US3097478A - Exhaust gas driven compressor - Google Patents

Exhaust gas driven compressor Download PDF

Info

Publication number
US3097478A
US3097478A US3097478DA US3097478A US 3097478 A US3097478 A US 3097478A US 3097478D A US3097478D A US 3097478DA US 3097478 A US3097478 A US 3097478A
Authority
US
United States
Prior art keywords
rotary piston
compressor
exhaust gas
rotary
engine
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
Publication date
Application granted granted Critical
Publication of US3097478A publication Critical patent/US3097478A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/16Control of the pumps by bypassing charging air

Definitions

  • EXHAUST GAS DRIVEN COMPRESSOR Filed Sept. 28, 1960 3 Sheets-Sheet 3 Unite rate ten 3,097,478
  • the present invention relates to an exhaust gas driven compressor for combustion engines which comprises a turbine or rotary piston motor driven by exhaust gases and a rotary piston blower driven by the turbine or motor, the delivery of the blower being controlled by control means.
  • Exhaust gas driven compressors comprising a turbine and a blower Wheel are known in which the speed of notation depends substantially on the quantity and pressure of the combustion gases being conveyed to the exhaust gas driven compressor.
  • the speed of rotation of the compressor is low because in spite of the reduced blower pressure, the quantity of exhaust gas will not sufiice to maintain the compressor at high speed. Consequently, whenever the compressor is being started it has to be brought up first to its normal speed. In view of the low quantity of combustion gases initially available and in view of the inertia of the rotating compressor elements, this bringing up the compressor to normal speed is effected at a more or less delay with regard to the quickly increasing engine speed.
  • FIG. 1 illustrates a longitudinal section through an exhaust gas driven compressor composed of two rotary piston units combined to a unit, said section being taken along the line I--I of FIG. 2.
  • FIG. 2 is a cross section taken along the line II-tlI of FIG. 1.
  • FIG. 3 represents a rotary piston unit similar to that of FIG. 1 but with a housing sub-divided along its longitudinal extension.
  • FIG. 3a is a section along the line IIIa-IIIa of FIG. 3.
  • FIG. 4 is a diagrammatic illustration of a rotary piston unit according to the invention in connection With an internal combustion engine.
  • FIG. 4a is a diagrammatic representation of a control device according to which the control member of an air compressor is adjusted in conformity with the speed of the engine.
  • a rotary piston blower provided with a quantity controlling member which automatically at low engine speed or low engine output will reduce the delivery in conformity with the engine speed or the pressure of the exhaust gases.
  • the thus reduced delivery means a reduced output of the blower or compressor and thus also a reduction in the output of the driving member thereby permitting a higher speed with the same quantity of exhaust gases.
  • rotary piston unit as a blower par-t suggests to design also the driving part as rotary piston unit.
  • the type of constructions must meet the fundamental requirement that their admissible speeds will be high and will be adapted to each other and that furthermore the blower part will be adapted to be controlled as to delivery.
  • rotary piston units which comprise two rotary pistons arranged one within the other and of which only the one driven rotary piston performs work, whereas the other rotary piston is idly rotated by direct contact with the driven piston or through the intervention of a pair of gears.
  • two of the above mentioned rotary piston units are em ployed While the work performing rotary pistons thereof are interconnected by coupling elements Whereas the other two rotary pistons are freely rotatable.
  • the two parts of the compressor ie the motor part and the compressor part, are combined into a unit.
  • this is effected by providing each of the two work performing rotary pistons with a short shaft or stud and by connecting these short shafts or studs in a rigid and bend-resistant manner.
  • the rotary piston combined as a unit are then journalled on the said short shafts or studs.
  • This type of connecting the rotary pistons to each other furthermore yields the possibilities of journalling both rotary pistons in a common housing.
  • the work performing rotary pistons may be made of one piece but in this instance they would have to be journalled in a housing which is split in longitudinal direction.
  • the employment of two rotary piston units according to the invention is not limited to exhaust gas driven compressors. Also prime mover and machine tools for other purposes may be connected in the same manner.
  • the exhaust gas driven compressor shown in FIG. 1 has on the left-hand side thereof the driving part With the outer rotary piston 1 and the inner rotary piston '5.
  • the blower or compressor part comprises an outer rotary piston 2 and an inner rotary piston 6.
  • the outer rotary piston 1 is rigidly and in a bend-resistant manner connected to the outer rotary piston 2 in any convenient manner for instance by means of annular tension springs 3.
  • the rotary pistons thus forming a unit are journ-alled in a common nonsplit housing 4.
  • the humor rotary pistons 5 and 6 which do not perform any Work and which are directly rotated by the outer rotary pistons.
  • the air inflow and outflow for both machine parts is effected through lids or covers 7 and 8, respectively.
  • These lids also have fixedly mounted therein bearing studs 9 and 10 for the inner rotary pistons 5 .and 6 respectively.
  • a control member 11 which for purposes of illustration has been angularly displaced into the plane of the section shown in FIG. 1.
  • FIG. 2 illustrates the control means and shows in dotdash lines the rotary pistons 2 and 6 which are for instance provided with six and five teeth respectively.
  • the shaded control member 11 is designed for instance as a segment or sector which is adapted to be adjusted in tangential direction in the slot 24 in lid 8 by means operable from the outside thereof in a well-known manner. On both sides of the segment 11 there are respectit/ely provided an inlet opening 13 and an outlet opening 14. These openings are de-limi-ted by two stationary radial and by two movable radial edges.
  • the stationary radial edge 15 determines the end of the intake cycle, whereas the stationary edge 16- releases the discharge of the compressed air..
  • the movable edge 17 controls the start of the intake cycle, and the movable edge 18 determines the end of the discharge or more specifically the quantity of the air conveyed into the pressure conduit.
  • the two rotary pistons rotating in clockwise direction confine for instance working chambers 19, 2t 21, 22, 23 which increase in volume ahead of the intake opening and which decrease in volume after passing the lower dead center. If now the control member is displaced in righthand-direction and moved into the position indicated by dash lines, control edge 18 will establish communication of the pressure connection behind the outlet opening 14 with the indrawing working chambers, in the particular showing with chamber 19. Air which has already been conveyed into the pressure connection will then be able from there to flow back into the working chambers. By reexpanding of the returned quantity of air, the major portion of the compressing work employed for this quantity of air will be re-gained.
  • the driving part of the compressor thus has to furnish substantially only the energy for the actually delivered quantity of air.
  • the housing for the rotary piston unit illustrated therein comprises an upper portion 25 and a lower portion 26.
  • the arrangement likewise comprises an outer rotor 27 and an inner rotor 28.
  • the outer spacing sleeve for the journalling of the inner rotor 28 is designated with the reference numeral 29 while the corresponding inner spacing sleeve is designated with the reference numeral 30.
  • the bearing stud for the inner rotor is designated with the reference numeral 31.
  • the housing portion for the rotary piston motor is closed by a lid 32, whereas the housing portion for the compressor is closed by a lid 33.
  • the internal combustion engine 35 is provided with an exhaust gas conduit 36 leading to the exhaust gas driven rot-ary piston motor 37 while leading from the motor 'is conduit 39. Coupled to the rotary piston motor 37 is a rotary piston compressor 38.
  • compressor 38 has connected thereto an intake conduit 40 and a pressure or discharge conduit 41 which simult-aneously represents the intake conduit for the internal combustion engine 85.
  • the internal combustion engine 35. is provided with a crank stud 42.
  • the compressor 38 has associated therewith a control member 43 which corresponds to the control member 11 of the arrangement shown in FIGS. '1 and 2.
  • the control member 43 is adjustable in circumferential direction for instance by means of a pinion 44 and crank 45.
  • an impulse conduit 46 branches olf from the exhaust conduit 36 and leads to the diaphragm 47 of a diaphragm valve 48 which in turn storms part of the valve 49.
  • the arrangement furthermore comprises an oil pump 50 adapted to take in oil from a conduit 51 which may communicate with the lubrieating system. of the engine 35. Oil pump 50 delivers the. oil through a conduit '52, valve 49 and a conduit 53 to a servomotor piston 54 which, by means of a link system 55, is connected to the crank 45.
  • the arrangement also comprises an oil circulating conduit 56, an oil return conduit 57. and a spring 58'.
  • the oil pump 50 delivers more oil than flows oif through the oil circulating conduit 56.
  • the valve 49 and the .servornotor piston 54 have each an overflow opening through which continuously a small quantity of oil passes which returns to the circuit through the oil return conduit 57.
  • diaphragm 47 closes valve 49 against the oil pressure acting thereupon.
  • Spring 58 presses servomotor piston 54 upwardly which latter through the rod system 55 rotates crank 45 so that the control member 43 will be moved into its position for full delivery ⁇ as illustrated in FIG. 2.
  • valve 49 will be opened by the oil pressure which presses against the servomotor piston in downward direction with regard to FIG. 4.
  • the control member 43 will be adjusted in the direction of a reduction of the delivery of the compressor without the speed of the exhaust gas driven compressor dropping.
  • the exhaust gas driven compressor need not have to. be accelerated again but the control device will under the influence of the increasing exhaust gas pressure adjust the control member 43 in such a way that without. delay there will be delivered the quantity of combustion air which corresponds to the increasing requirement of the engine 35.
  • FIG. 4a shows a control arrangement according to which the control member 43 of the compressor 38 is adjusted in conformity with the speed of the engine 35.
  • the crankshaft stud 42 has mounted thereon a worm wheel 60 which drives the worm 61 of a centrifugal governor 62.
  • the governor 62 acts by means of a sleeve 63 upon the crank 64 whereby the control member 43- by means of pinion 44 is adjusted in the above described manner in order without delay to adapt the delivery of the compressor 38 to the combustion air requirement of the engine 35.
  • an operator controlled pedal or the like is provided to adapt the fuel supply to the engine to the load.
  • a control element of this nature would control, for example, a valve in the engine suction conduit or the like.
  • an exhaust gas driven motor in the form of a first rotary piston uni-t connected to'receive exhaust gas from said combustion engine
  • a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit
  • each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston units is arranged so as to be idly moved by the respective adjacent working piston
  • said second rotary piston unit including control means adjustable for controlling the delivery of said compressor, and means operatively connecting said engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.
  • each of said two working pistons is provided with a short shaft,- and in which said shafts are substantially rigidly connected to each other for rota-tion of said working pistons as a unit.
  • an exhaust gas driven motor in the form of a first rotary piston uni-t connected to receive exhaust gas from said combustion engine
  • a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit
  • each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston units is arranged so as to be idly moved by the respective adjacent working piston, each of said working pistons having a short shaft connected thereto, means rigidly interconnecting said shafts, bearing means supporting said shafts and thereby said working pistons
  • said second rotary piston unit including control means adjust-able for controlling the delivery of said compressor, and means operatively connecting said engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.
  • an exhaust gas driven motor in the form of a first rotary piston unit connected to receive exhaust gas firom said engine
  • a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit
  • each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston units is arranged so as to be idly moved by the respective adjacent working piston, said two rotary piston units being combined in a single unit
  • said second rotary piston unit including control means adjustable for controlling the delivery of said compressor, and means operatively connecting said engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.

Description

July 16,- 1963 F. w. LUCK 3,097,478
EXHAUST GAS DRIVEN COMPRESSOR Filed Sept. 28, 1960 3 Sheets-Sheet 1 In van/0r:
Flea r11- ig July 16, 1963 F. w. LUCK 3,097,473
EXHAUST GAS DRIVEN COMPRESSOR Filed Sept. 28, 1960 5 Sheets-Sheet 2 July 16, 1963 F. w. LUCK 3,097,478
EXHAUST GAS DRIVEN COMPRESSOR Filed Sept. 28, 1960 3 Sheets-Sheet 3 Unite rate ten 3,097,478 EYHAUST GAS DRIVEN COMPRESSOR Friedrich W. Liiclr, Berlin-Tegel, Germany, assignor to Eorsig Aktiengesellschaft, Berlin-Togo], and Wankel G.m.b.H., Linden, Bodeusee, Germany Fiied Sept. 28, 1%0, Ser. No. 58,946 Claims priority, application Germany Oct. 1, 1959 6 Claims. (Cl. 60-43) The present invention relates to an exhaust gas driven compressor for combustion engines which comprises a turbine or rotary piston motor driven by exhaust gases and a rotary piston blower driven by the turbine or motor, the delivery of the blower being controlled by control means.
Exhaust gas driven compressors comprising a turbine and a blower Wheel are known in which the speed of notation depends substantially on the quantity and pressure of the combustion gases being conveyed to the exhaust gas driven compressor. At low engine speed, especially at idling speed, also the speed of rotation of the compressor is low because in spite of the reduced blower pressure, the quantity of exhaust gas will not sufiice to maintain the compressor at high speed. Consequently, whenever the compressor is being started it has to be brought up first to its normal speed. In view of the low quantity of combustion gases initially available and in view of the inertia of the rotating compressor elements, this bringing up the compressor to normal speed is effected at a more or less delay with regard to the quickly increasing engine speed. Consequently, the engine will for some time during the starting phase of the compressor work under a lack of air and with rather smoky exhaust gas which is frequently not permissible, especially with street vehicles in city tr-afiic. If the turbine part were coupled to a Roots blower, the result would not be better but rather worse because the mass of the Roots rotor exceeds that of a blower wheel.
It is, therefore, an object of the present invention to provide an exhaust gas driven compressor for combustion engines which will overcome the above mentioned drawbacks.
It is another object of this invention to provide an exhaust gas driven compressor which will obviate the necessity of bringing the compressor up to speed each time the engine has idled, and would also obviate the fuming of the surroundings of the engine.
These and other objects and advantages of the invention will appear more clearly from the following specification in connection with the accompanying drawings, in which:
FIG. 1 illustrates a longitudinal section through an exhaust gas driven compressor composed of two rotary piston units combined to a unit, said section being taken along the line I--I of FIG. 2.
FIG. 2 is a cross section taken along the line II-tlI of FIG. 1.
FIG. 3 represents a rotary piston unit similar to that of FIG. 1 but with a housing sub-divided along its longitudinal extension.
FIG. 3a is a section along the line IIIa-IIIa of FIG. 3.
FIG. 4 is a diagrammatic illustration of a rotary piston unit according to the invention in connection With an internal combustion engine.
FIG. 4a is a diagrammatic representation of a control device according to which the control member of an air compressor is adjusted in conformity with the speed of the engine.
The above mentioned objects have been realized in conformity with the present invention by a rotary piston blower provided with a quantity controlling member which automatically at low engine speed or low engine output will reduce the delivery in conformity with the engine speed or the pressure of the exhaust gases. The thus reduced delivery means a reduced output of the blower or compressor and thus also a reduction in the output of the driving member thereby permitting a higher speed with the same quantity of exhaust gases.
The employment of a rotary piston unit as a blower par-t suggests to design also the driving part as rotary piston unit. The type of constructions must meet the fundamental requirement that their admissible speeds will be high and will be adapted to each other and that furthermore the blower part will be adapted to be controlled as to delivery. These conditions are met particularly favorably by rotary piston units which comprise two rotary pistons arranged one within the other and of which only the one driven rotary piston performs work, whereas the other rotary piston is idly rotated by direct contact with the driven piston or through the intervention of a pair of gears.
According to a further development of the invention, two of the above mentioned rotary piston units are em ployed While the work performing rotary pistons thereof are interconnected by coupling elements Whereas the other two rotary pistons are freely rotatable. Advantageously, the two parts of the compressor, ie the motor part and the compressor part, are combined into a unit. According to the invention, this is effected by providing each of the two work performing rotary pistons with a short shaft or stud and by connecting these short shafts or studs in a rigid and bend-resistant manner. The rotary piston combined as a unit are then journalled on the said short shafts or studs. This type of connecting the rotary pistons to each other furthermore yields the possibilities of journalling both rotary pistons in a common housing.
if desired, the work performing rotary pistons may be made of one piece but in this instance they would have to be journalled in a housing which is split in longitudinal direction. The employment of two rotary piston units according to the invention is not limited to exhaust gas driven compressors. Also prime mover and machine tools for other purposes may be connected in the same manner.
Referring now to the drawing in detail, the exhaust gas driven compressor shown in FIG. 1 has on the left-hand side thereof the driving part With the outer rotary piston 1 and the inner rotary piston '5. The blower or compressor part comprises an outer rotary piston 2 and an inner rotary piston 6. The outer rotary piston 1 is rigidly and in a bend-resistant manner connected to the outer rotary piston 2 in any convenient manner for instance by means of annular tension springs 3. The rotary pistons thus forming a unit are journ-alled in a common nonsplit housing 4.
Within the outer rotary pistons there are .arranged the humor rotary pistons 5 and 6 which do not perform any Work and which are directly rotated by the outer rotary pistons. The air inflow and outflow for both machine parts is effected through lids or covers 7 and 8, respectively. These lids also have fixedly mounted therein bearing studs 9 and 10 for the inner rotary pistons 5 .and 6 respectively. Within lid 8 there is arranged a control member 11 which for purposes of illustration has been angularly displaced into the plane of the section shown in FIG. 1.
FIG. 2 illustrates the control means and shows in dotdash lines the rotary pistons 2 and 6 which are for instance provided with six and five teeth respectively. The shaded control member 11 is designed for instance as a segment or sector which is adapted to be adjusted in tangential direction in the slot 24 in lid 8 by means operable from the outside thereof in a well-known manner. On both sides of the segment 11 there are respectit/ely provided an inlet opening 13 and an outlet opening 14. These openings are de-limi-ted by two stationary radial and by two movable radial edges. The stationary radial edge 15 determines the end of the intake cycle, whereas the stationary edge 16- releases the discharge of the compressed air.. The movable edge 17 controls the start of the intake cycle, and the movable edge 18 determines the end of the discharge or more specifically the quantity of the air conveyed into the pressure conduit. The two rotary pistons rotating in clockwise direction confine for instance working chambers 19, 2t 21, 22, 23 which increase in volume ahead of the intake opening and which decrease in volume after passing the lower dead center. If now the control member is displaced in righthand-direction and moved into the position indicated by dash lines, control edge 18 will establish communication of the pressure connection behind the outlet opening 14 with the indrawing working chambers, in the particular showing with chamber 19. Air which has already been conveyed into the pressure connection will then be able from there to flow back into the working chambers. By reexpanding of the returned quantity of air, the major portion of the compressing work employed for this quantity of air will be re-gained. The driving part of the compressor thus has to furnish substantially only the energy for the actually delivered quantity of air.
Referring now to FIGS. 3 and 3a, the housing for the rotary piston unit illustrated therein comprises an upper portion 25 and a lower portion 26. The arrangement likewise comprises an outer rotor 27 and an inner rotor 28. The outer spacing sleeve for the journalling of the inner rotor 28 is designated with the reference numeral 29 while the corresponding inner spacing sleeve is designated with the reference numeral 30. The bearing stud for the inner rotor is designated with the reference numeral 31. The housing portion for the rotary piston motor is closed by a lid 32, whereas the housing portion for the compressor is closed by a lid 33.
In the diagrammatic illustration of FIG. 4 showing a unit according to the invention in connection with an internal combustion engine, the internal combustion engine 35 is provided with an exhaust gas conduit 36 leading to the exhaust gas driven rot-ary piston motor 37 while leading from the motor 'is conduit 39. Coupled to the rotary piston motor 37 is a rotary piston compressor 38. The
compressor 38 has connected thereto an intake conduit 40 and a pressure or discharge conduit 41 which simult-aneously represents the intake conduit for the internal combustion engine 85. The internal combustion engine 35. is provided with a crank stud 42. The compressor 38 has associated therewith a control member 43 which corresponds to the control member 11 of the arrangement shown in FIGS. '1 and 2. The control member 43 is adjustable in circumferential direction for instance by means of a pinion 44 and crank 45.
As will be seen from FIG. 4, an impulse conduit 46 branches olf from the exhaust conduit 36 and leads to the diaphragm 47 of a diaphragm valve 48 which in turn storms part of the valve 49. The arrangement furthermore comprises an oil pump 50 adapted to take in oil from a conduit 51 which may communicate with the lubrieating system. of the engine 35. Oil pump 50 delivers the. oil through a conduit '52, valve 49 and a conduit 53 to a servomotor piston 54 which, by means of a link system 55, is connected to the crank 45. The arrangement also comprises an oil circulating conduit 56, an oil return conduit 57. anda spring 58'.
The oil pump 50 delivers more oil than flows oif through the oil circulating conduit 56. The valve 49 and the .servornotor piston 54 have each an overflow opening through which continuously a small quantity of oil passes which returns to the circuit through the oil return conduit 57. At full load of the engine 35, i.e. at high exhaust gas pressure, diaphragm 47 closes valve 49 against the oil pressure acting thereupon. Spring 58 presses servomotor piston 54 upwardly which latter through the rod system 55 rotates crank 45 so that the control member 43 will be moved into its position for full delivery \as illustrated in FIG. 2. If the throttle of the engine 35 is moved toward closed position, also the exhaust gas pressure drops so that valve 49 will be opened by the oil pressure which presses against the servomotor piston in downward direction with regard to FIG. 4. As a result thereof, the control member 43 will be adjusted in the direction of a reduction of the delivery of the compressor without the speed of the exhaust gas driven compressor dropping. When again accelerating the engine 35 by opening the throttle therzof, the exhaust gas driven compressor need not have to. be accelerated again but the control device will under the influence of the increasing exhaust gas pressure adjust the control member 43 in such a way that without. delay there will be delivered the quantity of combustion air which corresponds to the increasing requirement of the engine 35.
While according to the arrangement of FIG. 4 the delivery of the compressor is reduced in response to the pressure of the exhaust gas furnished by the engine when the pressure drops below a certain magnitude, the arrangement of FIG. 4a shows a control arrangement according to which the control member 43 of the compressor 38 is adjusted in conformity with the speed of the engine 35. To this end, the crankshaft stud 42 has mounted thereon a worm wheel 60 which drives the worm 61 of a centrifugal governor 62. The governor 62 acts by means of a sleeve 63 upon the crank 64 whereby the control member 43- by means of pinion 44 is adjusted in the above described manner in order without delay to adapt the delivery of the compressor 38 to the combustion air requirement of the engine 35.
With any of the illustrated arrangements, it will be understood that an operator controlled pedal or the like is provided to adapt the fuel supply to the engine to the load. A control element of this nature would control, for example, a valve in the engine suction conduit or the like. a
It is, of course, to be understood that the present invention is, by no means, limited to the particular construction shown in the drawing but [also comprises any modifications within the scope of the appended claims.
What I claim is:
1. In combination with an internal combustion engine: an exhaust gas driven motor in the form of a first rotary piston uni-t connected to'receive exhaust gas from said combustion engine, a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit, each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston units is arranged so as to be idly moved by the respective adjacent working piston, said second rotary piston unit including control means adjustable for controlling the delivery of said compressor, and means operatively connecting said engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.
2. An arrangement according to claim 1, which in cludes \a-housing common to both of said rotary piston units to thereby combine the same as a unit.
3. An arrangement according to claim 1, in which each of said two working pistons is provided with a short shaft,- and in which said shafts are substantially rigidly connected to each other for rota-tion of said working pistons as a unit.
4. In combination with an internal combustion engine: an exhaust gas driven motor in the form of a first rotary piston uni-t connected to receive exhaust gas from said combustion engine, a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit, each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston units is arranged so as to be idly moved by the respective adjacent working piston, each of said working pistons having a short shaft connected thereto, means rigidly interconnecting said shafts, bearing means supporting said shafts and thereby said working pistons, said second rotary piston unit including control means adjust-able for controlling the delivery of said compressor, and means operatively connecting said engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.
5. In combination with a internal combustion engine: an exhaust gas driven motor in the form of a first rotary piston unit connected to receive exhaust gas firom said engine, a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit, each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston units is arranged so as to be idly moved by the respective adjacent working piston, said two rotary piston units being combined in a single unit, said second rotary piston unit including control means adjustable for controlling the delivery of said compressor, and means operatively connecting said engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.
"6. In combination with an internal combustion engine: an exhaust gas driven motor in the form of a first rotary piston unit connected to receive exhaust gas from said combustion engine, a compressor in the form of a second rotary piston unit drivingly connected to said first rotary piston unit, each of said rotary piston units comprising two rotary pistons one arranged within the other, one piston only of each of said rotary piston units being a working piston while the other rotary piston in each of said rotary piston uni-ts is arranged so as to be idly moved by the respective adjacent working piston, said working pistons consisting of a single piece, a longitudinally split housing surrounding all of said pistons and having the same journalled therein, said second rotary piston unit including control means adjustable for controlling the delivery of said compressor, and means operatively connecting said combustion engine with said control means for causing the latter to reduce the delivery of said compressor in response to the pressure of said exhaust gas furnished by said combustion engine dropping below a certain magnitude, whereby an undue drop in the speed of said compressor is avoided.
References Cited in the file of this patent UNITED STATES PATENTS 1,856,024 Buchi Apr. 26, 1932 2,217,364 Halford et a1. Oct. 8, 1940 2,480,621 Warner Aug. 30, 1949 2,559,623 Holmes July 10, 1951 2,656,675 Coat Oct. 27, 1953 2,838,907 Oowland June 17, 1958

Claims (1)

1. IN COMBINATION WITH AN INTERNAL COMBUSTION ENGINE: AN EXHAUST GAS DRIVEN MOTOR IN THE FORM OF A FIRST ROTARY PISTON UNIT CONNECTED TO RECEIVE EXHAUST GAS FROM SAID COMBUSTION ENGINE, A COMPRESSOR IN THE FORM OF A SECOND ROTARY PISTON UNIT DRIVINGLY CONNECTED TO SAID FIRST ROTARY PISTON UNIT, EACH OF SAID ROTARY PISTON UNITS COMPRISING TWO ROTARY PISTONS ONE ARRANGED WITHIN THE OTHER, ONE PISTON ONLY OF EACH OF SAID ROTARY PISTON INE ACH OF A WORKING PISTON WHILE THE OTHER ROTARY PISTON IN EACH OF SAID ROTARY PISTON UNITS IS ARRANGED SO AS TO BE IDLY MOVED BY THE RESPECTIVE ADJACENT WORKING PISTON, SAID SECOND ROTARY PISTON UNIT INCLUDING CONTROL MEANS ADJUSTABLE FOR CONTROLLING THE DELIVERY OF SAID COMPRESSOR, AND MEANS OPERATIVELY CONNECTING SAID ENGINE WITH SAID CONTROL MEANS FOR CAUSING THE LATTER TO REDUCE THE DELIVERY OF SAID COM-
US3097478D Exhaust gas driven compressor Expired - Lifetime US3097478A (en)

Publications (1)

Publication Number Publication Date
US3097478A true US3097478A (en) 1963-07-16

Family

ID=3451640

Family Applications (1)

Application Number Title Priority Date Filing Date
US3097478D Expired - Lifetime US3097478A (en) Exhaust gas driven compressor

Country Status (1)

Country Link
US (1) US3097478A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3229895A (en) * 1964-09-29 1966-01-18 Ingersoll Rand Co Means of loading and controlling reciprocating expansion engines
US3603079A (en) * 1968-08-22 1971-09-07 Ernst Kickbusch Supercharged internal combustion engine, particularly supercharged diesel engine for vehicular drives
JPS5752638A (en) * 1980-09-17 1982-03-29 Mazda Motor Corp Supercharging pressure control device for engine with supercharger
JPS5756625A (en) * 1980-09-19 1982-04-05 Mazda Motor Corp Superchange pressure controller for engine with supercharger
JPS58180724A (en) * 1982-03-03 1983-10-22 フエリツクス・ウエンケル Rotary piston supercharger

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3229895A (en) * 1964-09-29 1966-01-18 Ingersoll Rand Co Means of loading and controlling reciprocating expansion engines
US3603079A (en) * 1968-08-22 1971-09-07 Ernst Kickbusch Supercharged internal combustion engine, particularly supercharged diesel engine for vehicular drives
JPS5752638A (en) * 1980-09-17 1982-03-29 Mazda Motor Corp Supercharging pressure control device for engine with supercharger
JPS605773B2 (en) * 1980-09-17 1985-02-14 マツダ株式会社 Boost pressure control device for supercharged engines
JPS5756625A (en) * 1980-09-19 1982-04-05 Mazda Motor Corp Superchange pressure controller for engine with supercharger
JPS605772B2 (en) * 1980-09-19 1985-02-14 マツダ株式会社 Boost pressure control device for supercharged engines
JPS58180724A (en) * 1982-03-03 1983-10-22 フエリツクス・ウエンケル Rotary piston supercharger

Similar Documents

Publication Publication Date Title
US2519913A (en) Helical rotary compressor with pressure and volume regulating means
US3270495A (en) Apparatus for controlling speed and vibration of engine turbochargers
US3066488A (en) Power output control for a gas turbine engine
US2968914A (en) Turbocharging of internal combustion engines
US4157011A (en) Gas turbine flywheel hybrid propulsion system
US3771921A (en) Reactor air pump drive system
EP0048027A2 (en) Turbo-compound internal combustion engine
US2296268A (en) Charging device for internal combustion engines
US3238713A (en) Compound engines for motive power
US3232043A (en) Turbocompressor system
US2245163A (en) Power plant for aircraft
US3097478A (en) Exhaust gas driven compressor
US2386096A (en) Supercharger
US3603079A (en) Supercharged internal combustion engine, particularly supercharged diesel engine for vehicular drives
US2724340A (en) Rotary pump
US2172100A (en) Internal combustion engine
GB1037347A (en) Improvements in or relating to turbocharged two stroke cycle internal combustion engines of the compression ignition type
US3314232A (en) Gas turbine engine with aerodynamic torque converter drive
US3157993A (en) Starter arrangement
US3085392A (en) Internal combustion engines
US3490229A (en) Turbine-powered prime mover
US4362014A (en) Rotary machines and power systems using said machines
US3382855A (en) Torque converters and power plants
US2845774A (en) Gas turbine operatively associated with a piston engine-compressor unit
US3647327A (en) Circular piston internal combustion machine with reduced short circuit flow