US2576876A - Compressor - Google Patents

Compressor Download PDF

Info

Publication number
US2576876A
US2576876A US786515A US78651547A US2576876A US 2576876 A US2576876 A US 2576876A US 786515 A US786515 A US 786515A US 78651547 A US78651547 A US 78651547A US 2576876 A US2576876 A US 2576876A
Authority
US
United States
Prior art keywords
air
manifold
cylinder
compressor
cylinder head
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
US786515A
Inventor
Harold R Gamble
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.)
DeVilbiss Co
Original Assignee
DeVilbiss 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 DeVilbiss Co filed Critical DeVilbiss Co
Priority to US786515A priority Critical patent/US2576876A/en
Application granted granted Critical
Publication of US2576876A publication Critical patent/US2576876A/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

  • This invention relates to a V-type compressor and particularly to air inlet and outlet manifolds therefor.
  • the primary object of the invention is to provide a well balanced structure that is compact in design.
  • Another object is the provision of manifolds which are adaptable for use with either single or double stage compression.
  • a further object is the provision of a fastening arrangement that compensates for machining variations.
  • Another object is the provision of effective cooling means.
  • a still further object is the provision of an air inlet midwa between the air cylinders, and an inlet structure that reduces the compressor operating 'noise.
  • an air inlet manifold connected at each end with a cylinder head and with an air inlet opening on its top center portion.
  • This manifold has cooling fins extending laterally therefrom.
  • Its fastening means have flanged cylinder head-joining surfaces lying in a plane at each end parallel to the axis of the compressor cylinder and the fastening means are tubular for the transmission of air to the cylinder heads.
  • a horizontally disposed air manifold for cooling the air under first stage compression. This has upwardly bent andsubsequently downwardly turned connecting tubular portions for joining the manifold to the cylinder heads at locations alongside of those to which the inlet manifold is fastened.
  • Figure 1 is a side elevation of a compressor embodying my design with portions thereof shown invertical section;
  • Figure 2 is a plan view of the compressor shown in Figure 1 with a portion of the air inlet shown in horizontal section;
  • Figure 3 is a plan view of the secondary air outlet manifold
  • Figure 4 is a fragmentary vertical section of the connection between the inlet manifold and the cylinder head of the cylinder on the left side of the compressor shown in Figures 1 and 2.
  • crankcase Upon this crankcase as a supporting base are mounted cylinders 4 and 5.
  • Bothcylinders When used as a two-stage unit the larger cylinder 5 provides the initial compression of the air.
  • Bothcylinders include a conventional piston 6 with a connecting rod i.
  • cylinder heads 8 and 9 Within the heads are inlet and exhaust valves.
  • One of the former is shown at H in Figure 1.
  • caps ll, I2, I 3 and M Upon the heads are caps ll, I2, I 3 and M for holding the inlet and exhaust valve assemblies in place.
  • the compressor has, on the end of the crankshaft 40, a standard fly wheel or pulley I5 with vane-type spokes It to direct air against the cylinders, cylinder heads and air manifolds, all of which have cooling fins.
  • an air intake finned manifold I! having a circular cavity It at its center to which a lateral tubular extension l9 connects.
  • This extension terminates with a flange 20 by which it is fastened to a complementary flange 2
  • a passage 22 leads to the air inlet valve Iii.
  • a second tubular extension 23 joins the manifold with the other cylinder head.
  • the connecting extensions 19 and 23 are on opposite sides of the lengthwise center line of the manifold ll.
  • the larger cylinder 5 compresses all of the air initially and the cylinder head 8 does not receive air directly from the intake manifold 11 as the travel of air through the tubular extension 23 is prevented by plugging, with a threaded plug 39 as illustrated in Figure 4, the receiving passage in the cylinder head communicating with the extension.
  • a conical partition 24 Spanning the center cavity I8 is a conical partition 24 ported at its apex to receive the upper end of tube 25.
  • the edge of partition 24 is supported upon an annular shoulder 26, an integral part of the inlet manifold casting.
  • a cylindrical filter screen 21 Over the partition is positioned a cylindrical filter screen 21. Its vertical wall section stands on the edge of the partition within an annular lip 28 on the manifold casting.
  • a cover 29 lies over the upper end of the filter 2?.
  • a bolt 30 which passes from the under side of the manifold into the center of the cavity I 8, through the tube 25, and through the cover 29 cooperates with a thumb nut 3
  • the entering air is drawn inwardly through the filter screen '27 and passes downwardly through the central tube 25 into cavity l8.
  • the arrangement of the partition 24 cooperates with the tube and the cavity to absorb the compressor operating noise generally escaping through the air inlet.
  • the tangential connections between the cavity and the tubular extensions l9 and 23 may also contribute to the sound deadening results obtained with this structure.
  • the air filtering and sound deadening air inlet structure is not a part of this invention, being the subject of application Ser. No. 46,052 filed August 25, 1948, and which issued as U. S. Patent No. 2,564,814 to the assignee of this application.
  • a second finned air manifold 32 for compressed air is suspended between the cylinder heads by flanged elbows 33 and 34.
  • the connections 33 and 34 are on opposite sides of the lengthwise center line of manifold 32.
  • the elbow 34 communicates with the exhaust outlet of cylinder head 9.
  • the air from head 9 travels through the S passage 35 of the manifold through elbow 33 to the intake valve of cylinder head 8. From here it enters the compressing chamber of cylinder 4 where it is compressed to a higher pressure, before being discharged through the exhaust valve to outlet 36.
  • both cylinders When it is desired to use both cylinders for compressing atmospheric air instead of in series for two stage operation, the intake air passes to both cylinder heads from the cavity l8 and after being compressed enters the manifold 32 from the exhaust valves.
  • the positions of the exhaust and inlet valve assemblies of cylinder head 8 must be interchanged and the opening into the head 3 from the intake manifold opened.
  • the outlet 36 is closed with a pipe plug. The air after reaching the manifold 32, travels therefrom out opening 31 to reach the air tank or other receiving means.
  • the plug 38 shown in Figure 3, which closes this opening during two stage operation may be used to close outlet 36 for single stage compression.
  • the air inlet manifold ll delivers air only to the first stage cylinder head 9 and the lower manifold delivers air from cylinder head 9 to the cylinder head 8 of the other cylinder.
  • the air passing into the inlet manifold 11 travels to both cylinder heads and is delivered from both heads back into manifold 32 which then acts as an after cooler.
  • the cooling air form the fly wheel travels through the horizontal space between the manifolds as well as through the vertical openings 4
  • the manifolds l1 and 32 present substantial cooling surfaces as they are as wide as either cylinder head.
  • the vertical height of each manifold is limted, being less than half the width of the manifold. This permits them to fit compactly one above the other between the opposing or mutually facing sides of the cylinder heads with the lower portion of the upper air intake manifold lying horizontally below the uppermost portions of the cylinder heads.
  • the air inlet manifold in addition to its utility in distributing air and in sound deadening also contributes to the efiective operation of the compressor by assisting in the dissipation of heat as the latter travels from the cylinder heads through the walls of connecting tubular portions of the manifold and is carried off the outer surface of the manifold by the air from the flywheel.
  • this invention provides a structure that is particularly effective in quieting the sound of operation and in dispersing the heat of compression.
  • a crankcase providing a supporting base for the compressor, two upwardly diverging cylinders mounted on the crankcase, a cylinder head on the top of each cylinder, air inlet and exhaust valves in each cylinder head, a crankshaft extending horizontally from the crankcase on one side of the cylinders, a pulley on the exterior end of the crankshaft, vane type spokes on the pulley directing cooling air between and around the cylinders and cylinder heads, cooling fins on the cylinders and cylinder heads, a finned air intake manifold spanning the space between the cylinder heads, said manifold having at its center a large upwardl facing circular opening, an air filter between the atmosphere and the opening, a finned compressed air manifold below the air intake manifold extending between the cylinder heads, and connections joining said manifolds with the cylinder heads, the contacting surfaces between the connections and each cylinder head lying in a plane parallel to the axis of the cylinder upon which the cylinder
  • crankcase providing a supporting base for the compressor, two upwardly diverging cylinders mounted on the crankcase, a valved cylinder head on the top of each cylinder, a crankshaft extending horizontally from the crankcase on one side of the cylinders, a.
  • a finned air intake manifold extending directly and horizontally between the cylinder heads with its lower portion below the uppermost portions of the cylinder heads, said intake manifold being horizontally broadened to an extent whereby it is more than twice as broad as vertically thick, said manifold having a large upwardly facing air inlet opening, a similarly broadened finned compressed air manifold extending horizontally between the cylinder heads and positioned adjacently below the intake manifold and completely below the uppermost portions of the cylinder heads, and connections at the ends of the manifolds joining them to the mutually facing sides of the cylinder heads,,said manifolds being thus compactly placed between the cylinder heads in the path of cooling air from the pulley.
  • connection of each manifold to a cylinder head is on the opposite side of the lengthwise center line of the manifold from the connection of the manifold to the other cylinder head.
  • An air compressor as set forth in claim 2 in which the compressed air manifold is shaped to provide an interior S-shaped passage for the compressed air and there are spaced vertical webs extending exteriorly between the convolutions forming the S-shaped passage, the openings between the webs providing an upward path for the cooling air from the pulley.

Description

Nov. 27, 1951 H. R. GAMBLE 2,576,876
COMPRESSOR Filed Nov. 17, 1947 2 SHEETS--SHEET 1 llllllik- 8 0 0::- 6 a AW 36 5 INVENTOR flm ow R swam ATTORNEY Nov. 27, 1951 GAMBLE 2576 876 COMPRESSOR Filed NOV. 17, 1947 2 SHEETS-SHEET 2 4| 42 4| 42 34 37 L f A 41 I o v 1 5 0 o 1123 a 1n Fit g. 3
INVENTOR 659mm R2 Gan-m6 ATTORNEY Patented Nov. 27, 1951 COMPRESSOR Harold R. Gamble, Toledo, hio, assignor to The De Vilbiss Company, Toledo, Ohio, a corporation of Ohio Application November 17, 1947, Serial No. 786,515
Claims.
This invention relates to a V-type compressor and particularly to air inlet and outlet manifolds therefor.
The primary object of the invention is to provide a well balanced structure that is compact in design.
Another object is the provision of manifolds which are adaptable for use with either single or double stage compression.
A further object is the provision of a fastening arrangement that compensates for machining variations.
Another object is the provision of effective cooling means.
A still further object is the provision of an air inlet midwa between the air cylinders, and an inlet structure that reduces the compressor operating 'noise.
These-and other objects, which will become apparent upon reading the following description, are attained through the use of an air inlet manifold connected at each end with a cylinder head and with an air inlet opening on its top center portion. This manifold has cooling fins extending laterally therefrom. Its fastening means have flanged cylinder head-joining surfaces lying in a plane at each end parallel to the axis of the compressor cylinder and the fastening means are tubular for the transmission of air to the cylinder heads.
Below the intake manifold is a horizontally disposed air manifold for cooling the air under first stage compression. This has upwardly bent andsubsequently downwardly turned connecting tubular portions for joining the manifold to the cylinder heads at locations alongside of those to which the inlet manifold is fastened.
These and additional features will be more fully explained hereafter.
In the drawings:
Figure 1 is a side elevation of a compressor embodying my design with portions thereof shown invertical section;
Figure 2 is a plan view of the compressor shown in Figure 1 with a portion of the air inlet shown in horizontal section; and
Figure 3 is a plan view of the secondary air outlet manifold;
Figure 4 is a fragmentary vertical section of the connection between the inlet manifold and the cylinder head of the cylinder on the left side of the compressor shown in Figures 1 and 2.
The embodiment of this invention illustrated in the drawings includes an air compressor crankcase I. with end plate 2 and oil filling attachment 3.
2. Upon this crankcase as a supporting base are mounted cylinders 4 and 5.
When used as a two-stage unit the larger cylinder 5 provides the initial compression of the air. Bothcylinders include a conventional piston 6 with a connecting rod i. Upon the cylinders are mounted cylinder heads 8 and 9. Within the heads are inlet and exhaust valves. One of the former is shown at H in Figure 1. Upon the heads are caps ll, I2, I 3 and M for holding the inlet and exhaust valve assemblies in place.
The compressor has, on the end of the crankshaft 40, a standard fly wheel or pulley I5 with vane-type spokes It to direct air against the cylinders, cylinder heads and air manifolds, all of which have cooling fins.
Between the cylinder heads is mounted an air intake finned manifold I! having a circular cavity It at its center to which a lateral tubular extension l9 connects. This extension terminates with a flange 20 by which it is fastened to a complementary flange 2| on the cylinder head 9. From the flange connection 2| on the cylinder head a passage 22 leads to the air inlet valve Iii. From the other side of the cavity a second tubular extension 23 joins the manifold with the other cylinder head. The connecting extensions 19 and 23 are on opposite sides of the lengthwise center line of the manifold ll.
When the compressor is operated as a two stage unit the larger cylinder 5 compresses all of the air initially and the cylinder head 8 does not receive air directly from the intake manifold 11 as the travel of air through the tubular extension 23 is prevented by plugging, with a threaded plug 39 as illustrated in Figure 4, the receiving passage in the cylinder head communicating with the extension.
Spanning the center cavity I8 is a conical partition 24 ported at its apex to receive the upper end of tube 25. The edge of partition 24 is supported upon an annular shoulder 26, an integral part of the inlet manifold casting. Over the partition is positioned a cylindrical filter screen 21. Its vertical wall section stands on the edge of the partition within an annular lip 28 on the manifold casting. A cover 29 lies over the upper end of the filter 2?. A bolt 30 which passes from the under side of the manifold into the center of the cavity I 8, through the tube 25, and through the cover 29 cooperates with a thumb nut 3| which is threaded to the bolt at its upper end to hold the cover, filter and partition in assembled relation.
The entering air is drawn inwardly through the filter screen '27 and passes downwardly through the central tube 25 into cavity l8. The arrangement of the partition 24 cooperates with the tube and the cavity to absorb the compressor operating noise generally escaping through the air inlet. The tangential connections between the cavity and the tubular extensions l9 and 23 may also contribute to the sound deadening results obtained with this structure. The air filtering and sound deadening air inlet structure is not a part of this invention, being the subject of application Ser. No. 46,052 filed August 25, 1948, and which issued as U. S. Patent No. 2,564,814 to the assignee of this application.
Below the air intake manifold I! is positioned a second finned air manifold 32 for compressed air. This is suspended between the cylinder heads by flanged elbows 33 and 34. The connections 33 and 34 are on opposite sides of the lengthwise center line of manifold 32.
The elbow 34 communicates with the exhaust outlet of cylinder head 9. When the compressor is operating for two stage compression the air from head 9 travels through the S passage 35 of the manifold through elbow 33 to the intake valve of cylinder head 8. From here it enters the compressing chamber of cylinder 4 where it is compressed to a higher pressure, before being discharged through the exhaust valve to outlet 36.
When it is desired to use both cylinders for compressing atmospheric air instead of in series for two stage operation, the intake air passes to both cylinder heads from the cavity l8 and after being compressed enters the manifold 32 from the exhaust valves. For this use the positions of the exhaust and inlet valve assemblies of cylinder head 8 must be interchanged and the opening into the head 3 from the intake manifold opened. Also the outlet 36 is closed with a pipe plug. The air after reaching the manifold 32, travels therefrom out opening 31 to reach the air tank or other receiving means. The plug 38 shown in Figure 3, which closes this opening during two stage operation may be used to close outlet 36 for single stage compression.
It may be noted therefore that when the compressor is used for two stage operation, the air inlet manifold ll delivers air only to the first stage cylinder head 9 and the lower manifold delivers air from cylinder head 9 to the cylinder head 8 of the other cylinder.
Alternately when the compressor is operated for single stage compression, the air passing into the inlet manifold 11 travels to both cylinder heads and is delivered from both heads back into manifold 32 which then acts as an after cooler.
While the compressor shown in the drawings and discussed herein, is particularly adapted for two stage operation and would not ordinarily be used for single stage, it is here treated as serving in either manner in order to better point out the features of the invention.
The cooling air form the fly wheel travels through the horizontal space between the manifolds as well as through the vertical openings 4| between webs 42 which are exteriorly between the curves of the S-shaped passage in the lower manifold.
The manifolds l1 and 32 present substantial cooling surfaces as they are as wide as either cylinder head. The vertical height of each manifold is limted, being less than half the width of the manifold. This permits them to fit compactly one above the other between the opposing or mutually facing sides of the cylinder heads with the lower portion of the upper air intake manifold lying horizontally below the uppermost portions of the cylinder heads.
Because of machining discrepancies in the joining portions of the crankcase and the cylinders and between the cylinders and the heads, there may be some variation in the distance between the cylinder heads. In order to compensatefor such variation the contacting surfaces between each cylinder head and the flanged elbow connections joining the manifolds to the heads are disposed in a plane parallel with the axis of the cylinder on which the cylinder head is mounted. This parallel relationship may be noted by referring to the joint lines 43 in Figures 1 and 2. This arrangement permits the manifold to slide downwardly into a tight connection with the heads whether the distance between the heads is somewhat greater or less than that specified in production drawings. This, of course, would not be possible were the contacting surfaces in vertical planes. The bolt holes in the attaching flanges are oversize to permit entry of the bolts when the flanges are somewhat out of line.
The air inlet manifold in addition to its utility in distributing air and in sound deadening also contributes to the efiective operation of the compressor by assisting in the dissipation of heat as the latter travels from the cylinder heads through the walls of connecting tubular portions of the manifold and is carried off the outer surface of the manifold by the air from the flywheel.
It may thus be seen that this invention provides a structure that is particularly effective in quieting the sound of operation and in dispersing the heat of compression.
While simple in design the arrangement is suitable with minor alterations for both single and two stage compression. And, as has been brought out, the construction is confined to a minimum of space while retaining a maximum of eificient cooperation in functions.
Various changes and modifications could be made without departing from the spirit and scope of the invention and it is intended to cover such variations within the field of the accompanying claims.
What I claim is:
1. In an air compressor, a crankcase providing a supporting base for the compressor, two upwardly diverging cylinders mounted on the crankcase, a cylinder head on the top of each cylinder, air inlet and exhaust valves in each cylinder head, a crankshaft extending horizontally from the crankcase on one side of the cylinders, a pulley on the exterior end of the crankshaft, vane type spokes on the pulley directing cooling air between and around the cylinders and cylinder heads, cooling fins on the cylinders and cylinder heads, a finned air intake manifold spanning the space between the cylinder heads, said manifold having at its center a large upwardl facing circular opening, an air filter between the atmosphere and the opening, a finned compressed air manifold below the air intake manifold extending between the cylinder heads, and connections joining said manifolds with the cylinder heads, the contacting surfaces between the connections and each cylinder head lying in a plane parallel to the axis of the cylinder upon which the cylinder head is mounted.
2. In an air compressor, a crankcase providing a supporting base for the compressor, two upwardly diverging cylinders mounted on the crankcase, a valved cylinder head on the top of each cylinder, a crankshaft extending horizontally from the crankcase on one side of the cylinders, a. pulley on the exterior end of the crankshaft, vane-type spokes on the pulley directing cooling air between and around the cylinders and cylinder heads, a finned air intake manifold extending directly and horizontally between the cylinder heads with its lower portion below the uppermost portions of the cylinder heads, said intake manifold being horizontally broadened to an extent whereby it is more than twice as broad as vertically thick, said manifold having a large upwardly facing air inlet opening, a similarly broadened finned compressed air manifold extending horizontally between the cylinder heads and positioned adjacently below the intake manifold and completely below the uppermost portions of the cylinder heads, and connections at the ends of the manifolds joining them to the mutually facing sides of the cylinder heads,,said manifolds being thus compactly placed between the cylinder heads in the path of cooling air from the pulley.
3. An air compressor as set forth in claim 2 in which the manifolds are as wide as either cylinder head.
4. An air compressor as set forth in claim 2 in which the connection of each manifold to a cylinder head is on the opposite side of the lengthwise center line of the manifold from the connection of the manifold to the other cylinder head.
5. An air compressor as set forth in claim 2 in which the compressed air manifold is shaped to provide an interior S-shaped passage for the compressed air and there are spaced vertical webs extending exteriorly between the convolutions forming the S-shaped passage, the openings between the webs providing an upward path for the cooling air from the pulley.
HAROLD R. GAMBLE.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 317,629 Conacher May 12, 1885 397,780 Conacher Feb. 12, 1889 410,456 Shuls Sept. 3, 1889 1,004,278 Klein Sept. 26, 1911 1,024,919 Waterous Apr. 30, 1912 1,360,910 Fischbacher Nov. 30, 1920 1,369,618 Christensen Feb. 22, 1921 1,685,150 Davey et al Sept. 25, 1928 1,846,656 Rayfield Feb. 23, 1932 2,030,759 Neal Feb. 11, 1936 2,141,057 Whiles Dec. 20, 1938 2,403,814 Maniscalco July 9, 1946 2,564,814 Perrin Aug. 21, 1951
US786515A 1947-11-17 1947-11-17 Compressor Expired - Lifetime US2576876A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US786515A US2576876A (en) 1947-11-17 1947-11-17 Compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US786515A US2576876A (en) 1947-11-17 1947-11-17 Compressor

Publications (1)

Publication Number Publication Date
US2576876A true US2576876A (en) 1951-11-27

Family

ID=25138813

Family Applications (1)

Application Number Title Priority Date Filing Date
US786515A Expired - Lifetime US2576876A (en) 1947-11-17 1947-11-17 Compressor

Country Status (1)

Country Link
US (1) US2576876A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3031131A (en) * 1957-03-06 1962-04-24 Joy Mfg Co Compressor
US3109584A (en) * 1963-11-05 Compressor muffler construction and method for
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
US3193193A (en) * 1958-03-13 1965-07-06 Carrier Corp Compressor muffler construction and method for muffling compressor discharge gases
US5020973A (en) * 1986-04-25 1991-06-04 The Scott & Fetzer Company Air compressor shroud
US6287085B1 (en) * 2000-01-26 2001-09-11 Westinghouse Air Brake Company Rapid unloader retrofits
WO2013070330A1 (en) * 2011-11-10 2013-05-16 Gardner Denver, Inc. Retrofit of a reciprocating compressor with a concentric valve
WO2018000070A1 (en) 2016-06-30 2018-01-04 Schulz S/A Two stage air compressor

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US317629A (en) * 1885-05-12 Refrigerating apparatus
US397780A (en) * 1889-02-12 Air-pump
US410456A (en) * 1889-09-03 shuls
US1004278A (en) * 1910-06-08 1911-09-26 Daniel Klein Air-pump.
US1024919A (en) * 1910-12-21 1912-04-30 Frederick L Waterous Pump.
US1360910A (en) * 1919-07-30 1920-11-30 American Sanitary Refrigeratio Compressor for refrigerating-machines
US1369618A (en) * 1921-02-22 Motor-compressor
US1685150A (en) * 1924-03-31 1928-09-25 Davey Tree Expert Company Air compressor
US1846656A (en) * 1929-11-15 1932-02-23 Champion Pneumatic Machinery C Single stage compressor
US2030759A (en) * 1934-01-09 1936-02-11 Neal Bob Compressor unit
US2141057A (en) * 1937-09-13 1938-12-20 Virgil Scott Gas compressor
US2403814A (en) * 1942-02-17 1946-07-09 Maniscalco Pictro Compressor
US2564814A (en) * 1948-08-25 1951-08-21 Vilbiss Co Air cleaner and silencer

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1369618A (en) * 1921-02-22 Motor-compressor
US397780A (en) * 1889-02-12 Air-pump
US410456A (en) * 1889-09-03 shuls
US317629A (en) * 1885-05-12 Refrigerating apparatus
US1004278A (en) * 1910-06-08 1911-09-26 Daniel Klein Air-pump.
US1024919A (en) * 1910-12-21 1912-04-30 Frederick L Waterous Pump.
US1360910A (en) * 1919-07-30 1920-11-30 American Sanitary Refrigeratio Compressor for refrigerating-machines
US1685150A (en) * 1924-03-31 1928-09-25 Davey Tree Expert Company Air compressor
US1846656A (en) * 1929-11-15 1932-02-23 Champion Pneumatic Machinery C Single stage compressor
US2030759A (en) * 1934-01-09 1936-02-11 Neal Bob Compressor unit
US2141057A (en) * 1937-09-13 1938-12-20 Virgil Scott Gas compressor
US2403814A (en) * 1942-02-17 1946-07-09 Maniscalco Pictro Compressor
US2564814A (en) * 1948-08-25 1951-08-21 Vilbiss Co Air cleaner and silencer

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3109584A (en) * 1963-11-05 Compressor muffler construction and method for
US3031131A (en) * 1957-03-06 1962-04-24 Joy Mfg Co Compressor
US3193193A (en) * 1958-03-13 1965-07-06 Carrier Corp Compressor muffler construction and method for muffling compressor discharge gases
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
US5020973A (en) * 1986-04-25 1991-06-04 The Scott & Fetzer Company Air compressor shroud
US6287085B1 (en) * 2000-01-26 2001-09-11 Westinghouse Air Brake Company Rapid unloader retrofits
WO2013070330A1 (en) * 2011-11-10 2013-05-16 Gardner Denver, Inc. Retrofit of a reciprocating compressor with a concentric valve
US20130121860A1 (en) * 2011-11-10 2013-05-16 Gene Bluhm Retrofit of a reciprocating compressor with a concentric valve
WO2018000070A1 (en) 2016-06-30 2018-01-04 Schulz S/A Two stage air compressor
CN109891094A (en) * 2016-06-30 2019-06-14 舒尔茨压缩机有限责任股份公司 Two-stage air compressor
CN109891094B (en) * 2016-06-30 2020-10-30 舒尔茨压缩机有限责任股份公司 Two-stage air compressor
US11187218B2 (en) 2016-06-30 2021-11-30 Schulz Compressores Ltda Two stage air compressor

Similar Documents

Publication Publication Date Title
US2576876A (en) Compressor
US2257631A (en) Internal combustion engine
GB2097866A (en) Muffler system for refrigeration compressor
US2789662A (en) Air intake device for engines
DE3921662C1 (en)
US2229119A (en) Venturi silencer
CN107228061B (en) Air compressor of body cooling integration
US1846656A (en) Single stage compressor
US1846655A (en) Compressor
US2067253A (en) Engine exhaust system
US2702534A (en) Crankcase ventilation
US2578146A (en) Compressor
US1493935A (en) Compressor
US3530648A (en) Combined air-filter and induction silencer
US1890794A (en) Internal combustion engine of the oppositely-moving piston type
US2084670A (en) Fluid compressor
US1746394A (en) Multistage compressor
DE514131C (en) Device on multi-cylinder four-stroke internal combustion engines with discharge and suction device on the discharge line
US1738121A (en) Engine compressor
US2557236A (en) Mounting for combination air cleaner and carburetor silencer
US2764961A (en) Intake manifold structure
US1623388A (en) Fornia
US1787856A (en) Two-cycle-engine construction
DE919533C (en) Silencer arrangement for refrigeration machines
SU5416A1 (en) Engine compound internal combustion