US1520852A - Air-compressor piston - Google Patents

Air-compressor piston Download PDF

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Publication number
US1520852A
US1520852A US393066A US39306620A US1520852A US 1520852 A US1520852 A US 1520852A US 393066 A US393066 A US 393066A US 39306620 A US39306620 A US 39306620A US 1520852 A US1520852 A US 1520852A
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Prior art keywords
stage
piston
cylinder
air
pistons
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Expired - Lifetime
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US393066A
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Cable Frank Taylor
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Electric Boat Corp
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Electric Boat Corp
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Priority to US393066A priority Critical patent/US1520852A/en
Priority to US618257A priority patent/US1520853A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B25/00Multi-stage pumps
    • F04B25/02Multi-stage pumps of stepped piston type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/0005Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00 adaptations of pistons
    • F04B39/0022Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00 adaptations of pistons piston rods
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/12Casings; Cylinders; Cylinder heads; Fluid connections
    • F04B39/126Cylinder liners

Definitions

  • This invention relates to two-stagel aircompressors, and more particularly to the second-stage'pistons used in such compressors. n y
  • the first and second stage pistons of two-stage air compressors are rigidly connected. .
  • To ⁇ provide meansfor withdrawing' the second-stage piston through thefsecondestage hea-d and' without entailing adismantling of the'compressor;
  • A'still further object which shall be'm'ade clearer from the following description is to'provide ay self-aligning second-stage piston which shall have no mechanical connection with the first-stage piston, relying upon air pressure to force it'down.
  • Fig. 1 is a vertical section through a. twostage air compressor showing the construction of one form of second-stage piston made in accordance with this invention and a part of the first-stage piston connected thereto. As shown in this figure the second-stage head has been removed and the piston moved to a position in readiness for removal;
  • Fig. 2 is a vertical section of a modiiied form of second-stage piston designed to have no mechanical connection with the firststage piston;
  • Fig. 3 is a perspective view of the two-part collar used in forcing the bushing from its cylinder.
  • Fig. 4 is a vertical section through a twostage air compressor showing the second stage piston of Fig. 2 mounted within the second stage cylinder.
  • 1 represents a two-stage air-compressor.
  • 2 represents the first-stage cylinder
  • 3 the secondstage cylinder
  • 4 the first-stage. piston
  • 5 the second-stage piston, this last being provided with peripheral grooves 6 which fill with oil and serve as seal rings.
  • the walls of the two cylinders are integrally cast and form in effect one cylinder having bores of two different diameters.
  • the two pistons are connected by means of a bolt 7 which passes through the upper end of piston 4, being keyed thereto at 8, and is provided at its upper end with a special nut 9 which bears upon an internal annular flange 10 ⁇ situated near the upper end of piston 5.
  • This nut is screwed upon threaded end 11 of bolt 7 and locked in posit-ion by means of tapered pin 12' which is screwed in the upper end of nut 9 and seated in a tapered and split socket 13 in the threaded end 11 of the bolt. Insertion of pin 12 into socket 13 expands threaded end 11 and fixes the nut 9 tightly in position.
  • Piston 5 is provided at its upper end with a semi-spherical cap 14 locked in position by means of screw 15. Cylinder 3 is bushed by means of a removable sleeve or bushing 16 forming the wearing surface for the piston 5.
  • Cap 14 may then be readily removed and then in succession pin 12 and nut 9. IVith this done it becomes an easy matter to lift piston 5 from its cylinder with the help of a. special wrench having a pin which cooperates with a hole 21 drilled in the side of the piston near its upper end.
  • the first-stage piston is drawn down below the lower end o of the bushing and the two-part collar 22 shown in Fig. 3 introduced through cylinder 3 and seated upon the upper end of piston 4.
  • An annular groove 23 is bored in the upper end of this piston and is adapted to receive aI depending flange 24 on collar 22.
  • the diameter of this collar is greater than the internal diameter of the bushing but less than the external.
  • FIG. 2 A modified form of second-stage piston is shown in Figs. 2 and 4, the novelty of which resides in the fact that there is no mechanical connection whatever between it and the first-stage piston.
  • This modified piston comprises a cylindrical shell 25 provided with peripheral grooves 26 which act as sealing rings as described before.
  • a case-hardened cap 27 incloses the lower end of the piston and is locked in place by means of screw 28. This cap bears upon the upper end kof the first-stage piston.
  • the compression stroke of the first-stage piston pushes the second-stage piston along its cylinder and thus effects the second compression.
  • the air which has just previously been compressed in the first-stage cylinder and is under a pressure of about seventyfive pounds per square inch is led into the upper end of the second-stage cylinder. This pressure is ample to force the looselyv mounted second-stage piston downward and keep cap 27 in constant contact with the first-stage piston.
  • This arrangement even simpler than that shown in Fig. 1;
  • a second-stage piston for air-compressors comprising the combination of a cylindrical body portion and a cap at one end thereot4 adapted to bear upon the end of the first-stage piston.
  • first and second-stage cylinders in substantial alignment mounted to reciprocate within their respective cylinders, a removable hea-d on the second-stage cylinder and means per' mitting separation of the two pistons and removal of the second-stage piston through the outer end of the second-stage cylinder.
  • first and second-stage cylinders In a two-stage air-compressor, the combination of first and second-stage cylinders, first and second-stage pistons in substantial alignment mounted to reciprocate within their respective cylinders, a removable bushing or sleeve in the second-stage cylinder, a removable head on the second-stage cylinder, and means for removing both secondstage piston and bushing through the Outer end of the second-stage cylinder.
  • first and second-stage cylinders in substantial alignment mounted to reciprocate within their respective cylinders, a removable bushing or sleeve in the second-stage cylinder, a removable head on the second-stage cylinder, means for removing the second-stage piston and means cooperating with the upper end of' the first-stage piston to move the bushing out of its cylinder.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

Dec, 30, 1924.
F. T. CABLE AIR COMPRESSOR FISTON Filed June 30 1920 2 Sheets-Sheet 1 De@ 30, 19?-4. 1,520,852 F. T. CABLE A-IR COMPRESSOR PI STON Filed June 30, 1920 2 Sheets-Sheet 2 TUE/wwf aw/vmware cao/er l, ATTORNEYS Patented Dec. 30, 1924,
UNI-rr: STATES PATENT' OFI-#leila FRANK TAYLOR CABLE, OF.; NEW HII'.|O1\TZDO1\T,V CONNECTICUT, `ASSllGrN'ORiTO ELECTRIC i BOAT COMPANY, A CORPORATION F NEW JERSEY.
` AIR-COMPRESSOR PISTON.
Application led June 30, 1920K.v Serial No. 393,066.
To ally whom t may concern.'
Be `it knownthatl, FRANKrT. CABLE, a citizen of the United States, residing at New London, in thelcountyof NewV London, State of Connecticut, lhave invented certain new and useful Improvements in Air-Compressor Pistons; and I do hereby declare the following to be a. full, clear, andeXact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same. y
. This invention relates to two-stagel aircompressors, and more particularly to the second-stage'pistons used in such compressors. n y
According to the present practice the first and second stage pistons of two-stage air compressors are rigidly connected. .This
makes it necessary that the wallsof the first and second .stage cylinders be exactly parallel and-that the-two pistons be in perfect alignment. In practice Kthese conditions are difficult to meet, requiring as they do, exact and painstaking workmanship, and as a very r slight deviation from exact parallelism between the parts results in' rapid wear, particularly in the second stage cylinder, it has beenv found diicult to maintain a tight fit between the-second-stage piston and its cyl- 3U inder for more than short periods. The wea-r is taken up in llarge measure by the snap rings ofthe piston which must, in consequence, be renewed, sometimes as often as every two or three months. This operation is ditlicult and costly as the compressor must be entirely dismantled and both pistons removed in order to gain access to thesecondstage piston.
It is, therefore, clear that could some means be. devised for minimizing this wear and obviating the necessity for such frequent replacements of the second-stage piston rings, a very substantial saving in time and expense could be effected. It is broadly an object of the inventionto accomplish this.
Going back to `first causes, the origin of the trouble isy found in the practical difficulty of getting perfect alignment between the two cylinders which are preferabl yintegrally cast and must-be machined wit most exacting care. This difficulty has been overcome by thev present `invention through the simple expedient of doing away with the necessity for such exact alignment. To do this'the two pistons are mounted forre1- ative, lateral and angular play, and thus automatically adjust themselves to any i-naccuracies in the cylinder parallelism; -In doing this two important results yare obtained; first, the wear `is minimized, and,
second, the need for scrupulous care in machining or grinding the'cylinder bores is done away with. f However, aA certain amount o-f wear is inevitable, and as the' leakagearound the pistons incidentiupon this wear yis more pronounced in the second-stage cylinder than in the irst,'ity still becomes necessary and desirable occasionally to remove the second` stage piston for the replacement of its snap rings or the substitution of a new piston. Accordingto the present invention means have been devised whereby this may be done by simply removing the second stage head and without dismantling thel whole compressor. l l
It' has been found advantageous to eliminate pistonrings entirely on ythe lsecondstage piston and to employ a soecalled solid piston having considerablyl greater surface contact with the cylinder walls than is or dinarily the case, andpro-vided with a series of peripheral grooves vo-r seal rings, such grooves being old in this and analogous arts. As'the wear on such a piston and its cyl` inder cannot be compensatedfforvby theuse of a new set of snap rings,nor Iyet by the substitution of a new piston having the old original diameter, it becomes necessary to bush the cylinder with aremovable bushing. The provision of .suchi a bushing is contemplated by the presentinvention.
i To recapitulate,.the objects of this invention'are: f'
To minimize wear in the second-stage cylinder and do away with the need for nice alignmentY 'between thelirstf-and second stage, cylinders and pistons by mounting the two pistons for relative play: 1
To` provide meansfor withdrawing' the second-stage piston through thefsecondestage hea-d and' without entailing adismantling of the'compressor; and
To providel the second-stage':cylinderf with a bushingfwhich shall be removable in the same mannerthat thesecond-'stage piston is removable.`
A'still further object which shall be'm'ade clearer from the following description is to'provide ay self-aligning second-stage piston which shall have no mechanical connection with the first-stage piston, relying upon air pressure to force it'down.
Other `and minor objects will be apparent as the description proceeds.
In order that the invention may be more cle-arly understood reference is had to the accompanying drawings disclosing one speciiic embodiment thereof, although it is to be distinctly understood that the invention in its broader aspects is not limited to these details of construction.
Fig. 1 is a vertical section through a. twostage air compressor showing the construction of one form of second-stage piston made in accordance with this invention and a part of the first-stage piston connected thereto. As shown in this figure the second-stage head has been removed and the piston moved to a position in readiness for removal;
Fig. 2 is a vertical section of a modiiied form of second-stage piston designed to have no mechanical connection with the firststage piston;
Fig. 3 is a perspective view of the two-part collar used in forcing the bushing from its cylinder.
Fig. 4 is a vertical section through a twostage air compressor showing the second stage piston of Fig. 2 mounted within the second stage cylinder.
In the drawings, 1 represents a two-stage air-compressor. In this compressor, 2 represents the first-stage cylinder, 3 the secondstage cylinder, 4 the first-stage. piston, and 5 the second-stage piston, this last being provided with peripheral grooves 6 which fill with oil and serve as seal rings. The walls of the two cylinders are integrally cast and form in effect one cylinder having bores of two different diameters. The two pistons are connected by means of a bolt 7 which passes through the upper end of piston 4, being keyed thereto at 8, and is provided at its upper end with a special nut 9 which bears upon an internal annular flange 10` situated near the upper end of piston 5. This nut is screwed upon threaded end 11 of bolt 7 and locked in posit-ion by means of tapered pin 12' which is screwed in the upper end of nut 9 and seated in a tapered and split socket 13 in the threaded end 11 of the bolt. Insertion of pin 12 into socket 13 expands threaded end 11 and fixes the nut 9 tightly in position. Piston 5 is provided at its upper end with a semi-spherical cap 14 locked in position by means of screw 15. Cylinder 3 is bushed by means of a removable sleeve or bushing 16 forming the wearing surface for the piston 5.
Play between the two pistons is permitted by clearance spaces 17, 18 and 19. In a case where alignment of the two cylinders hap-- pened to be particularly bad, piston 5 might be twisted so far as to bind at the point where the edge of nut 9 bore upon flange 10. in order to prevent this the upper face. of this iiange is dished slightly as shown at 20.
To remove piston 5, the second-stage head is detached and the two pistons moved up to the position shown in Fig. 1. Cap 14 may then be readily removed and then in succession pin 12 and nut 9. IVith this done it becomes an easy matter to lift piston 5 from its cylinder with the help of a. special wrench having a pin which cooperates with a hole 21 drilled in the side of the piston near its upper end.
To remove the bushing, the first-stage piston is drawn down below the lower end o of the bushing and the two-part collar 22 shown in Fig. 3 introduced through cylinder 3 and seated upon the upper end of piston 4. An annular groove 23 is bored in the upper end of this piston and is adapted to receive aI depending flange 24 on collar 22. The diameter of this collar is greater than the internal diameter of the bushing but less than the external. Upon again moving the piston 4 upward the peripheral face of collar 22 will bear against the lower end of the bushing and force it out of its cylinder a short distance. It is then an easy matter to complete the removal.
By making both the piston and its bushing removable, it becomes possible to replace them with a new' pair which have been accurately fitted at the factory. A tight lit is, therefore, assured. IVithout the provision of a removable bushing it is a diHicult matter when replacing worn pistons of this type to attain a perfect iit for the obvious reason that there are no snap rings to take up the wear upon the cylinderwalls.
A modified form of second-stage piston is shown in Figs. 2 and 4, the novelty of which resides in the fact that there is no mechanical connection whatever between it and the first-stage piston. This modified piston comprises a cylindrical shell 25 provided with peripheral grooves 26 which act as sealing rings as described before. A case-hardened cap 27 incloses the lower end of the piston and is locked in place by means of screw 28. This cap bears upon the upper end kof the first-stage piston. In operation, the compression stroke of the first-stage piston pushes the second-stage piston along its cylinder and thus effects the second compression. Upon the return stroke the air which has just previously been compressed in the first-stage cylinder and is under a pressure of about seventyfive pounds per square inch is led into the upper end of the second-stage cylinder. This pressure is ample to force the looselyv mounted second-stage piston downward and keep cap 27 in constant contact with the first-stage piston. This arrangement even simpler than that shown in Fig. 1;
errors in alignment are automatically taken care of, and the removal of the piston is an easy mattei'.
Although this invention has been spoken of and described in connection with twostage air-compressors, it is obvious that the principles involved might easily be applied to compressors operating in more than two stages. It is also obvious that the invention is not necessarily limited to air-compressors, but is applicable to pumps or any other machines which present similar problems in the matter of alignment and removal of parts.
I claim:
l. In a two-stage air-compressor the comhination of first and second-stage pistons having no mechanical connection between them.
9,. In a two-stage air-compressor the combination of' first and second-stage cylinders and first and second-stage pistons in substantial alignment, mounted t-o reciprocate within their respective cylinders, and having no mechanical connection with each other, Contact between them being maintained by the air pressure within the secondstage cylinder.
3. In a multi-stage air-compressor or the like, the combination of a plurality of cylinders of progressively increasing pressure, a plurality of pistons in substantial alignment, mounted to reciprocate within their respective cylinders, and having no mechanical connection with one another, contact between adjacent pistons being maintained by the air pressure within the higher pressure cylinder.
4. A second-stage piston for air-compressors comprising the combination of a cylindrical body portion and a cap at one end thereot4 adapted to bear upon the end of the first-stage piston.
5. In a two-stage air-compressor, the combination of first and second-stage cylinders, first and second-stage pistons in substantial alignment mounted to reciprocate within their respective cylinders, a removable hea-d on the second-stage cylinder and means per' mitting separation of the two pistons and removal of the second-stage piston through the outer end of the second-stage cylinder.
6. In a two-stage air-compressor, the combination of first and second-stage cylinders, first and second-stage pistons in substantial alignment mounted to reciprocate within their respective cylinders, a removable bushing or sleeve in the second-stage cylinder, a removable head on the second-stage cylinder, and means for removing both secondstage piston and bushing through the Outer end of the second-stage cylinder.
7. In a two-stage air-compressor, the combination of' first and second-stage cylinders, first and second-stage pistons in substantial alignment mounted to reciprocate within their respective cylinders, a removable bushing or sleeve in the second-stage cylinder, a removable head on the second-stage cylinder, means for removing the second-stage piston and means cooperating with the upper end of' the first-stage piston to move the bushing out of its cylinder.
In testimony whereof I afx my signature.
FRANK TAYLOR CABLE.
US393066A 1920-06-30 1920-06-30 Air-compressor piston Expired - Lifetime US1520852A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2622791A (en) * 1947-12-16 1952-12-23 Bristol Pneumatic Tools Ltd Two-stage air compressor
US2758897A (en) * 1953-12-01 1956-08-14 Ingersoll Rand Co Piston and rod connection
US4098560A (en) * 1974-06-21 1978-07-04 Physics International Company Fuel injection pumps for internal combustion engines
US4141675A (en) * 1975-12-22 1979-02-27 Physics International Company Gas-actuated fuel pump wherein the pump piston is driven by a spring

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2622791A (en) * 1947-12-16 1952-12-23 Bristol Pneumatic Tools Ltd Two-stage air compressor
US2758897A (en) * 1953-12-01 1956-08-14 Ingersoll Rand Co Piston and rod connection
US4098560A (en) * 1974-06-21 1978-07-04 Physics International Company Fuel injection pumps for internal combustion engines
US4141675A (en) * 1975-12-22 1979-02-27 Physics International Company Gas-actuated fuel pump wherein the pump piston is driven by a spring

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