US1917444A - Supercharger - Google Patents

Supercharger Download PDF

Info

Publication number
US1917444A
US1917444A US522491A US52249131A US1917444A US 1917444 A US1917444 A US 1917444A US 522491 A US522491 A US 522491A US 52249131 A US52249131 A US 52249131A US 1917444 A US1917444 A US 1917444A
Authority
US
United States
Prior art keywords
rotor
vanes
shoes
valve member
end walls
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
US522491A
Inventor
Gregg David
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.)
Eclipse Aviation Corp
Original Assignee
Eclipse Aviation Corp
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 Eclipse Aviation Corp filed Critical Eclipse Aviation Corp
Priority to US522491A priority Critical patent/US1917444A/en
Application granted granted Critical
Publication of US1917444A publication Critical patent/US1917444A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03CPOSITIVE-DISPLACEMENT ENGINES DRIVEN BY LIQUIDS
    • F03C2/00Rotary-piston engines
    • F03C2/30Rotary-piston engines having the characteristics covered by two or more of groups F03C2/02, F03C2/08, F03C2/22, F03C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B33/00Engines characterised by provision of pumps for charging or scavenging
    • F02B33/32Engines with pumps other than of reciprocating-piston type
    • F02B33/34Engines with pumps other than of reciprocating-piston type with rotary pumps
    • F02B33/36Engines with pumps other than of reciprocating-piston type with rotary pumps of positive-displacement type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/32Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having both the movement defined in groups F04C2/02 and relative reciprocation between co-operating members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/30Rotary-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
    • F04C18/34Rotary-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
    • F04C18/344Rotary-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
    • F04C18/348Rotary-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 vanes positively engaging, with circumferential play, an outer rotatable member

Definitions

  • This invention relates to superchargers, and particularly to means for compressing the combustible mixture to be supplied to the combustion chambers of an internal combustion engine having a two-stroke cycle.
  • An orbject of the invention is to provide a novel construction for a supercharger of the type adapted to be driven fromA a rotatable member of an associated engine.
  • Another object of the invention is to provide a supercharger embodying a-rotary valve v mechanism of novel construction adapted to be rotated with a driven member mounted by novel means operating to vary the volume of the compression chamber in accordance with the variation in the angle described by a rotating element of said novel means.
  • a further object is to yprovide a supercharger in which the compression chambers are so controlled aspto be of constantly increasing volume during the intake period, and of constantly decreasing volume during the discharge period.
  • Fig. 1 is a transverse sectional view of a device embodying the invention.
  • ⁇ 2 is a sectional elevation view taken at right angles to the viewpoint and along the line 2-2 of Fig. 1.
  • the invention is shown embodied in a cylindrical casing' member 3 having oppositely disposed extensions 4 and 5, the former constituting an'entrance duct for the air or combustible mixture to be compressed in the casing 3 and then delivered to the intake manifold ofthe engine with which the exit passage 5 communicates.
  • a cylindrical valve member 6 of the sleeve'or tubular type having any desired number of pairs of longitudif nally extending ports 7 and 7 a each pair being cpt in the cylindrical wall thereof at diametrically opposite locations thereon, and at angular distances corresponding to the number. of ports, said sleeve member being adapted to closely fit the-cylindrical surface of the chamber 3 and be rotated relatively thereto.
  • the novel compressing means preferably y takes the-form of a plurality of curved blades or vanes 15 corresponding in number to the number of ports; and pivotally secured alt their outer ends to suitable pivots 9 extending from the inwardlyturned ends of the member 6 and spaced equally about the periphery of said member between the successive ports 7 and 7 a.
  • vanes 8 are preferably pivotally connected by pins V10 journale'd in ears 11 formed on shoes 12 whichare slidably mounted about the end portions of the circumference of the driven drumfor rotor 14, suitable annular grooves or tracks 13 being provided for this purpose in the end surfaces of the rotor 14, the latter being supported at either end thereof on bearing pins 18 secured in the supporting frame 19 eccentrically to the axis of rotation of sleeve 6, bearings 20 being provided to facilitate rotation of the member 14 about said bearing pms.
  • Y l journale'd in ears 11 formed on shoes 12 whichare slidably mounted about the end portions of the circumference of the driven drumfor rotor 14, suitable annular grooves or tracks 13 being provided for this purpose in the end surfaces of the rotor 14, the latter being supported at either end thereof on bearing pins 18 secured in the supporting frame 19 eccentrically to the axis of rotation of sleeve 6, bearings 20 being provided to facilitate rotation of the member 14 about said bearing pms.
  • any suitable driving means may be employed for imparting rotation to sleeve valve 6, but in the preferred form as illustrated, such driving means comprises the provision of a gear 23 rotatably supported on ball bearing 24 and secured to a flanged annular end of plate 25 by suitable screws 26 the gear 23 being also drivably secured to the sleeve 6 by means of said screws 26, and being inmesh with a gear 27 which is in turn rotatable with the crankshaft or other rotatable member of the associated engine.
  • the casing 5 is 4divided centrally by a partition 29 whichV thereby forms two exit ducts 30 and 31, each leading to the intake manifold or inlet port of a cylinder (or group of cylinders firing at the same time).
  • a partition 29 whichV thereby forms two exit ducts 30 and 31, each leading to the intake manifold or inlet port of a cylinder (or group of cylinders firing at the same time).
  • vanes 8 whereby they are pivotally mounted at their ends to produce a constantly changing angularity with respect to the rotor 14, in conjunction with the disposition of the ports 7 and 7a, operates to produce a proper timing of the compressing action with respect to the volume of the associated chambers.
  • the constantly changing angularity of the vanes causes shoes 12 to move at angular speeds which vary in accordance with the change in the angle described by the shoes while rotating.
  • a corresponding variation occurs in the volume of each chamber due to the disposition of the parts as above suggested, the relation of ports to vanes being such that each chamber is of constantly increasing volume during the entire period of communication between the intake duct and the valve port for the corresponding chamber, and is of constantly decreasing volume during the period of communication between the said port and the Huid discharge duct.
  • a tubular member a rotatable shoe associated therewith, a vane pivotally connected at one end to said tubular member and at the other end to said shoe, means for mounting said shoe for rotation about an axis eccentric to the axis of'said tubular member, and means for rotating said shoe about 'said eccentric axis ata non-uniform speed in response to track a tortuous sealing passageway.
  • a housing having a Huid entrance duct and a fluid exit duct, and means for establishing periodic communication therebetween
  • a tubular valve member having a port formed in a rotor for actuating said valve member to cause said port to register alternately with said entrance and exit ducts, and means mounted within said valve member to form a chamber in which the Yfluid entering said valve member through said Vport 'is compressed prior to delivery to sald'exit duct, said last named means com- Vmember having tubular member and having an inturned flange nested with the rotor to form a tortuous passage therebetween.
  • a cylindrical housing having end walls, a tubular valve member having closed ends rotatably mounted therein,- the valve member, vanes pivotally connected to the valve member, said rotor having annular guideways in its end faces arranged adjacent the end walls of the h ousing, shoes slidably positioned in the guideways iiush with the end walls of both rotor and valve, and said shoes having pivotal connections with the vanes.
  • a cylindrical housing having end walls, a tubular valve closed ends rotatably .mounted therein, a rotor eccentrically mounted in the valve member, vanes pivotally connected .to the valve member, said rotor having annular guideways of vL-shaped cross section in its end faces arrangedadjacent the end walls of the housing, shoes of L-shaped cross section slidably positioned in the guideways flush with the end walls of both rotor and valve, and said shoes having pivotal connections with the vanes.
  • a cylindrical housing having end walls, a tubular valve member having closed end walls rotatably mounted therein, said end walls having their inner faces in alignment, a rotor eccentrically molmted inthe valve member, vanes pivotally connected to the valve member and to the rotor by shoes relatively movable in their angular relation to the rotor, said shoes having a plane outer face adapted to contact the inner end walls of both the housing and tubular member for preventing leakage therebetween.
  • a cylindrical housing having end walls, a tubular valve member having closed end walls rotatably mounted therein, said end walls having their inner faces in alignment, va rotor eccentrical- 1y mounted in the valve member, vanes pivotally connected to the valve member and to a rotor eccentrically mounted in the rotor by shoes relatively movable in their angular relation to the rotor, Vsaid shoes having 'a plane outer face adapted to contact the inner end walls of both the housing and tubular member for preventing leakage therebetween, and each of said shoes having an inwardly extending flange slidably fitted in a corresponding annular groove in the end face of the rotor.
  • a rotary fluid compressor havin a cylindrical housing, a tubular valve mem er rotatably mounted therein, a rotor eccenltrically mounted in the member, hinged vanes connecting the rotor and member forming therewith sets of variable volume compartmcnt's, the connection of the vanes with the rotor including. shoes having arcuate projections coacting with an annular groove in the rotor end'face, said vanes being angularly movable with respect to the rotor, an inlet for the compressor, a plurality of outlets, conduits corresponding in number to the number of compartment sets, and means for delivering fluid from the compressor to the outlets selectively and in a regular recurring sequence.
  • a rotary iuid compressor havin a cylindrical housing, a tubular valve mem er rotatably mounted therein, a rotor eccentrically mounted in the member, hinged vanes connecting the rotor and member .forming therewith sets of variable volume compartments, the connection of the vanes with the rotor including shoes having arcuate projections coacting withan annular groove ⁇ in the rotor end face, said vanes being angularly movable with respect to the rot/0r, an inlet for the compressor, va plurality of outlets, conduits corresponding in number to the numberof compartment sets, means for delivering iluid from the compressor to the outlets selectively and in a regular recurring sequence, said means comprising axially spaced outlets in the tubular valve member, and spaced openings inthe housing having a communication with the outlet conduits and arranged to periodically coincide with the valve member outlets.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Rotary Pumps (AREA)

Description

Patented July 1l, 1933 UNITED STATES' PATENT lOFFICE DAVID GREGG, OF CALDWELL, NEW JERSEY, ASSIGNOR T0 ECLPSE AVIATION COBPO RATION, OF EAST ORANGE, NEW' JERSEY, A CORPORATION Ol' NEW JERSEY SUPERC'HARGER Application filed March 18, 1931. Serial No. 522,491.
' This invention relates to superchargers, and particularly to means for compressing the combustible mixture to be supplied to the combustion chambers of an internal combustion engine having a two-stroke cycle.
An orbject of the invention is to provide a novel construction for a supercharger of the type adapted to be driven fromA a rotatable member of an associated engine.
Another object of the invention is to provide a supercharger embodying a-rotary valve v mechanism of novel construction adapted to be rotated with a driven member mounted by novel means operating to vary the volume of the compression chamber in accordance with the variation in the angle described by a rotating element of said novel means.
A further object is to yprovide a supercharger in which the compression chambers are so controlled aspto be of constantly increasing volume during the intake period, and of constantly decreasing volume during the discharge period.
These and other objects of the invention will become apparent from inspection of the following specifications when read with reference to the accompanying drawing wherein is illustrated the preferred embodiment of the invention. It is to be expressly understood, however, that the drawing is for the purpose of illustration only, and is not designed as a deinition of the limits of the invention, reference being had to the appended claims for this purpose.
In the drawing,
Fig. 1 'is a transverse sectional view of a device embodying the invention; and
`2 is a sectional elevation view taken at right angles to the viewpoint and along the line 2-2 of Fig. 1. v
In the drawing, the invention is shown embodied in a cylindrical casing' member 3 having oppositely disposed extensions 4 and 5, the former constituting an'entrance duct for the air or combustible mixture to be compressed in the casing 3 and then delivered to the intake manifold ofthe engine with which the exit passage 5 communicates. c
may be interposed between the supercharger and the engine, or between'the supercharger and the air intake duct, any suitable means for carbureting the combustible mixture and otherwise conditioning the combustion supporting air to secure maximum efficiency of combustion in the combustion chambers of the engine, and that the location and operation of the same is not material to the present invention which consists in the construction of a novel supercharger capable of application and use with any suitable arrangement of such devices.
comprises the provision of a cylindrical valve member 6 of the sleeve'or tubular type having any desired number of pairs of longitudif nally extending ports 7 and 7 a each pair being cpt in the cylindrical wall thereof at diametrically opposite locations thereon, and at angular distances corresponding to the number. of ports, said sleeve member being adapted to closely fit the-cylindrical surface of the chamber 3 and be rotated relatively thereto.
b v novel means now to be described.
Such a novel supercharger construction4 It is to be understood, of course, that there.
v'The novel compressing means preferably y takes the-form of a plurality of curved blades or vanes 15 corresponding in number to the number of ports; and pivotally secured alt their outer ends to suitable pivots 9 extending from the inwardlyturned ends of the member 6 and spaced equally about the periphery of said member between the successive ports 7 and 7 a. ,The inner ends of the vanes 8 are preferably pivotally connected by pins V10 journale'd in ears 11 formed on shoes 12 whichare slidably mounted about the end portions of the circumference of the driven drumfor rotor 14, suitable annular grooves or tracks 13 being provided for this purpose in the end surfaces of the rotor 14, the latter being supported at either end thereof on bearing pins 18 secured in the supporting frame 19 eccentrically to the axis of rotation of sleeve 6, bearings 20 being provided to facilitate rotation of the member 14 about said bearing pms. Y l
Any suitable driving means may be employed for imparting rotation to sleeve valve 6, but in the preferred form as illustrated, such driving means comprises the provision of a gear 23 rotatably supported on ball bearing 24 and secured to a flanged annular end of plate 25 by suitable screws 26 the gear 23 being also drivably secured to the sleeve 6 by means of said screws 26, and being inmesh with a gear 27 which is in turn rotatable with the crankshaft or other rotatable member of the associated engine.
As shown best in Fig. 2, the casing 5 is 4divided centrally by a partition 29 whichV thereby forms two exit ducts 30 and 31, each leading to the intake manifold or inlet port of a cylinder (or group of cylinders firing at the same time). In the device illustrated thereare four vanes and two sets of ports,
compressing and timing the delivery of a charge for two cylinders or sets of cylinders. For a three cylinder engine, (or engine with three sets of cylinders firing together-as, for example, a six cylinder two cycle engine with opposed cylinders) there would be six vanes, and three sets of spaced ports, and three outlets.
Having thus identified the parts entering into the preferred embodiment of the invention herein illustrated, the operation will be seen to be as follows):
On rotation` being imparted to the sleeve 6 through the intermediary of gears 23 and 27, and driving screws 26, the combustible charge will be admitted through each ofthe ports 7 during a portion of each revolution of the sleeve 6, the gearing being preferably timed so that admission occurs as the piston is in proper position to insure properly timed delivery of the charge to the combustion chambers of the cylinder. Following the admission of the charge through the port 7, the
,oscillating action of the vanes 15 (as their shoes 12 slide at variable speeds along tracks 13)- compresses the charge and, after half a revolution, forces it through the port 7' into the chamber 31, from which chamber it leads to the proper combustion point. Continued.
rotation of sleeve 6 eccentrically to the rotor 14 will bring the port 7 a into registry with the intake passage 4, and at the same time will bring the op osite port 7a into registry with outlet chamher 30, whereupon a similarly compressedl charge will be delivered thereto.
Due to the spiral and rearwardly extend- Y ing disposition of the vanes 15 relatively to `rthe direction of rotation of sleeve 6, the dithe cylindrical wall thereof,
rection of the gases toward the outlet chambers is facilitated and greater eiiciency of operation therebyl assured. Moreover, the novel construction of the vanes 8 whereby they are pivotally mounted at their ends to produce a constantly changing angularity with respect to the rotor 14, in conjunction with the disposition of the ports 7 and 7a, operates to produce a proper timing of the compressing action with respect to the volume of the associated chambers.
The constantly changing angularity of the vanes causes shoes 12 to move at angular speeds which vary in accordance with the change in the angle described by the shoes while rotating. A corresponding variation occurs in the volume of each chamber due to the disposition of the parts as above suggested, the relation of ports to vanes being such that each chamber is of constantly increasing volume during the entire period of communication between the intake duct and the valve port for the corresponding chamber, and is of constantly decreasing volume during the period of communication between the said port and the Huid discharge duct. Thus there is obtained a perfect synchronization between volume change and pressure change whichinsures maximum eiiciency in operation.
It will be understood,however, that various changes may be made in the form, details of construction, arrangement of parts and the uses to which they are applied.
What is claimed is:
1. In a device of the class described, a tubular member, a rotatable shoe associated therewith, a vane pivotally connected at one end to said tubular member and at the other end to said shoe, means for mounting said shoe for rotation about an axis eccentric to the axis of'said tubular member, and means for rotating said shoe about 'said eccentric axis ata non-uniform speed in response to track a tortuous sealing passageway.
2. In a rotary compressor, a housing having a Huid entrance duct and a fluid exit duct, and means for establishing periodic communication therebetween comprising a tubular valve member having a port formed in a rotor for actuating said valve member to cause said port to register alternately with said entrance and exit ducts, and means mounted within said valve member to form a chamber in which the Yfluid entering said valve member through said Vport 'is compressed prior to delivery to sald'exit duct, said last named means com- Vmember having tubular member and having an inturned flange nested with the rotor to form a tortuous passage therebetween.
3. In a rotary compressor, a cylindrical housing having end walls, a tubular valve member having closed ends rotatably mounted therein,- the valve member, vanes pivotally connected to the valve member, said rotor having annular guideways in its end faces arranged adjacent the end walls of the h ousing, shoes slidably positioned in the guideways iiush with the end walls of both rotor and valve, and said shoes having pivotal connections with the vanes.
4.. In a rotary compressor, a cylindrical housing having end walls, a tubular valve closed ends rotatably .mounted therein, a rotor eccentrically mounted in the valve member, vanes pivotally connected .to the valve member, said rotor having annular guideways of vL-shaped cross section in its end faces arrangedadjacent the end walls of the housing, shoes of L-shaped cross section slidably positioned in the guideways flush with the end walls of both rotor and valve, and said shoes having pivotal connections with the vanes.
5. In a rotary compressor, a cylindrical housing having end walls, a tubular valve member having closed end walls rotatably mounted therein, said end walls having their inner faces in alignment, a rotor eccentrically molmted inthe valve member, vanes pivotally connected to the valve member and to the rotor by shoes relatively movable in their angular relation to the rotor, said shoes having a plane outer face adapted to contact the inner end walls of both the housing and tubular member for preventing leakage therebetween.
6. In a rotary compressor, a cylindrical housing having end walls, a tubular valve member having closed end walls rotatably mounted therein, said end walls having their inner faces in alignment, va rotor eccentrical- 1y mounted in the valve member, vanes pivotally connected to the valve member and to a rotor eccentrically mounted in the rotor by shoes relatively movable in their angular relation to the rotor, Vsaid shoes having 'a plane outer face adapted to contact the inner end walls of both the housing and tubular member for preventing leakage therebetween, and each of said shoes having an inwardly extending flange slidably fitted in a corresponding annular groove in the end face of the rotor.
7 In a rotary fluid compressor havin a cylindrical housing, a tubular valve mem er rotatably mounted therein, a rotor eccenltrically mounted in the member, hinged vanes connecting the rotor and member forming therewith sets of variable volume compartmcnt's, the connection of the vanes with the rotor including. shoes having arcuate projections coacting with an annular groove in the rotor end'face, said vanes being angularly movable with respect to the rotor, an inlet for the compressor, a plurality of outlets, conduits corresponding in number to the number of compartment sets, and means for delivering fluid from the compressor to the outlets selectively and in a regular recurring sequence.
8. In a rotary iuid compressor havin a cylindrical housing, a tubular valve mem er rotatably mounted therein, a rotor eccentrically mounted in the member, hinged vanes connecting the rotor and member .forming therewith sets of variable volume compartments, the connection of the vanes with the rotor including shoes having arcuate projections coacting withan annular groove `in the rotor end face, said vanes being angularly movable with respect to the rot/0r, an inlet for the compressor, va plurality of outlets, conduits corresponding in number to the numberof compartment sets, means for delivering iluid from the compressor to the outlets selectively and in a regular recurring sequence, said means comprising axially spaced outlets in the tubular valve member, and spaced openings inthe housing having a communication with the outlet conduits and arranged to periodically coincide with the valve member outlets.
In testimony whereof I have signed this specication.
DAVID GREGG.
US522491A 1931-03-13 1931-03-13 Supercharger Expired - Lifetime US1917444A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US522491A US1917444A (en) 1931-03-13 1931-03-13 Supercharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US522491A US1917444A (en) 1931-03-13 1931-03-13 Supercharger

Publications (1)

Publication Number Publication Date
US1917444A true US1917444A (en) 1933-07-11

Family

ID=24081080

Family Applications (1)

Application Number Title Priority Date Filing Date
US522491A Expired - Lifetime US1917444A (en) 1931-03-13 1931-03-13 Supercharger

Country Status (1)

Country Link
US (1) US1917444A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2634903A (en) * 1945-06-23 1953-04-14 A F Flournoy Pressure blower
US2792984A (en) * 1945-06-23 1957-05-21 A F Flournoy Pressure blower
US3185385A (en) * 1962-04-16 1965-05-25 Floyd J Moltchan Rotary air pump
US3821899A (en) * 1969-03-26 1974-07-02 A Granberg Fluid meter

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2634903A (en) * 1945-06-23 1953-04-14 A F Flournoy Pressure blower
US2792984A (en) * 1945-06-23 1957-05-21 A F Flournoy Pressure blower
US3185385A (en) * 1962-04-16 1965-05-25 Floyd J Moltchan Rotary air pump
US3821899A (en) * 1969-03-26 1974-07-02 A Granberg Fluid meter

Similar Documents

Publication Publication Date Title
US4844708A (en) Elliptical-drive oscillating compressor and pump
US5567139A (en) Two rotor sliding vane compressor
US3549286A (en) Rotary engine
US2136066A (en) Rotary engine
US2058817A (en) Rotary internal combustion engine
US2158532A (en) Complementary rotary engine
US1922363A (en) Rotary engine
US2580006A (en) Compressor
US3207425A (en) Rolling body engine with multiple rotors
US1605912A (en) barker
US1773635A (en) Motor
US3364907A (en) Rotary piston mechanism
US2779318A (en) Internal combustion engine
US2130054A (en) Blower
US3245389A (en) Internal combustion engine with disk piston
US1917444A (en) Supercharger
US1949723A (en) Air compressor and supercharger
US2090280A (en) Compressor
US4005682A (en) Rotary internal combustion engine
US2117700A (en) Internal combustion engine
US5271364A (en) Rotary internal combustion engine
US2089593A (en) Rotary compressor and the like
US3205875A (en) Four-cycle rotary internal combustion engines
US2403282A (en) Internal-combustion engine
US4022553A (en) Rotary piston compressor with inlet and discharge through the pistons which rotate in the same direction