US706979A - Compound air-compressor. - Google Patents

Compound air-compressor. Download PDF

Info

Publication number
US706979A
US706979A US7211501A US1901072115A US706979A US 706979 A US706979 A US 706979A US 7211501 A US7211501 A US 7211501A US 1901072115 A US1901072115 A US 1901072115A US 706979 A US706979 A US 706979A
Authority
US
United States
Prior art keywords
air
compressor
cylinders
cylinder
compression
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
US7211501A
Inventor
George E Martin
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.)
PEDRICK AND AYER Co
Original Assignee
PEDRICK AND AYER Co
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 PEDRICK AND AYER Co filed Critical PEDRICK AND AYER Co
Priority to US7211501A priority Critical patent/US706979A/en
Application granted granted Critical
Publication of US706979A publication Critical patent/US706979A/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
    • F04B39/06Cooling; Heating; Prevention of freezing

Definitions

  • THE wams PETER c., PuoToLrrna. wAsHlNsTou. n. c.
  • Nrrn rares artnr rricn
  • This invention relates to improvements in compound air-compressors 5 and it consists in the relative arrangement with the circulating water-jackets that surround the compressioncylinders and valve-chambers of the air-passages and air-receiving chambers, whereby a material reduction of the temperature of the air is maintained under the reduction in its volume, all as hereinafter more particularly described, reference being had to the accompanying drawings, forming a part of this specification, in which- Figure l represents a vertical section of the air-compressor.
  • Fig. 2 is an enlarged vertical section of compression-cylinders on line 2 2 of Fig. 3.
  • Fig. 3 is a top view of cylinder covers and valves.
  • Fig. l is a vertical section through cylinder covers and valves on lines 4 4 i 4 fl.
  • Fig. 5 is a horizontal section through cylinders on line 5 5 of Fig. 2.
  • the larger compression-cylinder is represented by A and the smaller cylinder by A', and the details of their construction and the operative parts are hereinafter referred to by letters of reference which denote similar detail parts in the respective figures.
  • the operative parts included ⁇ e ⁇ t ⁇ he main driving-shaft a, provided with the fast-and loose band'- wheels or belt-pulleys l) c, the cranks d e, connecting-rods f g, and pistons 7L t', together with the induction and discharge valves lettered, respectively, j and 7c, all relatively located in a manner common to this type of compressor.
  • the outer shell B includes both the larger and smaller compression-cylinders forming part of the shell of the water-jacket of the larger cylinder and the outer shell of an air-receiving chamber D, that embraces the water-jacket of the smaller cylinder, as shown in plan on the enlarged sectional view, Fig. 5.
  • the inner wall of the air-receiving chamber or cooler D is therefore completely exposed to the circulating waterjackets and its outer wall or shell to the atmosphere, and the temperature of the air is by this construction consequently reduced to the minimum degree possible in the utilization of the cir-u culating water-jackets of the operative cylinders.
  • This air-receiving chamber or intercooler D is in practice about two and onehalf times larger incapacity than the pistondisplacement in the larger cylinder A, and a constant pressure is maintained therein that will force the confined air through the induction-valves and lill the smaller cylinder A.
  • This pressure from the air-receiver or intercooler D also acts to assist the downward stroke of the smaller piston, and thereby a degree of mechanical work is derived equivalent tothe use of less operative power.
  • Upon the return or compressingstroke of the smaller piston the volume of the conlined air is still further compressed in the usual way, the consequent increase of temperature being checked by the effect of the surrounding water circulation.
  • the induction and discharge valves j and 7c are located in chambers provided in the top heads of the respective cylinders A A', covered with caps or bonnets m and normally held to their seats by springs n, as shown in the respective figures.
  • a compound air-compressor provided with an air-receiver intermediate of and adjacent to the respective compression-cylinders having its inner wall in contact with the circulating water-jackets of said cylinders, and cooling-jacketsinclosing the connecting air-spaces, whereby the air is in contact with cooled surfaces during the entire period of its passage, as set forth.
  • an airreceiver intermediate of and adjacent to the respective compression-cylinders having its inner wall in contact with the circulating water-jackets of said cylinders and its outer wall exposed to the atmosphere as set forth.
  • a compound air-compressor having an air-receiver intermediate of the respective compression-cylinders, its inner wall forming the outer surrounding wall of the circulating water-jacket of the smaller cylinder and adjacent wall of the water-jacket of the larger cylinder, as set forth.

Description

No. 706,979. Patented Aug. |2, |902.
G. E. MARTIN. CGMPOUND AIB UDMPBESSUR. (Application led Aug. 15, 1901.)
(No Model.) 4 Sheets-Sheet l.
lll lllnl':
'ull
y @gw @M0535 G. E. MARTIN.
' COMPOUND AIR (IMPH'ESSURl (Application filed Aug. 15, 1901.) l(-||u lli!del.)` 4 Sheets-Sheet 2.
Np. 706,979. Patented Aug. l2.: |902.
Nv l lil Ml A2M/4. mf*
THE wams PETER: c., PuoToLrrna. wAsHlNsTou. n. c.
No. 706,979. PatentedAug. I2'. |902.
G. E. MARTIN. comPouNn Am comvnssson.
(Applicativi: medAug. 15, 1901.)
4 Shaets-Sheet .(llo Model.)
wit/neon@ anna/WQ@ TME .scams PETERS C0., FHoTsLmm.. msnmuwn. n. c.
"0.706,979. Patented Aug. I2, |902. G. E. MARTIN. CMPDUND AIR ICUMPRESSR.
(Application led Aug. 15, 1901.) Y Udo Modem' 4 Sheets-Sheet 4.
v 44pm/Lto@ @fw/messes, @l aah/s :Manx/mmm l v E5 att l 1j wm%,7 ,yn-..
Nrrn rares artnr rricn,
GEORGE E. MARTIN, OF PHILADELPHIA, PENNSYLVANIA, ASSIGNOR TO THE PEDRICK AND AYER COMPANY, OF PHILADELPHIA, PENN SYL- VANIA.
COMPOUND AIR-COMPRESSOR SPECIFICATION forming' part 0f Letters Patent NO. 706,979, dated August 12, 1902.
I Application filed August 15, 1901. Serial No. 72,115. (No model.)
To all whom it muy concern:
Be it known that I, GEORGE E. MARTIN, a citizen of the United States, residing at'Philadelphia, in the county of Philadelphia and State of Pennsylvania, have invented certain new and useful Improvements in Compound Air-Compressors, of which the following is a specification, reference being had therein to the accompanying drawings.
This invention relates to improvements in compound air-compressors 5 and it consists in the relative arrangement with the circulating water-jackets that surround the compressioncylinders and valve-chambers of the air-passages and air-receiving chambers, whereby a material reduction of the temperature of the air is maintained under the reduction in its volume, all as hereinafter more particularly described, reference being had to the accompanying drawings, forming a part of this specification, in which- Figure l represents a vertical section of the air-compressor. Fig. 2 is an enlarged vertical section of compression-cylinders on line 2 2 of Fig. 3. Fig. 3 is a top view of cylinder covers and valves. Fig. l is a vertical section through cylinder covers and valves on lines 4 4 i 4 fl. Fig. 5 is a horizontal section through cylinders on line 5 5 of Fig. 2.
The larger compression-cylinder is represented by A and the smaller cylinder by A', and the details of their construction and the operative parts are hereinafter referred to by letters of reference which denote similar detail parts in the respective figures. The operative parts includ`e\t\he main driving-shaft a, provided with the fast-and loose band'- wheels or belt-pulleys l) c, the cranks d e, connecting-rods f g, and pistons 7L t', together with the induction and discharge valves lettered, respectively, j and 7c, all relatively located in a manner common to this type of compressor. The outer shell B includes both the larger and smaller compression-cylinders forming part of the shell of the water-jacket of the larger cylinder and the outer shell of an air-receiving chamber D, that embraces the water-jacket of the smaller cylinder, as shown in plan on the enlarged sectional view, Fig. 5. The inner wall of the air-receiving chamber or cooler D is therefore completely exposed to the circulating waterjackets and its outer wall or shell to the atmosphere, and the temperature of the air is by this construction consequently reduced to the minimum degree possible in the utilization of the cir-u culating water-jackets of the operative cylinders. In this invention it will be observed that a constant cooling effect is produced from Vthe initial compression of the air in the larger cylinder throughout its course through the compressor, and consequently the minimum degree of temperature and maximum efficiency possible in practice are obtained. The effect of this intermediate receiver or intercooler D, whereby the temperature is materially reduced, is to also reduce the volume of air discharged from the larger cylinder, which will `increase the efliciency of the compressor by the admission and manipulation of an increased quantity of air of greater density to the smaller cylinders under a given pressure. This air-receiving chamber or intercooler D is in practice about two and onehalf times larger incapacity than the pistondisplacement in the larger cylinder A, and a constant pressure is maintained therein that will force the confined air through the induction-valves and lill the smaller cylinder A. This pressure from the air-receiver or intercooler D also acts to assist the downward stroke of the smaller piston, and thereby a degree of mechanical work is derived equivalent tothe use of less operative power. Upon the return or compressingstroke of the smaller piston the volume of the conlined air is still further compressed in the usual way, the consequent increase of temperature being checked by the effect of the surrounding water circulation.
The induction and discharge valves j and 7c are located in chambers provided in the top heads of the respective cylinders A A', covered with caps or bonnets m and normally held to their seats by springs n, as shown in the respective figures.
The operation of the compressor may be readily understood from the drawings. By
the first downward movement of the large piston the air enters through the inlet-port 0 and through the air-spaces formed in the cylluder-head, as outlined in the plan view, Fig.
` 3, and passes into the larger cylinder through kthe upward and compression movement of the piston opens the discharge-valve, allowing the air to pass to the receiving-chamber or cooler D. Upon the following downward movement of the piston c' of the smaller cyly inder the airv under compression in the recei ver or intercooler D enters the smaller cylinder through its induction or check valve j, and upon the return or compression movement of the smaller piston the air is discharged through its discharge-valve 7s and passage p to a suitable storage-reservoir.
`The regulation of the operation of the -compressor as to the desired degree of compression and the adjustment of the parts, such as the variable requirements in the tension of the springs Athat maintain the valves in their proper normal position, will be readily understood by those skilled in the manufacture and use of inventions of this character.
What I claim, and desire to secure by Letters Patent, is-
1. A compound air-compressor provided with an air-receiver intermediate of and adjacent to the respective compression-cylinders having its inner wall in contact with the circulating water-jackets of said cylinders, and cooling-jacketsinclosing the connecting air-spaces, whereby the air is in contact with cooled surfaces during the entire period of its passage, as set forth.
2. In a compound air-compressor, an airreceiver intermediate of and adjacent to the respective compression-cylinders having its inner wall in contact with the circulating water-jackets of said cylinders and its outer wall exposed to the atmosphere as set forth.
3. A compound air-compressor having an air-receiver intermediate of the respective compression-cylinders, its inner wall forming the outer surrounding wall of the circulating water-jacket of the smaller cylinder and adjacent wall of the water-jacket of the larger cylinder, as set forth.
In testimony whereof I afx my signature in presence of two witnesses.
GEORGE E. MARTIN.
Witnesses:
THOMAS HEWETT, J. W. RITTER.
US7211501A 1901-08-15 1901-08-15 Compound air-compressor. Expired - Lifetime US706979A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US7211501A US706979A (en) 1901-08-15 1901-08-15 Compound air-compressor.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US7211501A US706979A (en) 1901-08-15 1901-08-15 Compound air-compressor.

Publications (1)

Publication Number Publication Date
US706979A true US706979A (en) 1902-08-12

Family

ID=2775509

Family Applications (1)

Application Number Title Priority Date Filing Date
US7211501A Expired - Lifetime US706979A (en) 1901-08-15 1901-08-15 Compound air-compressor.

Country Status (1)

Country Link
US (1) US706979A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2449408A (en) * 1945-09-13 1948-09-14 Ingersoll Rand Co Compressor
US2547914A (en) * 1946-01-15 1951-04-03 Jaeger Machine Co Cylinder head
US3136477A (en) * 1961-03-28 1964-06-09 Worthington Corp Multi-stage compressor
US3136478A (en) * 1962-04-11 1964-06-09 Worthington Corp Multi-stage compressor with annular ring valve service
US3279382A (en) * 1964-04-14 1966-10-18 Royal Industries Pump
US4035110A (en) * 1975-09-22 1977-07-12 The Bendix Corporation Air compressor cylinder head
US4936109A (en) * 1986-10-06 1990-06-26 Columbia Energy Storage, Inc. System and method for reducing gas compressor energy requirements
DE102004061224A1 (en) * 2004-12-20 2006-06-29 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH Piston-cylinder arrangement, in particular for a swash plate compressor
DE102017106147A1 (en) * 2017-03-22 2018-09-27 Voith Patent Gmbh Reciprocating engine with cooling device

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2449408A (en) * 1945-09-13 1948-09-14 Ingersoll Rand Co Compressor
US2547914A (en) * 1946-01-15 1951-04-03 Jaeger Machine Co Cylinder head
US3136477A (en) * 1961-03-28 1964-06-09 Worthington Corp Multi-stage compressor
US3136478A (en) * 1962-04-11 1964-06-09 Worthington Corp Multi-stage compressor with annular ring valve service
US3279382A (en) * 1964-04-14 1966-10-18 Royal Industries Pump
US4035110A (en) * 1975-09-22 1977-07-12 The Bendix Corporation Air compressor cylinder head
US4936109A (en) * 1986-10-06 1990-06-26 Columbia Energy Storage, Inc. System and method for reducing gas compressor energy requirements
DE102004061224A1 (en) * 2004-12-20 2006-06-29 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH Piston-cylinder arrangement, in particular for a swash plate compressor
DE102004061224B4 (en) * 2004-12-20 2010-09-09 Knorr-Bremse Systeme für Nutzfahrzeuge GmbH Piston-cylinder arrangement, in particular for a swash plate compressor
DE102017106147A1 (en) * 2017-03-22 2018-09-27 Voith Patent Gmbh Reciprocating engine with cooling device
DE102017106147B4 (en) 2017-03-22 2021-10-28 Voith Patent Gmbh Reciprocating machine with cooling device

Similar Documents

Publication Publication Date Title
US706979A (en) Compound air-compressor.
US1135476A (en) Valve for air-compressors.
US938004A (en) Combined air compressor and intercooler.
US173031A (en) Improvement in steam-pumps
US545032A (en) Condensing- pump
US805843A (en) Air or gas compressor.
US354563A (en) Device for cooling the cylinders of compressors for air and other gases
US236992A (en) gushier
US212777A (en) Improvement in double-acting pumps
US1249822A (en) Ice-machine compressor.
US960233A (en) Process of compressing air, gas, or other gaseous fluids.
US174904A (en) Imiprovement in force-pumps
US167568A (en) Improvement in air-engines
US505004A (en) Compound engine
US456643A (en) Engine
US415822A (en) Geant
US283925A (en) Pneumatic compressor
US262864A (en) Air-compressor
US474034A (en) Air-compressor
US610573A (en) wright
US430251A (en) Force-pump
US647883A (en) Compressor for air, &c.
US452537A (en) winklee
US263206A (en) overton
US186336A (en) Improvement in air-compressors