US1520853A - Air-compressor piston - Google Patents

Air-compressor piston Download PDF

Info

Publication number
US1520853A
US1520853A US618257A US61825723A US1520853A US 1520853 A US1520853 A US 1520853A US 618257 A US618257 A US 618257A US 61825723 A US61825723 A US 61825723A US 1520853 A US1520853 A US 1520853A
Authority
US
United States
Prior art keywords
stage
piston
pistons
air
rod
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
US618257A
Inventor
Frank T Cable
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.)
Electric Boat Corp
Original Assignee
Electric Boat 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
Priority claimed from US393066A external-priority patent/US1520852A/en
Application filed by Electric Boat Corp filed Critical Electric Boat Corp
Priority to US618257A priority Critical patent/US1520853A/en
Application granted granted Critical
Publication of US1520853A publication Critical patent/US1520853A/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
    • 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
    • F04B25/00Multi-stage pumps
    • F04B25/02Multi-stage pumps of stepped piston type

Definitions

  • This invention relates to two-stage air compressors, and more particularly to the second-stage pistons used in such compressors.
  • the first and second stage pistons of two-stage air compressors are rigidly connected. This makes it necessary that the walls of the first and second stage cylinders be exactly parallel and that the two pistons be in perfect alignment. In practice these conditions are difiicult tomeet, requiring as they do, exact and painstaking workmanship, and as a very slight deviation from exact parallelism between the parts results in rapid wear, particularly in the second stage cylinder, it has been found ditlicult to maintain a tight fit between the secondstagepiston and its cylinder for more than short periods. The wear is taken up in large measure by the snap rings of the piston which must, in consequence, be renewed, some times as often as every two or three months. This operation is difiicult and costly as the compressor must be entirely dismantled and both pistons removed in order to gain access to the second-stage piston.
  • Fig. 1 is a section through a two-stage air-compressor equipped with relatively movable pistons designed in accordance with the present invention
  • Fig. 2 is a section through the two pistons on an enlarged scale.
  • 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 integral cast and form in effect one cylinder having two different bores.
  • the two pistons are connected by means of a bolt 7 which passes through the upper end of the 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 position 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 18 expands threaded end 11 and fixes the nut 9 tightly in position.
  • Piston 5 is provided at its upper end with a semi-sphen ical cap 14 locked in position by means of screw 15. Cylinder 3 is hushed by means of a removable sleeve or bushing 16 forming the wearing surface for the piston 5.
  • piston 5 might I No. 393,066, filed June 30, 1920'.
  • a two-stage air compressor the combination of a first-stage piston, a. rod extending from the upper end thereof, a nut on the outer end of the rod, a. hollow second-stage piston, and an annular flange therein, dished around its upper and inner periphery, the nut on the rod bearing against the dished portion of the annular flange to hold the second-stage piston in place on the first-stage piston, there being. clearances between the rod and the secondstage piston permitting slight relative move ment between the two pistons.
  • first and secondstage pistons mounted to reciprocate within their respective cylinders, and means con necting the two pistons permitting slight unrestrained combined relative lateral and angular movement between them to compensate for inaccuracies in the alignment.
  • a two-stage air-compressor the combination of a one-piece casting forming the walls of the first and second-stage cylinders in substantial alignment, first and secondstage pistons mounted to reciprocate within their respective cylinders, said pistons abutting against one another and being provided with a connecting rod loosely connected at each end to one of the pistons so as to permit slight unrestrained 'elative movement between them to compensate for inaccuracies in the alignment of the pistons.
  • a two-stage air compressor the combination of a first-stage piston, a rod er;- tending from the outer end thereof, a hollow second-stage piston having annular flange therein, means on the rod bearing against the annular flange to hold the second-stage piston in place on the first-stage piston, there being a clearance between the rod and the flange permitting slight relative movement between the two pistons.
  • a two-stage air-compressor the com-- bination of a first-stage piston, a rod extending from the outer end thereof, a nut on the outer end of the rod, a hollow secondstage piston, and an annular flange therein, the nut on the rod bearing against the annular flange to hold the second-stage piston in place on the first-stage piston, there being a clearance between the inner end of the rod and the second-stage piston permitting slight relative movement between the two pistons.

Landscapes

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

Description

Dec. 1924b 1,520,853
F. T. CABLE AIR COMPRESSOR PISTON Original Filed June 30, 1920 2 Sheets-Sheet 1 76 eng/ne Zawpressure coo/er INVENTOR mil 7- 1&1. ATTORNEYS 'Dec. 30, 1924.
F. 'r. CABLE AIR COMPRESSOR PISTON original Filed Juh so, 1
2 Sheets-Sheet 2 IINVEN OR W J M A14 ATTORNEYS Patented Dec. 30, 1924.
FRANK '1. CABLE, OF NEW LONDON, CONNECTICUT, ASSIGNOR T0 ELECTRIC BOAT COMPANY, A. CORPORATION OF NEW JERSEY.
AIR-COMPRESSOR PISTON.
Original application filed June 30, 1920, Serial No. 393,066. Divided and this application filed. February 10, 1923. Serial No. 618,257.
To all whom it may concern:
Be it known that I, FRANK T. CABLE, a citizen of the United States, residing at New London, in the county of New London, State of Connecticut, have invented certain new and useful Improvements in Air-Compressor Pistons; and I do hereby declare the following to be a full, clear, and exact description of the invention, such as will. enable others skilled in the art to which it appertains to make and use the same.
This invention relates to two-stage air compressors, and more particularly to the second-stage pistons used in such compressors.
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 walls of the first and second stage cylinders be exactly parallel and that the two pistons be in perfect alignment. In practice these conditions are difiicult tomeet, requiring as they do, exact and painstaking workmanship, and as a very slight deviation from exact parallelism between the parts results in rapid wear, particularly in the second stage cylinder, it has been found ditlicult to maintain a tight fit between the secondstagepiston and its cylinder for more than short periods. The wear is taken up in large measure by the snap rings of the piston which must, in consequence, be renewed, some times as often as every two or three months. This operation is difiicult and costly as the compressor must be entirely dismantled and both pistons removed in order to gain access to the second-stage 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 invention to accomplish this.
Going back to first causes, the origin of the trouble is found in the practical. difii culty of getting perfect alignment between the two cylinders, which are preferably integrally cast and must be machined with most exacting care. This difliculty has been overcome by the present invention through the simple expedient of doing away clearly understood reference is had to the accompanying drawings disclosing One specific embodiment thereof.
In these drawings, Fig. 1 is a section through a two-stage air-compressor equipped with relatively movable pistons designed in accordance with the present invention; and Fig. 2 is a section through the two pistons on an enlarged scale.
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 integral cast and form in effect one cylinder having two different bores. The two pistons are connected by means of a bolt 7 which passes through the upper end of the 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 position 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 18 expands threaded end 11 and fixes the nut 9 tightly in position. Piston 5 is provided at its upper end with a semi-sphen ical cap 14 locked in position by means of screw 15. Cylinder 3 is hushed 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 I No. 393,066, filed June 30, 1920'.
I claim:
1. In twostage air-compressor the combination of a first-stage piston, a rod extending from the outer end thereof, a nut on the outer end of the rod, a hollow second-stage piston, and an annular flange therein, the nut on the rod bearing against the annular flange to hold the second-stage piston in place on the first-stage piston, there being clearances between the rod and the second-stage piston permitting slight relative movement between the two pistons.
2. In a two-stage air compressor, the combination of a first-stage piston, a. rod extending from the upper end thereof, a nut on the outer end of the rod, a. hollow second-stage piston, and an annular flange therein, dished around its upper and inner periphery, the nut on the rod bearing against the dished portion of the annular flange to hold the second-stage piston in place on the first-stage piston, there being. clearances between the rod and the secondstage piston permitting slight relative move ment between the two pistons.
3. In a two-stage air-compressor, the coml'ajination of a first-stage piston, a rod extending from the outer end thereof, a nut on the outer end of the rod, a hollow secondstage piston, an annular flange'therein, the nut on the rod bearing against the annular flange to hold the second-stage piston in place on the first-stage piston, there being clearances between the rod and the secondstage piston permitting slight relative movement between the two pistons, and a cap on the second-stage piston covering the nut.
4. In a two-stage air-compressor, the combination of a one-piece casting forming the walls of the first and second-stage cylinders in substantial alignment, first and secondstage pistons mounted to reciprocate within their respective cylinders, and means con necting the two pistons permitting slight unrestrained combined relative lateral and angular movement between them to compensate for inaccuracies in the alignment.
'5. In a two-stage air-compressor, the combination of a one-piece casting forming the walls of the first and second-stage cylinders in substantial alignment, first and secondstage pistons mounted to reciprocate within their respective cylinders, said pistons abutting against one another and being provided with a connecting rod loosely connected at each end to one of the pistons so as to permit slight unrestrained 'elative movement between them to compensate for inaccuracies in the alignment of the pistons.
6. In a two-stage air compressor the combination of a first-stage piston, a rod er;- tending from the outer end thereof, a hollow second-stage piston having annular flange therein, means on the rod bearing against the annular flange to hold the second-stage piston in place on the first-stage piston, there being a clearance between the rod and the flange permitting slight relative movement between the two pistons.
7. In a two-stage air-compressor the com-- bination of a first-stage piston, a rod extending from the outer end thereof, a nut on the outer end of the rod, a hollow secondstage piston, and an annular flange therein, the nut on the rod bearing against the annular flange to hold the second-stage piston in place on the first-stage piston, there being a clearance between the inner end of the rod and the second-stage piston permitting slight relative movement between the two pistons.
In testimony whereof I aliiX my signature.
FRANK T. CABLE.
US618257A 1920-06-30 1923-02-10 Air-compressor piston Expired - Lifetime US1520853A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US618257A US1520853A (en) 1920-06-30 1923-02-10 Air-compressor piston

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US393066A US1520852A (en) 1920-06-30 1920-06-30 Air-compressor piston
US618257A US1520853A (en) 1920-06-30 1923-02-10 Air-compressor piston

Publications (1)

Publication Number Publication Date
US1520853A true US1520853A (en) 1924-12-30

Family

ID=27014145

Family Applications (1)

Application Number Title Priority Date Filing Date
US618257A Expired - Lifetime US1520853A (en) 1920-06-30 1923-02-10 Air-compressor piston

Country Status (1)

Country Link
US (1) US1520853A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2695132A (en) * 1948-06-25 1954-11-23 Joy Mfg Co Compressor
US4173432A (en) * 1977-04-19 1979-11-06 Vines Dorwin J Vertical wave air compression device
EP0640764A1 (en) * 1993-08-25 1995-03-01 Maschinenfabrik Sulzer-Burckhardt AG Piston compressor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2695132A (en) * 1948-06-25 1954-11-23 Joy Mfg Co Compressor
US4173432A (en) * 1977-04-19 1979-11-06 Vines Dorwin J Vertical wave air compression device
EP0640764A1 (en) * 1993-08-25 1995-03-01 Maschinenfabrik Sulzer-Burckhardt AG Piston compressor
US5467687A (en) * 1993-08-25 1995-11-21 Maschinenfabrik Sulzer Burckhardt Ag Piston compressor

Similar Documents

Publication Publication Date Title
US3465651A (en) Composite pistons
US1520853A (en) Air-compressor piston
US2604076A (en) Multistroke fluid operated power actuator
US2726887A (en) Plunger connection for reciprocating pumps
US1520852A (en) Air-compressor piston
US2396500A (en) Oil cooled piston
US1866873A (en) Internal combustion engine
US1784291A (en) Piston
US2683638A (en) Liner for compressors
US1156312A (en) Cylinder for internal-combustion engines.
US2258576A (en) Circumferentially tightening packing ring
US1180777A (en) High-pressure piston.
US2282721A (en) Engine construction
US1925444A (en) Cylinder head construction
US2084834A (en) Piston
US1898145A (en) Composite cylinder for internal combustion engines
US774710A (en) Metallic packing.
US1067484A (en) Multiple-expansion engine.
US1860274A (en) Resilient packing
US1301740A (en) Construction of water-jacketed engine-cylinders.
US451478A (en) William e
US1095840A (en) Packing and bushing.
US896870A (en) Stuffing-box.
US2051305A (en) Piston
US1488153A (en) Packing box