US475301A - Cylinder for rotary blowers or engines - Google Patents
Cylinder for rotary blowers or engines Download PDFInfo
- Publication number
- US475301A US475301A US475301DA US475301A US 475301 A US475301 A US 475301A US 475301D A US475301D A US 475301DA US 475301 A US475301 A US 475301A
- Authority
- US
- United States
- Prior art keywords
- cylinder
- engines
- piston
- center
- point
- 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
Links
- 238000010276 construction Methods 0.000 description 3
- 238000012856 packing Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 2
- 230000001788 irregular Effects 0.000 description 2
- 241001446467 Mama Species 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 238000007429 general method Methods 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/10—Outer members for co-operation with rotary pistons; Casings
- F01C21/104—Stators; Members defining the outer boundaries of the working chamber
- F01C21/106—Stators; Members defining the outer boundaries of the working chamber with a radial surface, e.g. cam rings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F01C1/3441—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/344—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F04C18/3441—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
Definitions
- This invention relates generally to cylinders employed in rotary engines, blast-fans, blowers, or the like, wherein the radially-sliding pistons or blades are carried by a rotating hub or drum set eccentric to the approximate center of the cylinder.
- this type of blower or engine it is exceedingly diiiicult to obtain perfect and satisfactory results from the fact that there are pointsin the diameter of the stationary cylinder where both ends of the piston do not accurately fill the cylinder, in consequence of which leakage and loss of power or pressure result.
- a sliding piston having no springs or packings 01' followers and carried by a drum eccentrically journaled in acylindrical case has never, so far as I know, been practically used for any considerable length of time.
- the objects of my invention are to avoid the above objections, to provide a novel construction whereby the radiallyslidin g pistons or blades touch and accurately tit diametrically-opposite points at every part of theinternal caliber of the stationary cylinder without employing springs or packings or followers, and to provide a novel fan-blade or piston for this special type of blower or engine.
- my invention involves the novel cylinder bored to provide a common diameter taken on lines through a predetermined point eccentric to the approximate center of the cylinder, the internal periphery of which cylinder is formed one half semi-cylindrical and the other on a curve formed by a plurality of arcs with a gradually changing radius from the center of rotation of the piston, as fully hereinafter described and claimed, reference being made to the ac companying drawings, in which- Figure 1 is a diagrammatic view of the internal caliber of a cylinder, illustrating its oval contour and the moving centers from which it is bored.
- Fig. 2 is a vertical central sectional view of sufficient of an air-blast
- FIG. 3 shows a scriber, by which the contour-of the cylinder maybe obtained, which device, however, or the general method of obtaining the contour, is not claimed in the present specification.
- the bore of the cylinder 1 has in general an oval contour consisting in the main of an arc 6, described by a radius 26 and having the point 2 for its center, which are 6 constitutes substantially onehalf of a circle. It may extend for a distance slightly greater than one-half of the cylinder as, for instance, between the points 5 indicated on the arc.
- the bounding chord of this half-circle is situated substantially on a line drawn through the center of rotation of the pistonviz., the point 24.
- the radially-sliding pistons or blades 12 are carried by a rotating drum 13, journaled eccentrically in the stationary cylinder on the axis 24.
- a positive measured distance across the cylinder on the line 7 8 which is co-ordinate to the distance across the cylinder on the line 9 10
- the opposite extremities of the pistons or blades 12 will in their revolution preserve accurate and close contact or fit throughout the diameter of the internal caliber without liability of leakage at any point past a blade, whereby I attain, by actual demonstration, twenty per cent. increased power or pressure in the working of the blower or engine.
- the fan or pistonblades be driven or serve to drive is immaterial, and therefore I do not enter into further detailed illustration and explanation in this respect, as it is not essential for the proper understanding of my improvement.
- a base-piece having an interior curved surface formed on a radius which is substantially that of the cylinder to be produced. This surface is a half-circle.
- the 31 is an eccentrically-situated guide-pin having the position of the center of revolution of the piston or blade in the finished cylinder.
- the parts 30 and 31 may be fixed in place upon any suitable surface.
- a bar which is of a length from its end 33 to a scriber-point 34, with which it is provided, equal to the definite diameter hereinbefore referred to and equal in length to the piston or blade.
- Said bar is formed with a slot or other guide 35, adapted to engage the pin 31.
- the end 33 of the bar 32 is held firmly in contact with the base-piece 30 and revolved around the pin 31. This will cause the point 34: to describe a curve 36, which, together with the curve of the base-piece 30, will constitute the pattern for the entire contour of a cylinder whose shaft or center of rotation of the piston is to be situated at the point 31.
- the axis of the rotating drum in my construction is composed of a through-shaft 14, jou rnaled eccentrically in the cylinder-heads,
- the fan-blades may be practically 6o continuous in a radial line the pins 15 are provided, each passing through perforations 1n the shaft with either end in contact with the end of a piston or blade, there being apair of pins for each pair of blades, the whole free to slide back and forthwith respect to the axis.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
(No Model.) 2 Sheets-Sheet 1.
e. CROWELL. CYLINDER FOR ROTARY BLOWERS 0R ENGINES. No. 475,301. PatentdMay 24, 1892.
Fig: 1.
' wi/tweo oey I SWMICOL Gem/a Mmhwwv A a a W 075 Hiozna Q 2i 1 was mama Penna cu, mam-1km, msnmaran, n. c.
(No Model.) 2 Sheets-Sheet 2,
' G. OROWELL. GYLINDBR FOR ROTARY BLOWERS 0R ENGINES. No. 475,301. Patented May 24, 1892-;
@Wlbweooeo 5 g 0-1:120 6 2 5: :1 H01, m Z, M 0% 16 1112 noems mins 00., wn'm'mr pqoj, mwmumu, n.- c.
UNITED STATES.
PATENT OFFICE.
GILMER CRO\VELL, OF BROOKLYN, NEWV YORK.
CYLINDER FOR ROTARY BLOWERS OR ENGINES.
SPECIFICATION forming part of Letters Patent No. 475,301, dated May 24, 1892.
Application filed April 11, 1891. Serial No. 388,448. (No model.)
To all whom it may concern:
Be it known that I, GILMER CRoWELL, of the city of Brooklyn, county of Kings, and State of New York, have invented certain new and useful Improvements in Cylinders for Rotary Blowers or Engines, fully set forth in the following description and represented in the accompanying drawings.
This invention relates generally to cylinders employed in rotary engines, blast-fans, blowers, or the like, wherein the radially-sliding pistons or blades are carried by a rotating hub or drum set eccentric to the approximate center of the cylinder. In this type of blower or engine it is exceedingly diiiicult to obtain perfect and satisfactory results from the fact that there are pointsin the diameter of the stationary cylinder where both ends of the piston do not accurately fill the cylinder, in consequence of which leakage and loss of power or pressure result. For this reason a sliding piston having no springs or packings 01' followers and carried by a drum eccentrically journaled in acylindrical case has never, so far as I know, been practically used for any considerable length of time.
The objects of my invention are to avoid the above objections, to provide a novel construction whereby the radiallyslidin g pistons or blades touch and accurately tit diametrically-opposite points at every part of theinternal caliber of the stationary cylinder without employing springs or packings or followers, and to provide a novel fan-blade or piston for this special type of blower or engine.
To accomplish these objects my invention involves the novel cylinder bored to provide a common diameter taken on lines through a predetermined point eccentric to the approximate center of the cylinder, the internal periphery of which cylinder is formed one half semi-cylindrical and the other on a curve formed by a plurality of arcs with a gradually changing radius from the center of rotation of the piston, as fully hereinafter described and claimed, reference being made to the ac companying drawings, in which- Figure 1 is a diagrammatic view of the internal caliber of a cylinder, illustrating its oval contour and the moving centers from which it is bored. Fig. 2 is a vertical central sectional view of sufficient of an air-blast,
blower, or engine to exhibit the improvements claimed. Fig. 3 shows a scriber, by which the contour-of the cylinder maybe obtained, which device, however, or the general method of obtaining the contour, is not claimed in the present specification.
In order to enable those skilled in the art to make and use my invention, 1 will now describe the cylinder of the novel contour, referring now to Fig. 1. The bore of the cylinder 1 has in general an oval contour consisting in the main of an arc 6, described by a radius 26 and having the point 2 for its center, which are 6 constitutes substantially onehalf of a circle. It may extend for a distance slightly greater than one-half of the cylinder as, for instance, between the points 5 indicated on the arc. The bounding chord of this half-circle is situated substantially on a line drawn through the center of rotation of the pistonviz., the point 24. The remaining and in this case lesser are 27 of the cylinder is inscribed from a moving center moving in the path indicated by the oval line of dots a, with substantially the line 28 as a radius. From the foregoing it will be apparent that the center of the boring-tool, when a movable tool is used, instead of moving cylindrically will inscribe the oval a, resting for a time at the point 2 to inscribe the are 6, and then constantly moving to inscribe the irregular are 27, until it again reaches the point 2. The effect of this is to provide an irregularly-formed oval-bored cylinder, irregular so far as the contour or are 27 is concerned, and which arc, with the other are 6, provides a con tour adapted to a piston or blade set to revolve from an axis 24, eccentric with respect to the approximate center of the cylinder, whereby the extremities of such piston or blade will preserve accurate and close contact or fit throughout the diameter of the internal caliber of the cylinder.
lVith this general understanding of the nature of the cylinder and one manner in which it may be bored, I will now proceed to describe its use in an air-blast, blower, or other engine in detail, referring to Fig. 2, wherein The numeral 1 designates the stationary cylinder, which in practice is bored in the manner just explained.
The radially-sliding pistons or blades 12 are carried by a rotating drum 13, journaled eccentrically in the stationary cylinder on the axis 24. As there is a positive measured distance across the cylinder on the line 7 8 which is co-ordinate to the distance across the cylinder on the line 9 10, the opposite extremities of the pistons or blades 12 will in their revolution preserve accurate and close contact or fit throughout the diameter of the internal caliber without liability of leakage at any point past a blade, whereby I attain, by actual demonstration, twenty per cent. increased power or pressure in the working of the blower or engine. Whether the fan or pistonblades be driven or serve to drive is immaterial, and therefore I do not enter into further detailed illustration and explanation in this respect, as it is not essential for the proper understanding of my improvement.
I have shown in Fig. 3 a means by which the contour of the cylinder may be readily obtained.
30 is a base-piece having an interior curved surface formed on a radius which is substantially that of the cylinder to be produced. This surface is a half-circle.
31 is an eccentrically-situated guide-pin having the position of the center of revolution of the piston or blade in the finished cylinder. The parts 30 and 31 may be fixed in place upon any suitable surface.
32 is a bar, which is of a length from its end 33 to a scriber-point 34, with which it is provided, equal to the definite diameter hereinbefore referred to and equal in length to the piston or blade. Said bar is formed with a slot or other guide 35, adapted to engage the pin 31. In using the scriber the end 33 of the bar 32 is held firmly in contact with the base-piece 30 and revolved around the pin 31. This will cause the point 34: to describe a curve 36, which, together with the curve of the base-piece 30, will constitute the pattern for the entire contour of a cylinder whose shaft or center of rotation of the piston is to be situated at the point 31.
It has been proposed to strike the internal caliber of a cylinder from three different centers; but the construction has never been worked in consequence of theimpossibility of obtaining fan-blades or pistons that will practicahly operate con jointly therewith and avoid leakage without using spring followers or packings and the like, for the working fluid will at points in the cylinder blow past the extremities of the pistons.
The axis of the rotating drum in my construction is composed of a through-shaft 14, jou rnaled eccentrically in the cylinder-heads,
and that the fan-blades may be practically 6o continuous in a radial line the pins 15 are provided, each passing through perforations 1n the shaft with either end in contact with the end of a piston or blade, there being apair of pins for each pair of blades, the whole free to slide back and forthwith respect to the axis.
While the drum is journaled eccentrically in the cylinder and the internal diameter thereof is formed by a plurality of arcs struck from a moving center, still the extremities of the fan-blades accurately fit the cylinder at every point in the revolution of the fan, and there is no possibility of the air or other fluid blowing past the extremity of a blade, whereby the power of the engine is enlarged and good results attained.
Having th us described my invention, what I claim is 1. The herein-described cylinder, the internal periphery of substantially one -half of which is semi-cylindrical and the other portion of which is on a curve formed by a plurality of ares with a gradually-changing radius from the center of rotation of the piston, substantially as set forth.
2. The herein-described cylinder, the inter- .nal periphery of one-half of which is semicylindrical and the other portion of which is on a curve formed by a plurality of arcs with a gradually-changing radius from the center of rotation of the piston, the bounding chord of the semi-cylindrical portion being situated substantially on a line drawn through said center of rotation, substantially as set forth.
In witness whereof I have hereunto set my hand, this 8th day of April, A. D. 1891, in presence of two witnesses.
GILMER OROWELL. Witnesses:
Gate. II. GRAHAM, N. MARLER.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US475301A true US475301A (en) | 1892-05-24 |
Family
ID=2544157
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US475301D Expired - Lifetime US475301A (en) | Cylinder for rotary blowers or engines |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US475301A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4299097A (en) * | 1980-06-16 | 1981-11-10 | The Rovac Corporation | Vane type compressor employing elliptical-circular profile |
| US5181843A (en) * | 1992-01-14 | 1993-01-26 | Autocam Corporation | Internally constrained vane compressor |
| US6099261A (en) * | 1998-06-08 | 2000-08-08 | Worden; Gary | Roller vane stage for a fuel pump |
| US6513482B1 (en) * | 1999-03-05 | 2003-02-04 | Honda Giken Kogyo Kabushiki Kaisha | Rotary fluid machinery, vane fluid machinery, and waste heat recovery device of internal combustion engine |
-
0
- US US475301D patent/US475301A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4299097A (en) * | 1980-06-16 | 1981-11-10 | The Rovac Corporation | Vane type compressor employing elliptical-circular profile |
| US5181843A (en) * | 1992-01-14 | 1993-01-26 | Autocam Corporation | Internally constrained vane compressor |
| US6099261A (en) * | 1998-06-08 | 2000-08-08 | Worden; Gary | Roller vane stage for a fuel pump |
| US6513482B1 (en) * | 1999-03-05 | 2003-02-04 | Honda Giken Kogyo Kabushiki Kaisha | Rotary fluid machinery, vane fluid machinery, and waste heat recovery device of internal combustion engine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1953378A (en) | Rotary motor | |
| US3981645A (en) | Displaced piston machine | |
| US475302A (en) | Rotary blower or engine | |
| US1196977A (en) | Rotary pump. | |
| US3791779A (en) | Pump rotor adjustment mechanism | |
| US771593A (en) | Rotary engine. | |
| US3274898A (en) | Hydraulic motor | |
| US1007866A (en) | Rotary engine. | |
| US1358504A (en) | Pump | |
| US646024A (en) | Fluid-pressure engine. | |
| US644256A (en) | Rotary engine. | |
| US325276A (en) | Rotary pump | |
| US150788A (en) | Improvement in rotary blowers | |
| US558144A (en) | Rotary engine | |
| US1200505A (en) | Rotary pump or motor. | |
| US1902345A (en) | Fluid pressure pump | |
| US1718894A (en) | Power-transmission mechanism | |
| US713663A (en) | Rotary engine. | |
| US812527A (en) | Reciprocating rotary engine. | |
| US258534A (en) | Dextee d | |
| US351986A (en) | Steam-engine | |
| US1041646A (en) | Rotary engine. | |
| US2212283A (en) | Engine | |
| US3947164A (en) | Rotatable machine operating as a compressor or a motor | |
| US1084635A (en) | Rotary engine. |