[go: up one dir, main page]

US3034451A - Pintle port construction for pumps - Google Patents

Pintle port construction for pumps Download PDF

Info

Publication number
US3034451A
US3034451A US808443A US80844359A US3034451A US 3034451 A US3034451 A US 3034451A US 808443 A US808443 A US 808443A US 80844359 A US80844359 A US 80844359A US 3034451 A US3034451 A US 3034451A
Authority
US
United States
Prior art keywords
pintle
rotor
port
adjacent
pumps
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
US808443A
Inventor
Richard N Sullivan
Raymond P Lambeck
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.)
RTX Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Priority to US808443A priority Critical patent/US3034451A/en
Application granted granted Critical
Publication of US3034451A publication Critical patent/US3034451A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/04Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B1/10Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary
    • F04B1/107Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders
    • F04B1/1071Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders with rotary cylinder blocks
    • F04B1/1074Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders with rotary cylinder blocks with two or more serially arranged radial piston-cylinder units
    • F04B1/1077Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement the cylinders being movable, e.g. rotary with actuating or actuated elements at the outer ends of the cylinders with rotary cylinder blocks with two or more serially arranged radial piston-cylinder units located side-by-side
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/04Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B1/0404Details or component parts
    • F04B1/0452Distribution members, e.g. valves
    • F04B1/0456Cylindrical

Definitions

  • FIG. l is a schematic showing of a pump pintle of the prior art construction
  • FIG. 1A is a diagrammatic illustration of the pressure pattern of a pintle such as shown in FIG. l;
  • FIG. 2 is a schematic illustration of a pump rotor and pintle showing the improved port construction of this invention
  • FIG. 2A is a diagrammatic illustration of the pressure pattern of a pintle such as shown in FIG. 2;
  • FIG. 3 is a side elevation in partial cross section of a pump embodying the principles of this invention.
  • the leakage pressure will vary between 3000 p.s.i. and zero in very nearly a linear fashion across the bearing surface and will average about 1500 p.s.i. This will create a bearing load of about 1500 p.s.i. on the opposite side of the pintle.
  • this bearing load may be- 3,034,451 Patented May 15, 1962 come 2000 p.s.i. due to a narrower bearing surface at the inlet side of the pintle than is presented at the outlet side and due possibility to a diierence between the projected areas of the pintle outlet and the pistons which are under pressure.
  • a wide (axial dimension) pintle outlet port of the type described above also tends to weaken the pintle in a critical area leading to high stresses and high pintle dellections which tend to cause binding between the pintle and rotor.
  • a pintle 12 is illustrated as being surrounded by a rotor 14 which may have a bearing sleeve 16 therebetween.
  • the outlet port 18 is approximately equal to the area of the pistons 20, 22, 24 which are subject to outlet pressure in each of the three rows.
  • the piston 22 is shown above the center line in the cross section of FIG. 1 but actually there is a piston adjacent to the pistons 20, 24 but staggered with respect thereto and hence not seen in a vertical section.
  • the pressure pattern for the outlet port approximately equals the pattern 32 for the total effective cylinder area so that these pressures balance out.
  • leakage pressure patterns 34 and 36 respectively which impose an' eccentric load between the pintle and the rotor.
  • FIG. 2 it is the purpose of the present invention to have the cylinders and pistons connected in groups of three to a single row of ports approximately in the center of the rotor. Both the inlet port 40 and the outlet port 42 are made only long enough along the axis to permit proper port opening for the single row of cylinders 44. As mentioned previously in connection with FIG. 1 the cylinder 44 is shown above the center line but a similar cylinder in the same row will be located adjacent and substantially between the cylinders 46, 48 shown below the center line according to the construction of this invention.
  • This projected area of the pintle outlet port 42 is less than the projected areas of the adjacent cylinders of adjacent rows.
  • the pressure pattern for the port 42 is indicated along the line 50 while the pressure pattern for the cylinders is indicated as extending along the line 52.
  • This force is then in a direction that tends to counterbalance the leakage pressure force indicated by the patterns 56 andlSS between the rotor and pintle and therefore reduces the bearing pressure at the top of the pintle.
  • FIG. 3 A typical embodiment of this invention is better shown in FIG. 3.
  • a pump casing 70 is illustrated as surrounding ya track ring 72 which includes an inner ring 74 engaging the outer ends of a plurality of lrows of pistons 76, 78 and 80 carried by a rotor 82.
  • a central fixed pintle 84 is tixedly mounted in the casing 70 and carries inlet passage 86 and outlet passage 88.
  • the rotor 82 may be suitably driven yby a gear 90 through a suitable grouping 92 which may be of the type shown and described in the labove-referred-to patent.
  • a track ring 72 may be pivotally mounted for movement about a pivot 94 lby a suitable stroke control device as also shown in the above-referred-to patent.
  • the outlet port 96 and the inlet port 98 are substantially of the same projected area or axial length of the area of the cylinder 100 and its corresponding piston 7S.
  • the pistons 76 ⁇ and 80 have their corresponding pressure areas 102 and 104 connected to the adjacent cylinder and the outlet port 96 by means of recessed passages 106 and 108 respectively.
  • the inner end 1'10 of the wall 112 of the x rotor is spaced away from the pintle axis a distance farther than the remaining inner wall portions 116, 118 of the rotor on either side ot the wall portion 112 and the adjacent pistons 76 and 80.
  • the uid under pressure from the chambers 102and 104 can passthrough the passages 1061 and 108 respectively tothe adjacent cylinder of the central row and then ⁇ out through the outlet port 96.
  • a rotorrotatably supported in said casing having three rowsof cylinders each spacedyapart along the axis of rotation of the rotor, said cylinders of said rows being arranged such that the adjacent cylinders alongY saidVV axis are arranged in staggered groups,
  • inlet and outlet passageways including inlet and outlet ports in said pintle communicating in timed relation-with said cylinders, said sleeve having a single row of ports registering with the center row of cylinders and intermittedly with said outlet ports, the projected area of pintle outlet port being less than the projected area of the adjacent cylinders of an adjacent group,

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Reciprocating Pumps (AREA)

Description

2 Sheets-Sheec l FIG 2 F- ICLA R. N. SULLIVAN I'AL PINTLE PORT CONSTRUCTION FOR PUMPS 5f/Maf afssz//Pf ,O4/75%# //wzf Mawr/0 mmf/'paw fffz/f May 15, 1962 Filed April 23, 1959 F- l G l F-l G IA D/PIP;
INVENTORS RAYMOND P. LAMBECK RICHARD N. SULLIVAN ,M-Wpef BY/ ATTORNEY May 15, 1962 R. N. SULLIVAN Erm. I 3,034,451
PINTLE PORT CONSTRUCTION FOR PUMPS Filed April 23, '1959 2 sheets-sheet 2 /N VE N TORS RVMOND F. LAMBECK RICHARD N SULL/VAN United States Patent 3,034,451 PINTLE PORT CONSTRUCTION FOR PUMPS Richard N. Sullivan, Bloomfield, and Raymond P. Lambeck, Simsbury, Conn., assignors to United Aircraft Corporation, East Hartford, Conn., a corporation of Delaware Filed Ap 23, 1959, Ser. No. 808,443 1 Claim. (Cl. 103-161) This invention relates to rotary piston hydraulic pumps and more particularly to the pintle and port construction for such pumps.
The normal design practice for radial piston pumps is to provide a separate port in the rotor for each row of pistons and to make the outlet port in the pintle long enough in the axial direction to span the piston ports in the rotor. This results in a projected pintle port area (projected in the direction away from the pintle pressure port toward the adjacent piston) which is approximately equal to the projected area of the pistons that are under pressure. When these projected areas, i.e., the port and the piston areas, are equal there is no tendency for the rotor to be forced eccentric on the pintle by the pressure in the outlet port.l This statement holds true if leakage conditions `were perfect.
There is, however, a leakage pressure between the pintle and the rotor in the bearing areas adjacent to the outlet port on either side thereof. As one moves further from the port along the pintle the leakage tends to drop to zero. However, this pressure does force the rotor to an eccentric position and creates a bearing pressure on the opposite side of the pintle adjacent to the inlet port.
It is therefore an object of this invention to provide a pintle-port construction for rotary piston hydraulic pumps and the like wherein the outlet and inlet ports in the pintle are substantially smaller in projected area than the projected area of the pistons under pressure at any particular time.
It is a further object of this invention to provide a multiple row radial piston pump wherein the outlet port is connected to only one of the rows of pistons with the other adjacent rows being connected to said one row by means of passages externally of the pintle.
These and other objects of this invention will become readily apparent Ifrom the following detailed description of the drawing in which:
FIG. l is a schematic showing of a pump pintle of the prior art construction;
FIG. 1A is a diagrammatic illustration of the pressure pattern of a pintle such as shown in FIG. l;
FIG. 2 is a schematic illustration of a pump rotor and pintle showing the improved port construction of this invention;
FIG. 2A is a diagrammatic illustration of the pressure pattern of a pintle such as shown in FIG. 2; and
FIG. 3 is a side elevation in partial cross section of a pump embodying the principles of this invention.
In describing the prior art and the principles of this invention with respect to the drawing a conventional three-row piston rotor construction will be referred to. As desecribed herein, the adjacent pistons of adjacent rows are slightly staggered so as to permit shortening of the rotor along its axis. However, the adjacent pistons of adjacent rows may be in-line as clearly shown in Patent No. 2,673,526 issued to R. F. Horton on March 20, 1954.
In a pump operating, at for example, 3000 p.s.i., the leakage pressure will vary between 3000 p.s.i. and zero in very nearly a linear fashion across the bearing surface and will average about 1500 p.s.i. This will create a bearing load of about 1500 p.s.i. on the opposite side of the pintle. In actual designs this bearing load may be- 3,034,451 Patented May 15, 1962 come 2000 p.s.i. due to a narrower bearing surface at the inlet side of the pintle than is presented at the outlet side and due possibility to a diierence between the projected areas of the pintle outlet and the pistons which are under pressure. A wide (axial dimension) pintle outlet port of the type described above also tends to weaken the pintle in a critical area leading to high stresses and high pintle dellections which tend to cause binding between the pintle and rotor.
As seen in FIG. 1, a pintle 12 is illustrated as being surrounded by a rotor 14 which may have a bearing sleeve 16 therebetween. In this construction the outlet port 18 is approximately equal to the area of the pistons 20, 22, 24 which are subject to outlet pressure in each of the three rows. The piston 22 is shown above the center line in the cross section of FIG. 1 but actually there is a piston adjacent to the pistons 20, 24 but staggered with respect thereto and hence not seen in a vertical section. As seen herein the pressure pattern for the outlet port approximately equals the pattern 32 for the total effective cylinder area so that these pressures balance out. However, to the left and right of these patterns are leakage pressure patterns 34 and 36 respectively which impose an' eccentric load between the pintle and the rotor. These pressures cause a high bearing load on the other side of the pintle near the inlet port 38.
As seen in FIG. 2, it is the purpose of the present invention to have the cylinders and pistons connected in groups of three to a single row of ports approximately in the center of the rotor. Both the inlet port 40 and the outlet port 42 are made only long enough along the axis to permit proper port opening for the single row of cylinders 44. As mentioned previously in connection with FIG. 1 the cylinder 44 is shown above the center line but a similar cylinder in the same row will be located adjacent and substantially between the cylinders 46, 48 shown below the center line according to the construction of this invention.
This projected area of the pintle outlet port 42 is less than the projected areas of the adjacent cylinders of adjacent rows. Thus the pressure pattern for the port 42 is indicated along the line 50 while the pressure pattern for the cylinders is indicated as extending along the line 52. Hence, there is a net Eforce on the rotor upward toward the pintle outlet. This force is then in a direction that tends to counterbalance the leakage pressure force indicated by the patterns 56 andlSS between the rotor and pintle and therefore reduces the bearing pressure at the top of the pintle. This permits an arrangement of outlet port length, bearing lengths and piston areas such that there is a zero net bearing pressure between the rotor and the pintle. Where exact dimensioning is not feasible, compromise dimensions will permit reductions of bearing loads as high as 50%.
A typical embodiment of this invention is better shown in FIG. 3. As shown herein a pump casing 70 is illustrated as surrounding ya track ring 72 which includes an inner ring 74 engaging the outer ends of a plurality of lrows of pistons 76, 78 and 80 carried by a rotor 82. A central fixed pintle 84 is tixedly mounted in the casing 70 and carries inlet passage 86 and outlet passage 88. The rotor 82 may be suitably driven yby a gear 90 through a suitable grouping 92 which may be of the type shown and described in the labove-referred-to patent. A track ring 72 may be pivotally mounted for movement about a pivot 94 lby a suitable stroke control device as also shown in the above-referred-to patent. The outlet port 96 and the inlet port 98 are substantially of the same projected area or axial length of the area of the cylinder 100 and its corresponding piston 7S. The pistons 76 `and 80 have their corresponding pressure areas 102 and 104 connected to the adjacent cylinder and the outlet port 96 by means of recessed passages 106 and 108 respectively.
back the inner end 110 of the wall 112 of the rotor which separates -adjacent pistons. Thus the inner end 1'10 of the wall 112 of the x rotor is spaced away from the pintle axis a distance farther than the remaining inner wall portions 116, 118 of the rotor on either side ot the wall portion 112 and the adjacent pistons 76 and 80.
As a result, then the uid under pressure from the chambers 102and 104 can passthrough the passages 1061 and 108 respectively tothe adjacent cylinder of the central row and then` out through the outlet port 96.
As a result of this invention it will be apparent that a very simple highly effective means has been provided for hydraulically balancingthe. bearing loads of a pintle-rotor combination in a rotary piston hydraulic pump- This provides for relieved bearing loads, reduction in pintle deetioil, with the deflecting force having a shorter moment arm if deflecting pressures do exist. Furthermore, there isa better distribution ofthe bearing stress between thev pintle and the rotor while'also a longer'lealcage path is provided, Thisim-mediately results in a more uniform clearance along the leakage path dueto the reduced pintle deection.
Y Although oneV embodiment of this inventionv has beenY illustrated and described herein, itwill be, apparent that Various Changes may be made in the construction and arrangement of thev variousV parts without departing from the scene. of the novel cauces# We claim:
In a rotary hydraulic pump w) a Cas-ine,
(b.) a rotorrotatably supported in said casing having three rowsof cylinders each spacedyapart along the axis of rotation of the rotor, said cylinders of said rows being arranged such that the adjacent cylinders alongY saidVV axis are arranged in staggered groups,
(c) piston in said cylinders adapted to be reciprocated therein to provide. a pumping action,
These passages are formed externally of they pintle 84 by cutting.
(d) a pintle running along the axis of rotation of the rotor about which the rotor rotates,
(e) a sleeve mounted in the bore of the rotor and extending the length of the bore,
(f) means for securing the sleeve to the rotor,
(g) inlet and outlet passageways including inlet and outlet ports in said pintle communicating in timed relation-with said cylinders, said sleeve having a single row of ports registering with the center row of cylinders and intermittedly with said outlet ports, the projected area of pintle outlet port being less than the projected area of the adjacent cylinders of an adjacent group,
(h) and wall 'means between adjacent cylindersinsaid one group forming part of said rotor, said wall means being spaced at its inner end further from said sleeve thanV the remainder of said rotor thereby providing communicationV between said adjacent cylin-Y ders of said one group, said Yspaced wall means formed for each of said group and extending solely between the cylinders formed within said group.
References Cited in the file of this patent UNITED STATES PATENTS 1,998,984 Ferris Apr. 23, 1935 2,074,068 Ferris Mar. 16, 1937 2,105,454 Ferris Jan. 11, 1938 2,426,588 Benedek Sept. 2, 1947 2,455,678 Jennings Dec. 7, 1948 2,673,526 Horton Mar. 30, 19-54 OTHER REFERENCES Ernst: Oil Hydraulic'Power and lts Industrial Applications, McGraw-Hill Book C0., 1949.
Wilson: Positive Displacement Pumps, etc., Pitman & Sons, London, 1950.
Hadek-el: Displacement Pumps and Motors, Pitman & Sons, London, 1951.
US808443A 1959-04-23 1959-04-23 Pintle port construction for pumps Expired - Lifetime US3034451A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US808443A US3034451A (en) 1959-04-23 1959-04-23 Pintle port construction for pumps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US808443A US3034451A (en) 1959-04-23 1959-04-23 Pintle port construction for pumps

Publications (1)

Publication Number Publication Date
US3034451A true US3034451A (en) 1962-05-15

Family

ID=25198768

Family Applications (1)

Application Number Title Priority Date Filing Date
US808443A Expired - Lifetime US3034451A (en) 1959-04-23 1959-04-23 Pintle port construction for pumps

Country Status (1)

Country Link
US (1) US3034451A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3174408A (en) * 1961-10-10 1965-03-23 Cessna Aircraft Co Pressure loaded fluid motor with high starting torque
US3274946A (en) * 1964-04-13 1966-09-27 Edward E Simmons Pump
US3345916A (en) * 1965-11-17 1967-10-10 Tobias Jaromir High efficiency hydraulic apparatus
US3426695A (en) * 1966-05-24 1969-02-11 Beckman Instruments Inc Metering pump
US3777624A (en) * 1969-07-28 1973-12-11 K Dixon Radial hydraulic motors and pumps
US5081908A (en) * 1991-05-08 1992-01-21 Teleflex Incorporated Hydraulic pump having floating spigot valve

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1998984A (en) * 1933-11-27 1935-04-23 Oilgear Co Pump or motor
US2074068A (en) * 1933-03-23 1937-03-16 Oilgear Co Pump or motor
US2105454A (en) * 1935-12-13 1938-01-11 Oilgear Co Pump or motor
US2426588A (en) * 1945-02-06 1947-09-02 Elek K Benedek Pump or motor
US2455678A (en) * 1944-02-04 1948-12-07 Irving C Jennings Power transmission
US2673526A (en) * 1950-09-27 1954-03-30 United Aircraft Corp Support ring mounting for rotary radial piston pumps or motors

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2074068A (en) * 1933-03-23 1937-03-16 Oilgear Co Pump or motor
US1998984A (en) * 1933-11-27 1935-04-23 Oilgear Co Pump or motor
US2105454A (en) * 1935-12-13 1938-01-11 Oilgear Co Pump or motor
US2455678A (en) * 1944-02-04 1948-12-07 Irving C Jennings Power transmission
US2426588A (en) * 1945-02-06 1947-09-02 Elek K Benedek Pump or motor
US2673526A (en) * 1950-09-27 1954-03-30 United Aircraft Corp Support ring mounting for rotary radial piston pumps or motors

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3174408A (en) * 1961-10-10 1965-03-23 Cessna Aircraft Co Pressure loaded fluid motor with high starting torque
US3274946A (en) * 1964-04-13 1966-09-27 Edward E Simmons Pump
US3345916A (en) * 1965-11-17 1967-10-10 Tobias Jaromir High efficiency hydraulic apparatus
US3426695A (en) * 1966-05-24 1969-02-11 Beckman Instruments Inc Metering pump
US3777624A (en) * 1969-07-28 1973-12-11 K Dixon Radial hydraulic motors and pumps
US5081908A (en) * 1991-05-08 1992-01-21 Teleflex Incorporated Hydraulic pump having floating spigot valve

Similar Documents

Publication Publication Date Title
US3142262A (en) Pressure fluid pistons or plungers
US2845941A (en) Plate valve for rotary units
US3034451A (en) Pintle port construction for pumps
US3921601A (en) Rotary machine
GB1286405A (en) Radial hydraulic motors and pumps
US2431175A (en) Pump structure
US2918012A (en) Self regulating pump
US3855903A (en) Engines, pumps and motors
FI80131C (en) VEVSTAKE FOER SLAGKOLVFOERBRAENNINGSMOTORER.
US3050014A (en) Pump timing device
US3858483A (en) Pressure relief expansion chamber for hydrostatic motors
US2151402A (en) Air compressor
US2056622A (en) Multicylinder reciprocating piston machine
US2268532A (en) Internal combustion engine
US3122971A (en) russell
US4332532A (en) Piston pump, especially radial piston pump
US2881973A (en) Compressors for air or other gas
US3277834A (en) Rotary radial piston machine with enlarged piston stroke
US3135094A (en) Drive for conversion of a reciprocating movement into a rotary movement with a liquid as conversion means
US3508466A (en) Hydraulic machine
US2434584A (en) Multiple cylinder opposed piston and pumps
US3053197A (en) Axial piston pump with balanced drive plate
DE3322549A1 (en) Vane cell pump with variable delivery stroke for hydraulic operating media, especially of motor vehicles
US3082697A (en) Drive for barrel pumps and engines
US2421164A (en) Sleeve balancing arrangement for radial engines