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US1802887A - Rotary compressor - Google Patents

Rotary compressor
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Publication number
US1802887A
US1802887AUS204068AUS20406827AUS1802887AUS 1802887 AUS1802887 AUS 1802887AUS 204068 AUS204068 AUS 204068AUS 20406827 AUS20406827 AUS 20406827AUS 1802887 AUS1802887 AUS 1802887A
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United States
Prior art keywords
piston
shaft
chamber
guide
compressor
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Expired - Lifetime
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US204068A
Inventor
Feyens Francois
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.)
Generale D'etudes Industrielles (general Research Corporation) SA Ste
Ind General Res Corp SA Soc Ge
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Ind General Res Corp SA Soc Ge
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Application filed by Ind General Res Corp SA Soc GefiledCriticalInd General Res Corp SA Soc Ge
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Publication of US1802887ApublicationCriticalpatent/US1802887A/en
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Expired - Lifetimelegal-statusCriticalCurrent

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Description

April 28 1933.
F. FEYENS ROTARY COMPRES SOR' Filed July 7, 1927 13 Sheets-Sheet 1 April 28, 1931- 'F. FEYENS ROTARY COMPRESSOR Filed July '7, 1927 3 Sheets-Sheet 2 April 2%, 1931. FEYENS 1,8@2,,83 7
ROTARY COMPRES SOR Filed July 7, 1927 ESheets-Sheet 3 Patented Apr. 28, 1931 UNITED STATES PATENT OFFICE FBANQOIS FEYENS, OF BRUSSELS, BELGIUM, ASSIGNOR '10 SOGIETE GFNERALE DETUDES INDUSTRIELLES (GENERAL RESEARCH CORPORATION), SOCIETE ANO- NYME, OF BRUSSELS, BELGIUM ROTARY COMPRESSOR Application filed Iuly 7, 1927, Serial No. 204,068, and in Belgium December 30, 1926.-
The present invention concerns a rotary compressor in which compression is obtained by the rotation within a cylindrical chamber of a piston, of which the operative surfaces are the peripheral surfaces of two segments of a cylinder of equal radius to that of the chamber and the greatest width of each said segment diametral of the chamber is less than half of the diameter of said cylinder, the diameter and length of said piston being the factors which determine-the output. The piston which may be designated as lenticular in shape is rotated by a shaft located eccentrically with respect to the cylindrical chamber, and the arrangement is such that although the piston may be closely adjacent to or even in contact with the wall of the chamber, at given parts of its rotation, there is no actual friction between it and the said chamber.
As an exam 1e one form in which the compressor con (1 be designed in' accordance with the present invention is described hereafter, reference being made to the accompanying drawings in which:
1 is a vertical section of the compressor along line 11 of Fig. 2, showing the iston in end elevation;
Fig. 2 is a vertical section taken practical 1y centrally ofFig. 1;
Fi 3 and 4 are diagrammatic views showing the different sitions taken up by thepiston and its guid during the exhaust and suction periods res ectively;
Figs..15, 6, 7 and 8 are. iagrammatic views showing the different positions assumed by it during its cycle of rotation, and
Fi 9 is a diagrammatic cross section of the piston and its guiding means.
is shown in Fig. 1' the compressor comprises a casing a with a water jacket I) surrounding thecylinder 0 in which moves the piston 01. The piston d is of .elongated form, having the shape of two juxtaposed segments whose convex surfaces or outer configuration have the same radius as has thechamber 0 in which said piston operates, this piston being fitted. with packing strips .6 housed in grooves f in which they can move, so as to remain in permanent contact with the cylindrical wall of the chamber a whatever may be the position of the said piston in the chamber.
The piston d is operated by a shaft 9 mounted in a bearing 2' located eccentricallv in the end or cover a of the casing a. The eccentricity of this hearing i-with respect to thecylinder 0 corresponds to the distance between the centres 00 and g] of the bearing and cylinder respectively, whose value is half the height 71.- separating the middle of the face of the piston (Z from thecylinder 0 when the piston is in the position shown in Fig. 1, i. e. when it completely fills the upper portion of the cylinder. One of the lateral faces of the piston d has formed in it a slot or guide 7' which engages with a substantially square block or boss m mounted on the as well as theengaging surfaces of the boss m are parallel; further, the longitudinal axis of the said guide j coincides with the longitudinal axis of the lateral face of the piston (Z.
The reference :22 used above in connection with Fig. 1, for identifying the centre of the bearing 2', also serves in that figure, to indicate the point or line at which cross the two planes containing the longer axes of the slots j and p, as well as the longitudinal axis of the piston, all of which are in coincidence in that figure.
The cover t closing the opposite end of chamber, rota-tably supports, in a-bearing s. a short shaft 1' Whose inner end 9 is of practically square contour and engages with a sliding fit within a parallel-sided slot or guide 1) formed in the juxtaposed end of the piston (Z. The shaft 1 is concentric with thechamber 0, and the longitudinal axis of the guide ;0 is perpendicular to that of the guide 3'. The parallel shafts g and 1' whose axes are out of alignment, are A hereinafter referred to as deaxial.
If, for convenience, it be assumed that the compressor is at the stage of its operative cycle indicated by Fig. 1, the operation may .be described as follows:
is horizontal with the face k upwards, and which gives the output for a half revolution the piston (2 completely fills the portion of of thecylinder comprised between the points 1, 2, and 3 (Fig. 1). 1
If the shaft 9 is then rotated, say clock- Wise, as viewed in Figs. 1, 2, 3, 4, 6 and 7, the piston (Z will move on the square m through a distance varying with the an le through which the shaft turns,finally arriving in thevertical position shown in Fig. 3 when the shaft g has made a quarter of a revolution.
During this movement the upper face of the piston (Z moves progressively away from the wall of thecylinder 0 and begins to inhale fluid through the inlet orifices 12. provided in the casing a.
If the shaft 9 and consequently the piston d rotate through a further quarter of a revolution, it is evident that the piston d will again find itself in a horizontal position, smilar to that occuped by it in Fig. 1, but on this occasion the side l of the guide will take the place of the side is.
It follows therefore, that for a halfrevolution of the shaft, passing from the position shown in Fig. 1 to the position shown in Fig. 4, the piston has forced the liquid, which was under it and which has been admitted through the inlet orifices n, through the outlet orifices o.
If the movement of rotation is continued for a further half revolution of the shaft, the piston 11 will effect the same movement as above, repeating the work of suction, compression and dehvery, and will return to the position shown in Fig. 1 in whichthe side 7.: of the guide will have come back to its starting point. Two phases-of suction and delivery will therefore have taken place for each complete revolution of the shaft 9.
As can be clearly seen in Figs. 5 to 8, given the perpendicularity of the guides j and p and the relative position of the square 9 on the guide p, the function of the device is at all times to guide the piston (l, which will continue to rotate without ever rubbing on the wall of the cylinder with which the packing strips '4: alone are in contact. Figs. 6 and 7 show the relative positions of the guide j and of its driving boss m compared with the position occupied at that moment by the opposite guide p and the square q (Figs. 5 and 8). It is obvious that the shaft 1* could be used for transmitting the movement of rotation to a second, third or fourth unit according to the size of the compressor set.
The output of a compressor of ,this kind can be determined in the following manner:
The area of the crescent shaped space having the height h (Fig. 1) comprised between the wall of the cylinder and the piston is multiplied by the length of the cylinderof the piston. 1"
The arrangement described above enables a compressor to be designed in such a way that the piston is cooled on all its faces, the result being rapid transfusion of the calories and consequently an increase in the volumetric efliciency of the compressor, the leak age in the latter being very limited.
What I claim is': u A rotary compressor comprising a casing having a substantially cylindrical chamber provided with inlet and outlet ports spaced apart, a lenticular piston arranged in said chamber and having guide slots in opposite sides, one parallel with the longer center lines of the piston and the other at right angles thereto, a driving shaft mounted in a bearing in said casing and arranged eccentricall of the chamber, the inner end of said riving shaft having a block fixed thereto which is slidably arranged in the said longer slot of the piston, a shaft mounted in a bearing in the opposite side of the casing from that of the driving shaft, said last named shaft bein concentric with said chamber and provide at its inner end with a block which is arranged in' the other slot of the piston.
In testimony whereof I afiix my si tur'e.
FRANCOIS FEY NS.
US204068A1926-12-301927-07-07Rotary compressorExpired - LifetimeUS1802887A (en)

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BE1802887X1926-12-30

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3259113A (en)*1961-08-161966-07-05Yanmar Diesel Engine CoRotary diesel engines
US3289601A (en)*1965-02-121966-12-06Fawick CorpFluid displacement device usable as a hydraulic motor or pump
US3367239A (en)*1964-07-281968-02-06Takagi MoriyukiFluid reducers
US3690791A (en)*1970-02-101972-09-12Robert L DieterRotary engine with radially shiftable rotor
US3873245A (en)*1973-01-021975-03-25Nastol Research IncSteam-driven engine
US4008988A (en)*1974-12-161977-02-22Putz A FrankRotary piston expansible chamber device
US4030861A (en)*1974-12-161977-06-21Putz A FrankVariable displacement rotary piston expansible chamber device
US4173438A (en)*1975-11-171979-11-06Putz A FrankRotary piston device which displaces fluid in inner and outer variable volume chambers simultaneously
US6786128B1 (en)*2003-01-022004-09-07Ronald M. GaudetFluid motor
US20060233653A1 (en)*2003-08-272006-10-19Yannis TrapalisRotary mechanism
US20070160487A1 (en)*2005-12-012007-07-12Gray David DRotary combustion apparatus
US7350500B1 (en)2006-02-242008-04-01Webb David WInverted cardioid engine
AU2004269045B2 (en)*2003-08-272010-07-29Kcr Technologies Pty LtdRotary mechanism
US20210372408A1 (en)*2018-07-182021-12-02Gree Electric Appliances, Inc. Of ZhuhaiPump body assembly, fluid machinery, and heat exchange device

Cited By (21)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3259113A (en)*1961-08-161966-07-05Yanmar Diesel Engine CoRotary diesel engines
US3367239A (en)*1964-07-281968-02-06Takagi MoriyukiFluid reducers
US3289601A (en)*1965-02-121966-12-06Fawick CorpFluid displacement device usable as a hydraulic motor or pump
US3690791A (en)*1970-02-101972-09-12Robert L DieterRotary engine with radially shiftable rotor
US3873245A (en)*1973-01-021975-03-25Nastol Research IncSteam-driven engine
US4008988A (en)*1974-12-161977-02-22Putz A FrankRotary piston expansible chamber device
US4030861A (en)*1974-12-161977-06-21Putz A FrankVariable displacement rotary piston expansible chamber device
US4173438A (en)*1975-11-171979-11-06Putz A FrankRotary piston device which displaces fluid in inner and outer variable volume chambers simultaneously
US6786128B1 (en)*2003-01-022004-09-07Ronald M. GaudetFluid motor
JP2007503543A (en)*2003-08-272007-02-22ケーシーアール・テクノロジーズ・ピーティーワイ・リミテッド Rotary mechanism
US20060233653A1 (en)*2003-08-272006-10-19Yannis TrapalisRotary mechanism
US7549850B2 (en)*2003-08-272009-06-23Kcr Technologies Pty LtdRotary mechanism
AU2004269045B2 (en)*2003-08-272010-07-29Kcr Technologies Pty LtdRotary mechanism
US20070160487A1 (en)*2005-12-012007-07-12Gray David DRotary combustion apparatus
JP2009518569A (en)*2005-12-012009-05-07デイビッド ディー. グレイ, Rotary combustion device
US7942657B2 (en)*2005-12-012011-05-17Gray David DusellRotary combustion apparatus
JP2012122484A (en)*2005-12-012012-06-28David D GrayRotary combustion apparatus
US8539930B2 (en)2005-12-012013-09-24David DuSell GrayRotary combustion apparatus
US7350500B1 (en)2006-02-242008-04-01Webb David WInverted cardioid engine
US20210372408A1 (en)*2018-07-182021-12-02Gree Electric Appliances, Inc. Of ZhuhaiPump body assembly, fluid machinery, and heat exchange device
US12286972B2 (en)*2018-07-182025-04-29Gree Electric Appliances, Inc. Of ZhuhaiPump body assembly, fluid machinery, and heat exchange device

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