the scope of the invention.
What I claim is:
-1. In a gear engine of the type including a casing having separable sections and containing a working chamber whose opposite ends are closed by transverse end walls, one of said transverse end walls being a surface of a first one of the casing sections, and meshing gears located in the working chamber and having side faces substantially parallel with and closely adjacent the transverse end walls, the improvement which comprises (a) a bias chamber defined by a void in the material from which said first casing section is made, said bias chamber being spaced inward from the surface constituting said transverse end wall to define an intervening deflectable portion of said casing material that may be bowed outward into sealing engagement with the side faces of the gears; and
(b) means for transmitting to the bias chamber fluid from a high pressure space of the engine.
2. In a gear engine of the type including a casing having separable sections and containing high and low pressure ports and a working chamber whose opposite ends are closed by transverse end walls, one of said transverse end walls being a surface of a first one of the casing sections, a pair of externally meshing gears located in the working chamber and having side faces substantially parallel with and closely adjacent the transverse end walls, spaced parallel shafts carrying the gears and supported in said first and another casing sections, and means connecting the high and low pressure ports with high and low pressure regions, respectively, of the Working chamber located on opposite sides of a plane containing the shaft axes, the improvement which comprises (a) a bias chamber defined by a void in the material from which said first casing section is made, said bias chamber being spaced inward from the surface constituting said transverse end wall to define an intervening deflectable portion of said casing material that may be bowed outward into sealing engagement with the side faces of the gears,
(b) the bias chamber having a generally Y-shape with the central leg located between the shafts and the two branch legs flaring outward in the direction of one of the low and high pressure regions of the working chamber; and
(c) an opening in the first casing section extending into the bias chamber from the high pressure region.
3. The improvement defined in claim 2 in which (a) the two branch legs of the bias chamber extend in the direction of the low pressure region;
(b) a portion of the central leg of the bias chamber is on the high pressure side of said plane containing the shaft axes; and
(c) said opening enters that portion of the bias chamber located on the high pressure side of said plane.
References Cited by the Examiner UNITED STATES PATENTS 164,147 6/1875 Conver 103126 2,176,322 10/1939 Barrett 1O3126 2,702,509 2/1955 Garnier 103126 2,742,862 4/1956 Banker 103-126 2,809,592 10/1957 Miller et al. 10 3126 2,824,524 2/1958 Banker 103-126 3,101,673 8/196-3 Clark et a1. 103--126 MARK NEWMAN, Primary Examiner.
WILBUR J. GOODLIN, Examiner.
Claims (1)
1. IN A GEAR ENGINE OF THE TYPE INCLUDING A CASING HAVING SEPARABLE SECTIONS AND CONTAINING A WORKING CHAMBER WHOSE OPPOSITE ENDS ARE CLOSED BY TRANSVERSE END WALLS, ONE OF SAID TRANSVERSE END WALLS BEING A SURFACE OF A FIRST ONE OF THE CASING SECTIONS, AND MESHING GEARS LOCATED IN THE WORKING CHAMBER AND HAVING SIDE FACES SUBSTANTIALLY PARALLEL WITH AND CLOSELY ADJACENT THE TRANSVERSE END WALLS, THE IMPROVEMENT WHICH COMPRISES (A) A BIAS CHAMBER DEFINED BY A VOID IN THE MATERIAL FROM WHICH SAID FIRST CASING SECTION IS MADE, SAID BIAS CHAMBER BEING SPACED INWARD FROM THE SURFACE CONSTITUTING SAID TRANSVERSE END WALL TO DEFINE AN INTERVENTING DEFLECTABLE PORTION OF SAID CASING MATERIAL THAT MAY BE BOWED OUTWARD INTO SEALING ENGAGEMENT WITH THE SIDE FACES OF THE GEARS; AND (B) MEANS FOR TRANSMITTING TO THE BIAS CHAMBER FLUID FROM A HIGH PRESSURE SPACE OF THE ENGINE.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US344294A US3280754A (en) | 1964-02-12 | 1964-02-12 | Engine |
GB51534/64A GB1029519A (en) | 1964-02-12 | 1964-12-18 | Improvements in and relating to gear pumps and motors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US344294A US3280754A (en) | 1964-02-12 | 1964-02-12 | Engine |
Publications (1)
Publication Number | Publication Date |
---|---|
US3280754A true US3280754A (en) | 1966-10-25 |
Family
ID=23349906
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US344294A Expired - Lifetime US3280754A (en) | 1964-02-12 | 1964-02-12 | Engine |
Country Status (2)
Country | Link |
---|---|
US (1) | US3280754A (en) |
GB (1) | GB1029519A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3376824A (en) * | 1965-07-01 | 1968-04-09 | Turolla Marco | Gear pump |
US3404634A (en) * | 1966-09-16 | 1968-10-08 | Eaton Yale & Towne | Pump |
US5222886A (en) * | 1991-03-20 | 1993-06-29 | Mannesmann Rexroth Gmbh | Cheek plate for a vane pump |
US20050106055A1 (en) * | 2003-11-15 | 2005-05-19 | Lipscombe Brian R. | Rotary positive displacement hydraulic machines |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US164147A (en) * | 1875-06-08 | Improvement in pumps | ||
US2176322A (en) * | 1937-06-28 | 1939-10-17 | Gar Wood Ind Inc | Fluid pump |
US2702509A (en) * | 1951-04-06 | 1955-02-22 | Air Equipment | Rotary pump |
US2742862A (en) * | 1953-03-09 | 1956-04-24 | New Prod Corp | Fluid pump |
US2809592A (en) * | 1954-01-13 | 1957-10-15 | Cessna Aircraft Co | Rotary pump or motor |
US2824524A (en) * | 1955-01-18 | 1958-02-25 | New Prod Corp | Gear pump with externally adjustable shroud |
US3101673A (en) * | 1961-06-16 | 1963-08-27 | Thompson Ramo Wooldridge Inc | Implement and power steering pump |
-
1964
- 1964-02-12 US US344294A patent/US3280754A/en not_active Expired - Lifetime
- 1964-12-18 GB GB51534/64A patent/GB1029519A/en not_active Expired
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US164147A (en) * | 1875-06-08 | Improvement in pumps | ||
US2176322A (en) * | 1937-06-28 | 1939-10-17 | Gar Wood Ind Inc | Fluid pump |
US2702509A (en) * | 1951-04-06 | 1955-02-22 | Air Equipment | Rotary pump |
US2742862A (en) * | 1953-03-09 | 1956-04-24 | New Prod Corp | Fluid pump |
US2809592A (en) * | 1954-01-13 | 1957-10-15 | Cessna Aircraft Co | Rotary pump or motor |
US2824524A (en) * | 1955-01-18 | 1958-02-25 | New Prod Corp | Gear pump with externally adjustable shroud |
US3101673A (en) * | 1961-06-16 | 1963-08-27 | Thompson Ramo Wooldridge Inc | Implement and power steering pump |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3376824A (en) * | 1965-07-01 | 1968-04-09 | Turolla Marco | Gear pump |
US3404634A (en) * | 1966-09-16 | 1968-10-08 | Eaton Yale & Towne | Pump |
US5222886A (en) * | 1991-03-20 | 1993-06-29 | Mannesmann Rexroth Gmbh | Cheek plate for a vane pump |
US20050106055A1 (en) * | 2003-11-15 | 2005-05-19 | Lipscombe Brian R. | Rotary positive displacement hydraulic machines |
US7264455B2 (en) * | 2003-11-15 | 2007-09-04 | Brian Robert Lipscombe | Rotary positive displacement hydraulic machines |
Also Published As
Publication number | Publication date |
---|---|
GB1029519A (en) | 1966-05-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3961872A (en) | Gear machine with fluid-biased end face sealing elements | |
US2932254A (en) | Gear pump | |
US3528756A (en) | Pressure loaded pump | |
US2641192A (en) | Gear pump | |
US2842066A (en) | Gear pump | |
US2824522A (en) | Pump, pressure loaded with offset loading | |
EP0349574B1 (en) | Screw rotor machine | |
US3131643A (en) | Engine | |
US3482524A (en) | Pump or motor | |
US2923249A (en) | Gear pump with pressure loaded end plate and with pressure loaded peripheral tooth sealing means | |
US2965040A (en) | Gear pumps | |
US3902827A (en) | Screw compressor | |
US3473476A (en) | Gear pump seal | |
US3280754A (en) | Engine | |
US3043230A (en) | High pressure gear pump | |
US3416459A (en) | Rotary pump or motor | |
US3891360A (en) | Gear machine with axially movable end wall seal | |
US3083645A (en) | Gear pump or the like | |
US3161349A (en) | Thrust balancing | |
US4177025A (en) | High-pressure rotary fluid-displacing machine | |
US2471149A (en) | Rotary gear pump | |
US2864315A (en) | Liquid pump | |
GB1079127A (en) | Rotary piston machines | |
US3068804A (en) | Pressure loaded pump seal | |
US2823615A (en) | Pump with pressure loaded bushings |