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US2622791A - Two-stage air compressor - Google Patents

Two-stage air compressor Download PDF

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Publication number
US2622791A
US2622791A US65203A US6520348A US2622791A US 2622791 A US2622791 A US 2622791A US 65203 A US65203 A US 65203A US 6520348 A US6520348 A US 6520348A US 2622791 A US2622791 A US 2622791A
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United States
Prior art keywords
cylinder
compression
air
space
high pressure
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Expired - Lifetime
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US65203A
Inventor
Wescombe Hugh Carlisle
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Bristol Pneumatic Tools Ltd
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Bristol Pneumatic Tools Ltd
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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
    • 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
    • F04B39/066Cooling by ventilation

Definitions

  • the invention consists broadly of an air compressor in which air is compressed in two or more stages wherein a mechanically generated air blast, in addition to its utilisation for cooling the air during its passage from a lower pressure cylinder to a higher pressure cylinder by means of an inter-cooler, is directed onto the compression cylinder or cylinders so that cooling is also effected during the actual compression.
  • Figure 1 being a sectional view of the compressor on the line AA of Figure 2
  • Figure 2 is a sectional view on the line B-B of Figure 1
  • Figure 3 is a plan of Figure 2
  • Figure 4 is a section on the line C-C of Figure 2.
  • the numeral l designates the compressor cylinder and 2 is the piston.
  • the piston In Figure 1 the piston is shown at or toward the end of its high compression stroke and in Figure 2 the piston is shown at the end of its low compression stroke.
  • Air which is compressed to comparatively low pressure, for example, some 30 lbs. to the square inch in the top end of the cylinder l enters the cylinder during the high compression stroke through the inlet valve 3 and the air compressed to the required low pressure is discharged through the outlet valve 4 to the inter-cooler 5 by way of the header 6 and passes thence into the high pressure header 6a and thence to the annular high pressure cylinder or chamber 1 through the high pressure inlet valve 8 and after compression to the high pressure, for example some 100/200 lbs.
  • the apparatus in the example shown, is driven by the belt-driven ianwheel l through the usual crank and connecting rod mechanism which needs no description.
  • the fanwheel ID has the usual fan blades II.
  • the inter-cooler which consists of gilled pipes connected up to the headers 6 and 6a by the pipes l2 and connections l2a is arranged in the path of the air-blast coming from the lower part of the fan.
  • the gilled portion of the intercooler coils are disposed substantially semi-circularly in the way of the blast from the lower part of the fanwheel and the gilled portions of the coils, which are spread over as large an area as possible so that all the coils are subject to as much of the cooling blast as possible, terminate well below the compression cylinders, so
  • the number of differential cylinders can be increased.
  • two or three cylinders can be arranged side by side so long as care is exercised in seeing that the blast from the fanwheelor maybe blast from an additional fan-is caused to impinge directly both on the inter-cooler and onto the compression cylinders.
  • the invention is not limited to the specific construction shown and described herein, the characteristic of the invention being the provision of means in a compressor in which air is compressed in two or more stages, whereby a mechanically generated air cooling blast is utilised to cool both the inter-cooler or inter-coolers and the compression cylinder or cylinders.
  • the invention has been particularly described in relation to a two-stage compressor, but of course the same general principles are applicable to cases where more than two stages of compression are employed.
  • one difierential cylinder could effect the first and second stages of compression and another similar but smaller differential cylinder could efiect third and fourth stages of compression with inter-cooling between both the first and second and second and third stages.
  • a two-stage air compressor comprising a single cylinder including a low pressure space at one end and a high pressure space at the other end, a differential piston reciprocable in said cylinder and operable to effect low-stage compression in said low pressure space and highstage compression in said high pressure space, blower means for producing an air blast, and intercooler conduit means communicating with said cylinder spaces for conducting air from the low pressure space to the high pressure space, said cylinder spaces, said blower means and said conduit means being disposed in positions relative one to another in which the air blast of the blower means impinges directly and unobstructedly upon said high pressure cylinder space and said conduit means.
  • a two-stage air compressor comprising a single cylinder including a low pressure space at one end and an annular high pressure space at.
  • a differential piston reciprocable in said cylinder and operable to effect low-stage compression in said lower pressure space and high-stage compression in said high pressure space
  • finned intercooler coils communicating with said cylinder spaces for conducting air from the low pressure space to the high pressure space, substantially the entire finned portion of said coils being disposed in staggered relationship with said cylinder
  • fan means disposed laterally spaced relative to the cylinder and the intercooler coils and arranged to produce an air blast guided to impinge directly and unobstructedly against said high pressure cylinder space and said main portion of the intercooler coils.
  • a two-stage air compressor comprising a single cylinder including a low pressure space at one end and a high pressure annular space at the other end, a difierential piston reciprocable in said cylinder and operable to effect low-stage compression in said low pressure space and highstage compression in said high pressure space,
  • finned intercooler coils communicating at each end with said cylinder spaces for conducting air from the low pressure space to the high pressure space, the main portion of said finned coils being curved to form an open loop, high and low pressure headers communicating with said loop, the general plane of said coil loop and the general plane of said cylinder being positioned substantially plane-parallel one to the other, and fan means mounted laterally spaced relative to the cylinder and the coil 100p and arranged to produce an air blast guided to impinge directly and unobstructedly upon said high pressure cylinder space and said coil loop.
  • a two-stage air compressor comprising a single cylinder, a reciprocable piston having differential efiective areas, said cylinder including a low pressure compression space whose air content is subject to compression by the larger area of said piston and an annular high compression space whose air content is subject to compression by the smaller annular area of said piston, a driving shaft, a crank on one end of said shaft, a connecting rod connecting said crank to said piston, a driving wheel on the end of the shaft remote from the crank, a fan connected with said driving wheel for rotation in unison therewith and positioned to direct its blast on to the high compression zone of the cylinder, and an intercooler comprising coils connected to conduct air compressed in the low pressure compression space of the cylinder to the high pressure compression space of the cylinder, said coils conforming in curvature substantially to the curvature of a part of the fan periphery remote from the cylinder, said intercooler being positioned between the fan and the cylinder position, whereby the blast of cooling air from one part of the fan acts directly and unobst

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressor (AREA)

Description

1952 H, c. WESCOMBE TWO-STAGE AIR COMPRESSOR 2 Sl-IEE'I'S-SHEETl Filed Dec. 14, 1948 Inventor Hue 1 (film m4: WESCONBE BY 3 H- Attorne 2- SHEETSSHEET 2 I LIL H. C. WESCOMBE TWO-STAGE AIR COMPRESSOR Dec. 23, 1952 Filed Dec. 14, 1948 Inventor HUGH C/lRL/JLE Waco/v25 UM Q v \D W M y B.
Patented Dec. 23, 1952 TWO-STAGE AIR COMPRESSOR Hugh Carlisle Wescombe, Bristol, England, as-
signor to Bristol Pneumatic Tools Limited, Bristol, England, a British company Application December 14, 1948, Serial No. 65,203 In Great Britain December 16, 1947 6 Claims.
The invention consists broadly of an air compressor in which air is compressed in two or more stages wherein a mechanically generated air blast, in addition to its utilisation for cooling the air during its passage from a lower pressure cylinder to a higher pressure cylinder by means of an inter-cooler, is directed onto the compression cylinder or cylinders so that cooling is also effected during the actual compression.
In the accompanying drawings the invention is shown applied to a two-stage compressor, Figure 1 being a sectional view of the compressor on the line AA of Figure 2, Figure 2 is a sectional view on the line B-B of Figure 1, Figure 3 is a plan of Figure 2 and Figure 4 is a section on the line C-C of Figure 2.
Referring to these drawings, the numeral l designates the compressor cylinder and 2 is the piston. In Figure 1 the piston is shown at or toward the end of its high compression stroke and in Figure 2 the piston is shown at the end of its low compression stroke. Air which is compressed to comparatively low pressure, for example, some 30 lbs. to the square inch in the top end of the cylinder l enters the cylinder during the high compression stroke through the inlet valve 3 and the air compressed to the required low pressure is discharged through the outlet valve 4 to the inter-cooler 5 by way of the header 6 and passes thence into the high pressure header 6a and thence to the annular high pressure cylinder or chamber 1 through the high pressure inlet valve 8 and after compression to the high pressure, for example some 100/200 lbs. to the square inch, is discharged through the high pressure outlet valve 9 to the receiver (not shown) in conventional manner which will be readily understood by those skilled in the art. The apparatus, in the example shown, is driven by the belt-driven ianwheel l through the usual crank and connecting rod mechanism which needs no description. The fanwheel ID has the usual fan blades II. The inter-cooler which consists of gilled pipes connected up to the headers 6 and 6a by the pipes l2 and connections l2a is arranged in the path of the air-blast coming from the lower part of the fan. As will be best seen on reference to Figure 4 the gilled portion of the intercooler coils are disposed substantially semi-circularly in the way of the blast from the lower part of the fanwheel and the gilled portions of the coils, which are spread over as large an area as possible so that all the coils are subject to as much of the cooling blast as possible, terminate well below the compression cylinders, so
2 that the inter-cooler ofiers no interference with the blast from the top of the fan which thus impinges directly on the cylinder wall and cools the air compressed in the cylinder during both stages of compression but particularly during the high compression stage.
It is to be understood that where high output is required, the number of differential cylinders can be increased. For example, two or three cylinders can be arranged side by side so long as care is exercised in seeing that the blast from the fanwheelor maybe blast from an additional fan-is caused to impinge directly both on the inter-cooler and onto the compression cylinders.
It will also be understood that the invention is not limited to the specific construction shown and described herein, the characteristic of the invention being the provision of means in a compressor in which air is compressed in two or more stages, whereby a mechanically generated air cooling blast is utilised to cool both the inter-cooler or inter-coolers and the compression cylinder or cylinders.
The invention has been particularly described in relation to a two-stage compressor, but of course the same general principles are applicable to cases where more than two stages of compression are employed. Thus one difierential cylinder could effect the first and second stages of compression and another similar but smaller differential cylinder could efiect third and fourth stages of compression with inter-cooling between both the first and second and second and third stages.
I claim:
1. A two-stage air compressor comprising a single cylinder including a low pressure space at one end and a high pressure space at the other end, a differential piston reciprocable in said cylinder and operable to effect low-stage compression in said low pressure space and highstage compression in said high pressure space, blower means for producing an air blast, and intercooler conduit means communicating with said cylinder spaces for conducting air from the low pressure space to the high pressure space, said cylinder spaces, said blower means and said conduit means being disposed in positions relative one to another in which the air blast of the blower means impinges directly and unobstructedly upon said high pressure cylinder space and said conduit means.
2. A two-stage air compressor comprising a single cylinder including a low pressure space at one end and an annular high pressure space at.
the other end, a differential piston reciprocable in said cylinder and operable to effect low-stage compression in said lower pressure space and high-stage compression in said high pressure space, finned intercooler coils communicating with said cylinder spaces for conducting air from the low pressure space to the high pressure space, substantially the entire finned portion of said coils being disposed in staggered relationship with said cylinder, and fan means disposed laterally spaced relative to the cylinder and the intercooler coils and arranged to produce an air blast guided to impinge directly and unobstructedly against said high pressure cylinder space and said main portion of the intercooler coils.
3. An air compressor as described in claim 2, wherein said cylinder is vertically disposed, and wherein the main portion of said finned intercooler coils is positioned below the level of the lower end of the cylinder.
4. An air compressor as described in claim 2, wherein said piston has two opposite faces with different effective areas, the face with the larger effective area facing the said low pressure space and the face with the smaller effective area facing the said high pressure space, said latter space forming an annular ring space encompassing and concentric with a portion of said piston.
5. A two-stage air compressor comprising a single cylinder including a low pressure space at one end and a high pressure annular space at the other end, a difierential piston reciprocable in said cylinder and operable to effect low-stage compression in said low pressure space and highstage compression in said high pressure space,
finned intercooler coils communicating at each end with said cylinder spaces for conducting air from the low pressure space to the high pressure space, the main portion of said finned coils being curved to form an open loop, high and low pressure headers communicating with said loop, the general plane of said coil loop and the general plane of said cylinder being positioned substantially plane-parallel one to the other, and fan means mounted laterally spaced relative to the cylinder and the coil 100p and arranged to produce an air blast guided to impinge directly and unobstructedly upon said high pressure cylinder space and said coil loop.
6. A two-stage air compressor comprising a single cylinder, a reciprocable piston having differential efiective areas, said cylinder including a low pressure compression space whose air content is subject to compression by the larger area of said piston and an annular high compression space whose air content is subject to compression by the smaller annular area of said piston, a driving shaft, a crank on one end of said shaft, a connecting rod connecting said crank to said piston, a driving wheel on the end of the shaft remote from the crank, a fan connected with said driving wheel for rotation in unison therewith and positioned to direct its blast on to the high compression zone of the cylinder, and an intercooler comprising coils connected to conduct air compressed in the low pressure compression space of the cylinder to the high pressure compression space of the cylinder, said coils conforming in curvature substantially to the curvature of a part of the fan periphery remote from the cylinder, said intercooler being positioned between the fan and the cylinder position, whereby the blast of cooling air from one part of the fan acts directly and unobstructedly on to the cylinder wall and from another part of the fan directly and unobstructedly on to the intercooler coils.
HUGH CARLISLE WESCOMBE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 1,450,032 Gardner Mar. 27, 1923 1,467,489 Nodberg Sept. 11, 1923 1,520,852 Cable Dec. 30, 1924 1,535,856 Rix Apr. 28, 1925 1,622,876 Leo Mar. 29, 1927 1,694,218 Hazard Dec. 4, 1928 1,747,457 Putnam Feb. 18, 1930
US65203A 1947-12-16 1948-12-14 Two-stage air compressor Expired - Lifetime US2622791A (en)

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899130A (en) * 1959-08-11 Compressor
US3075690A (en) * 1960-04-18 1963-01-29 Emerson Electric Mfg Co Enclosed transmission mechanism
US4391568A (en) * 1978-06-20 1983-07-05 Tenney William L Gas compressor
US4536132A (en) * 1981-02-25 1985-08-20 London Fog, Inc. Gas compressor
CN111306036A (en) * 2020-03-12 2020-06-19 中国船舶重工集团公司第七0三研究所 Air compressor applied to gas turbine

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1450032A (en) * 1919-09-23 1923-03-27 Gardner Governor Company Compressor mechanism
US1467489A (en) * 1918-08-12 1923-09-11 Bruno V Nordberg Compressor
US1520852A (en) * 1920-06-30 1924-12-30 Electric Boat Co Air-compressor piston
US1535856A (en) * 1924-05-15 1925-04-28 Edward A Rix Combination air compressor and vacuum pump
US1622876A (en) * 1925-06-13 1927-03-29 Leo Hermann Air pump
US1694218A (en) * 1924-06-11 1928-12-04 Kellogg Mfg Co Air-compressing mechanism
US1747457A (en) * 1927-02-07 1930-02-18 Rhoda S Dunlap Compressor

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1467489A (en) * 1918-08-12 1923-09-11 Bruno V Nordberg Compressor
US1450032A (en) * 1919-09-23 1923-03-27 Gardner Governor Company Compressor mechanism
US1520852A (en) * 1920-06-30 1924-12-30 Electric Boat Co Air-compressor piston
US1535856A (en) * 1924-05-15 1925-04-28 Edward A Rix Combination air compressor and vacuum pump
US1694218A (en) * 1924-06-11 1928-12-04 Kellogg Mfg Co Air-compressing mechanism
US1622876A (en) * 1925-06-13 1927-03-29 Leo Hermann Air pump
US1747457A (en) * 1927-02-07 1930-02-18 Rhoda S Dunlap Compressor

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899130A (en) * 1959-08-11 Compressor
US3075690A (en) * 1960-04-18 1963-01-29 Emerson Electric Mfg Co Enclosed transmission mechanism
US4391568A (en) * 1978-06-20 1983-07-05 Tenney William L Gas compressor
US4536132A (en) * 1981-02-25 1985-08-20 London Fog, Inc. Gas compressor
CN111306036A (en) * 2020-03-12 2020-06-19 中国船舶重工集团公司第七0三研究所 Air compressor applied to gas turbine

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