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US1634141A - Pump valve - Google Patents

Pump valve Download PDF

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Publication number
US1634141A
US1634141A US54181222A US1634141A US 1634141 A US1634141 A US 1634141A US 54181222 A US54181222 A US 54181222A US 1634141 A US1634141 A US 1634141A
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US
United States
Prior art keywords
valve
wings
pump
pump valve
straight
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
Inventor
William R Hamilton
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.)
Individual
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Individual
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 Individual filed Critical Individual
Priority to US54181222 priority Critical patent/US1634141A/en
Application granted granted Critical
Publication of US1634141A publication Critical patent/US1634141A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K15/00Check valves
    • F16K15/02Check valves with guided rigid valve members
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S137/00Fluid handling
    • Y10S137/906Valves biased by fluid "springs"
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/6198Non-valving motion of the valve or valve seat
    • Y10T137/6253Rotary motion of a reciprocating valve
    • Y10T137/6307Turbine on valve

Definitions

  • My invention relates to an improvement in pump valves.
  • This invention consists of a valve of this character having turbine wings the purpose of which is to cause the valve to rotate and prevent it from continually going straight up and down and remaining in one place all the time thereby preventing the wearing of creases or grooves in the walls of the valve seats and the burning of the face of the valve seats, this valve, on the contrary, wearing the parts regularly all around'and maintaining a perfect fit on the seat, in other words keeping the valve and valve seat continually ground to an air-tight fit which assures a perfect vacuum at all times.
  • Figure 1 is a view in perspective of the valve
  • Figure 2 is a section
  • Figure 3 is a bottom plan view.
  • A represents the valve and 1 the wings cast integral with one face of the valve.
  • the wings 1 are provided with straight outer edges 2 substantially at right angles to the face 4 of the valve A.
  • the inner edges of the wings 1 are bevelled as at 5, as indicated in Fig. 1, from the face 4 to the chisel-shaped points 3 at the outer ends of the wings.
  • the straight or plain sides 6 of the Wings extend substantially at right angles to the surface 4 of the valve, but the opposite side 7 from said side 6 is bevelled in a substantially convex form, extending from the surface 4 to the chisel-shaped end 3 of each wing. It will be noted by referring to Fig.
  • the wings are elongated in a radial direction and that the outer edge 2 and one side of each Wing is straight and substantially at right angles to the surface 4 of the valve whereas the inner edge 5 and opposite'side are bevelled, the latter being in a substantially convex form.
  • the convex sides 7 formed on the corresponding wings are on the same, side of each wing as is also true of the straight slde 6.
  • a valve having a plurality of wings, each of said wings being elongated in a substantial radial direction and having a plane side and an outer face substantially parallel to the axis of the valve, and the opposite side and inner face beveled and terminating in a sharp edge at the outer end, to cause the valve to turn on being engaged by a liquid, said opposite side being curved from the base to the outer end thereof in a substantially convex form.

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Details Of Valves (AREA)

Description

1 June 28, 1927. 1,634,141
W. R. HAMILTON PUMP VALVE v Filed March '7, 92
Patented June 28, 1927.
UNITED STATES WILLIAM R. HAMILTON, F DEWEY, OKLAHOMA.
PUMP VALVE.
Application filed March 7, 1922. Serial No. 541,812.
My invention relates to an improvement in pump valves.
This invention consists of a valve of this character having turbine wings the purpose of which is to cause the valve to rotate and prevent it from continually going straight up and down and remaining in one place all the time thereby preventing the wearing of creases or grooves in the walls of the valve seats and the burning of the face of the valve seats, this valve, on the contrary, wearing the parts regularly all around'and maintaining a perfect fit on the seat, in other words keeping the valve and valve seat continually ground to an air-tight fit which assures a perfect vacuum at all times.
In the accompanying drawings:
Figure 1 is a view in perspective of the valve,
Figure 2 is a section, and
Figure 3 is a bottom plan view.
A represents the valve and 1 the wings cast integral with one face of the valve. The wings 1 are provided with straight outer edges 2 substantially at right angles to the face 4 of the valve A. The inner edges of the wings 1 are bevelled as at 5, as indicated in Fig. 1, from the face 4 to the chisel-shaped points 3 at the outer ends of the wings. The straight or plain sides 6 of the Wings extend substantially at right angles to the surface 4 of the valve, but the opposite side 7 from said side 6 is bevelled in a substantially convex form, extending from the surface 4 to the chisel-shaped end 3 of each wing. It will be noted by referring to Fig. 3 that the wings are elongated in a radial direction and that the outer edge 2 and one side of each Wing is straight and substantially at right angles to the surface 4 of the valve whereas the inner edge 5 and opposite'side are bevelled, the latter being in a substantially convex form. The convex sides 7 formed on the corresponding wings are on the same, side of each wing as is also true of the straight slde 6.
Thewings hang downwardly and as the fluid from the pump comes up through them it causes the valves to turn just a trifle each time the pump plunger makes a stroke thereby maintaining a perfect fit of the valve surface 4 upon the seat 8.
In other words this action keeps the valve and seat continually ground to an air-tight fit insuring a perfect vacuum at all times. In this way the burring or creasing of the valve seats is absolutely prevented.
By rotating the valve in this way by means of the turbine wings it prevents the valve from continually reseating itself in the same positionor relation with straight up and down movement but on the contrary every time the valve resumes its seat it has been slightly turned by the pressure of the fluid against the beveled surface of the wings.
It is because of this action that the term turbine winged valve has been employed, that is to say because the wings are all beveled on the same side, consequently when the piston plunger of the pump is operated the fluid is-forced through the valve causing the latter to turn in the direction opposite to the beveled sides, the fluid impinging on the beveled surface simultaneously with the effect of forcing the wings aside in turning the valve.
I claim:
A valve having a plurality of wings, each of said wings being elongated in a substantial radial direction and having a plane side and an outer face substantially parallel to the axis of the valve, and the opposite side and inner face beveled and terminating in a sharp edge at the outer end, to cause the valve to turn on being engaged by a liquid, said opposite side being curved from the base to the outer end thereof in a substantially convex form. y
In testimony whereof I allix my signature.
WILLIAM R. HAMILTON.
US54181222 1922-03-07 1922-03-07 Pump valve Expired - Lifetime US1634141A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US54181222 US1634141A (en) 1922-03-07 1922-03-07 Pump valve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US54181222 US1634141A (en) 1922-03-07 1922-03-07 Pump valve

Publications (1)

Publication Number Publication Date
US1634141A true US1634141A (en) 1927-06-28

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Family Applications (1)

Application Number Title Priority Date Filing Date
US54181222 Expired - Lifetime US1634141A (en) 1922-03-07 1922-03-07 Pump valve

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1173298B (en) * 1958-10-03 1964-07-02 Unilever Nv Self-opening and closing cap for compressible tubes
US20060054850A1 (en) * 2004-09-13 2006-03-16 Cooper Cameron Corporation Rotating check valve for compression equipment

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1173298B (en) * 1958-10-03 1964-07-02 Unilever Nv Self-opening and closing cap for compressible tubes
US20060054850A1 (en) * 2004-09-13 2006-03-16 Cooper Cameron Corporation Rotating check valve for compression equipment
US7073775B2 (en) 2004-09-13 2006-07-11 Cameron International Corporation Rotating check valve for compression equipment

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