US1122085A - Compressor. - Google Patents
Compressor. Download PDFInfo
- Publication number
- US1122085A US1122085A US79410413A US1913794104A US1122085A US 1122085 A US1122085 A US 1122085A US 79410413 A US79410413 A US 79410413A US 1913794104 A US1913794104 A US 1913794104A US 1122085 A US1122085 A US 1122085A
- Authority
- US
- United States
- Prior art keywords
- cylinders
- shaft
- compressors
- sleeve
- cam
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
- F16H25/08—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for interconverting rotary motion and reciprocating motion
- F16H25/12—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for interconverting rotary motion and reciprocating motion with reciprocation along the axis of rotation, e.g. gearings with helical grooves and automatic reversal or cams
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18056—Rotary to or from reciprocating or oscillating
- Y10T74/18296—Cam and slide
- Y10T74/18304—Axial cam
- Y10T74/18312—Grooved
Definitions
- the invention relatesto animproveinent in compressors and particularly to a means for operating ya series of compressors in an even an uniform manner.
- Figi'ire 1 is a longitudinal sectional view showing two compressors coupled tothe im# provedA operating means.
- Fig. 2 is an end elevationv of the saine.
- Fig. is a trans-' the cam vsleeve is correspondingly rotated Awith the effect to reciprocate the pistons Vwithin the cylinders for the desired-comy verse section oi the same.
- the improved. operating means designated generally' by l is shown as ,connected to two double compressors designated-@generally by 2 whichas shown are duplicates of each other.
- the compressors comprise cylinders 3 ha ving heads Ll-.und o'sets 5, whereby'7 they maybe bolted as at G to an appropriate hase" 7.
- Within the cylinder 3 are mounted pistbns 8 connected for simultaneous move- Mounted centrally vbetween the cylinders is a drive shaft 1,0, preferably supported in bearings. l1 rising from the base plate 7.
- the' shaft is enlarged at 12 on which through the maximiniof the key 13 is secured a sleeve y 14 .formed Vwith a cam channel 15 in its outer surface', the channel extending circum.y Vferentially of the sleeve, so as to present its maximum operating portion approximately 'i at the respective ends oi' the sleeve.
- ⁇ cam sleeve V14 is of such diameter as to pron ject vwithin the plane of the cylinders 3,
- a connector 17, comprising a .cruci- :t'orm element centrally formed with an opening 18 to slidably engage the piston rod.
- the connector is provided with a threaded opening 19 extending at right anglesto the opening 18 for the reception ofthe threaded stud20, the outer terminal of which projects' through a slot 21 in the cylinder 3 and is provided with a head 22 for wrench application.
- a pair of cylindershaving an operating mechanism therein including piston rods, a frame connecting the cylinders together, a drive shaft positioned 1 intermediate said cylinders, said shaft having an enlargement formed thereon inter mediate the ends of the cylinders, bearings for said shaft and contacting with the ends justably mounted on said piston rods, said
Description
l -A. IjUDGBoN.
GoMPRBssoR. vAP}?LICATI()1\T FILED OCT. 8, 1913y 1,1 22,085. Patented. Dec. 22, 1914.
2 SHEETS-SHEET 1.
] vw auto@ Addelerbaqgeom Stimm 0.13 1
A' tionproviding for the` adustment ofthel i 2o l details will be described in' the -following ment through a piston rod 9.
UNITED strains rn, orriicii.,l
Anheuser nUnenoN, or nnrnoisnfrnnnsnvnnm, Assieivon or ons-roeiers 'ro J. H. WILLQUGHBY AND oNnEIenTH 'ron'.` E. nWiNc; Born or Lernens. Pensa sYLvAme.
'coiur'nnsson 'Patented Dee, 22, 1914.
a' citizen of the United States, residing at Latrobe, in the county of Westmoreland and State of Pennsylvania, have invented new and useful Improvements in Compressors, of which/the following is a specification.
The invention relatesto animproveinent in compressors and particularly to a means for operating ya series of compressors in an even an uniform manner.
'Ilie/ main object of the present invention is the provision of a compressor operating device including a rotating element having cam and pin connection with the piston 4stem oa pln'ralityof compressors, the construccomiection to vary the stro ce of the piston or pistons at will. 5' y The invention in its preferred form of specification, reference being had particularly to the accompanying drawings, in whieli'- y y Figi'ire 1 isa longitudinal sectional view showing two compressors coupled tothe im# provedA operating means. Fig. 2 is an end elevationv of the saine. Fig. is a trans-' the cam vsleeve is correspondingly rotated Awith the effect to reciprocate the pistons Vwithin the cylinders for the desired-comy verse section oi the same.
In the accompanying drawings, the improved. operating means designated generally' by l is shown as ,connected to two double compressors designated-@generally by 2 whichas shown are duplicates of each other. -The compressors comprise cylinders 3 ha ving heads Ll-.und o'sets 5, whereby'7 they maybe bolted as at G to an appropriate hase" 7. Within the cylinder 3 are mounted pistbns 8 connected for simultaneous move- Mounted centrally vbetween the cylinders is a drive shaft 1,0, preferably supported in bearings. l1 rising from the base plate 7.
Centrally of the valve of the cylinders the' shaft is enlarged at 12 on which through the mediuiniof the key 13 is secured a sleeve y 14 .formed Vwith a cam channel 15 in its outer surface', the channel extending circum.y Vferentially of the sleeve, so as to present its maximum operating portion approximately 'i at the respective ends oi' the sleeve. The
` cam sleeve V14: is of such diameter as to pron ject vwithin the plane of the cylinders 3,
the latter being cut away at 16 toireceive the sleeve.
f i Slidably mounted upon each piston rod 9 is a connector 17,. comprising a .cruci- :t'orm element centrally formed with an opening 18 to slidably engage the piston rod. The connector is provided with a threaded opening 19 extending at right anglesto the opening 18 for the reception ofthe threaded stud20, the outer terminal of which projects' through a slot 21 in the cylinder 3 and is provided with a head 22 for wrench application. By means of the ystud 20 it is obvious that the connector may be locked in any desired position upon the piston. rod 9 'within the limits of the slot 21. From the connector at a point dihmetrically opposite the stud 20 there is extended a shaft 23, the
`. ee terminal of whichis( designed to fit iny the cam groove 15l of the sleeve 14, the
.terminal of' the shaft being if desired in the form of a freely rotatable roller 'to avoid friction. The connectbr'is further guided `in movement by a stud-*24 extending there- 'from at vright angles to the shaft 23'to a screw stud 20,v which stud is guided in the' slot 25 formed lin the cylinder 3.
From the above description, it will be ap-I 'l parent that in 4the rotation of the shaft 1'0 pression of theirr eiiect, It is obvious that any number of cylinders maybe operatively connectedl to the cam sleeve, the cylinders being arranged in annular series. The improved operating device insures a ysmooth noiseless operation, eliminates crank connection, and requiresicomparatively little power to drive it.
What 1s claimed is i 'In combination, a pair of cylindershaving an operating mechanism therein including piston rods, a frame connecting the cylinders together, a drive shaft positioned 1 intermediate said cylinders, said shaft having an enlargement formed thereon inter mediate the ends of the cylinders, bearings for said shaft and contacting with the ends justably mounted on said piston rods, said
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US79410413A US1122085A (en) | 1913-10-08 | 1913-10-08 | Compressor. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US79410413A US1122085A (en) | 1913-10-08 | 1913-10-08 | Compressor. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1122085A true US1122085A (en) | 1914-12-22 |
Family
ID=3190245
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US79410413A Expired - Lifetime US1122085A (en) | 1913-10-08 | 1913-10-08 | Compressor. |
Country Status (1)
Country | Link |
---|---|
US (1) | US1122085A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2612312A (en) * | 1944-11-07 | 1952-09-30 | Christine Ass Inc | Air pump |
US4133215A (en) * | 1976-08-11 | 1979-01-09 | Worcester Controls Ag | Linear-rotary converter |
US6199884B1 (en) | 1996-12-23 | 2001-03-13 | 7444353 Alberta Ltd. | Helical drive bicycle |
US6241565B1 (en) | 1996-12-23 | 2001-06-05 | Helixsphere Technologies, Inc. | Helical drive human powered boat |
WO2009111149A1 (en) | 2008-03-03 | 2009-09-11 | Alis Corporation | Gas field ion source with coated tip |
-
1913
- 1913-10-08 US US79410413A patent/US1122085A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2612312A (en) * | 1944-11-07 | 1952-09-30 | Christine Ass Inc | Air pump |
US4133215A (en) * | 1976-08-11 | 1979-01-09 | Worcester Controls Ag | Linear-rotary converter |
US6199884B1 (en) | 1996-12-23 | 2001-03-13 | 7444353 Alberta Ltd. | Helical drive bicycle |
US6213487B1 (en) | 1996-12-23 | 2001-04-10 | 744353 Alberta Ltd. | Helical drive wheelchair |
US6241565B1 (en) | 1996-12-23 | 2001-06-05 | Helixsphere Technologies, Inc. | Helical drive human powered boat |
WO2009111149A1 (en) | 2008-03-03 | 2009-09-11 | Alis Corporation | Gas field ion source with coated tip |
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