US3905198A - Rotary thermal engine - Google Patents

Rotary thermal engine Download PDF

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Publication number
US3905198A
US3905198A US407129A US40712973A US3905198A US 3905198 A US3905198 A US 3905198A US 407129 A US407129 A US 407129A US 40712973 A US40712973 A US 40712973A US 3905198 A US3905198 A US 3905198A
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Prior art keywords
source
chambers
chamber
thermal engine
heat
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Expired - Lifetime
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US407129A
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English (en)
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Claude Malaval
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00—Hot gas positive-displacement engine plants
    • F02G1/04—Hot gas positive-displacement engine plants of closed-cycle type
    • F02G1/043—Hot gas positive-displacement engine plants of closed-cycle type the engine being operated by expansion and contraction of a mass of working gas which is heated and cooled in one of a plurality of constantly communicating expansible chambers, e.g. Stirling cycle type engines
    • F02G1/053—Component parts or details
    • F02G1/055—Heaters or coolers
    • 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
    • F01C7/00—Rotary-piston machines or engines with fluid ring or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/04—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being formed by spirally-wound plates or laminae
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G2258/00—Materials used
    • F02G2258/10—Materials used ceramic

Definitions

  • the present invention concerns a rotary thermal en gine drawing away a drive fluid, in a closed circuit according to a cycle almost similar to the Stirling cycle.
  • Such a device requires elements for transforming the rectilinear movement of the piston into a rotating movement of the drive shaft leading to an appreciable increase in the weight and the price of the device.
  • such an engine implements piston rings operating at high temperature whose reliabiliy is still sometimes haphazard.
  • the inventor has preferred to use the principle of the rotating engine, thus avoiding, moreover, the use of in termediate elements for transforming the rectilinear movement into a circular movement. It is indeed a known practice to use a stator having a definite geometrical shape, within which a rotor limiting, with the stator, during its rotation, chambers having a variable volume, is made to rotate but all the sealing and cooling problems set by devices of that type are also known.
  • the inventor has overcome these various difficulties by implementing chambers one of whose walls is constituted by a portion of liquid ring obtained by driving in a rotating movement the liquid contained in a cylindrical body having a horizontal axis by means of a flash wheel also having a horizontal axis but excentric in re' lation to the axis of the cylindrical body in the same way as a compressor or pump of the liquid ring type.
  • the chamber is limited by two blades, by the portion of liquid ring which they determine and by two lateral rims perpendicular to the blades.
  • the chamber is all the smaller as the two blades which limit it on two sides are immersed deeper in the liquid ring.
  • the variation of the volume of the chamber is therefore effected without any seal or friction other than that of the liquid ring driven by the rotation of the blades and remaining very slight.
  • the inventor has constituted a rotating thermal engine by combining a certain number of such cylindrical bodies in which a fluid flows in a closed circuit. That fluid is at least partly put into contact with a hot source and a cold source according to the cycle almost similar to the Stirliing cycle.
  • the object of the invention is a rotating thermal en gine constituted by a hot source, a cold source, a cylindrical volume, several flash wheels fltted with lateral rims and a certain quantity ofliquid, the axis of the said flash wheels being parallel and excentric in relation to the axis of the cylindrical volume, the rotation of each flash wheel giving rise to a liquid ring, limiting, with the rims of the said wheel, a cylindrical body which the successive blades divide up into chambers having a vari able volume, characterised in that a drive fluid moves in a closed circuit comprising the hot source and the cold source arranged outside the cylindrical bodies.
  • rotating internal combustion engines have the disadvantage of produc ing particularly polluting gases when they operate at low speed.
  • the chamber itself rotates on the axis and only the wall formed by the portion of liquid ring moves forward or backward in a radial direction it is therefore easy to choose the place at which the injection is to be made.
  • the very structure of the engine then allows the drive fluid to be brought close to the heat source and to re-inject it in the best output conditions, whatever the speed of rotation of the engine may be and to avoid causing a correlation between the rotation speed of the engine and the combustion rate of the heating gases of the hot source.
  • the object of the invention is therefore also a rotat ing thermal engine of the closed circuit type, constituted according to the preceding description, characterised in that communication means enable at least a part of the gases to be drawn off successively from each chamber at the instant when the latter takes up the minimum volume to re-inject them in a chamber having an increasing volume after having put them in contact with the hot source.
  • the drive fluid is therefore drawn off successively from the chambers at an instant when these latter take up the minimum volume to lead it into an exchanger device forming the hot source where the drive fluid is heated then sent back into a chamber whose volume is increasing so that this hot fluid provides drive force during its expansion.
  • An engine according to the invention operates between a hot source with which the drive fluid drawn off from the chamber taking up the minimum volume is put in contact and a cold source with which the cold fluid drawn off during compression is put in contact to re-inject it into the chamber taking up the maximum volume.
  • the object of the invention is therefore also a thermal engine constituted according to the preceding descriptions. characterised in that means enable a part of the drive fluid in the chambers in the compression phase to be drawn off, the said fluid to be put in contact with the said cold source and sent back into the following chambers at the instant when the compression is the lowest.
  • liquid ring does not heat up permanently and does not have a tendency to become vaporized as circumstances may lead it to be believed. Indeed, the direct contact with the hot gases takes place only during a short fraction of the revolution cycle, moreover by means of the smallest surface,
  • FIG. 1 is a perspective view, partially in section, showing diagrammatically the central part of the engine of the present invention
  • FIG. 2 is a diagrammatic cutaway view showing the connecting of the central part of the engine of FIG. 1 to the two sources.
  • FIG. 3 is a sectional view of the engine of FIGS. 1 and 2 showing the feeding of the chambers with drive fluid.
  • FIG. 1 shows diagrammatically the central part of an engine implementing a variant of the invention which comprises two cylindrical bodies having four chambers arranged in a line on the same shaft, arranged in the same cylindrical volume I.
  • a cylindrical volume through which a shaft 2 passes may be distinguished at l.
  • the cylindrical volume is therefore constituted by two coaxial cylindrical bodies 3 and 4 having the same diameter.
  • the cylindrical body 3 is limited by the sides 5 and 6.
  • the cylindrical body 4 is limited by the sides 7 and 8.
  • Each of the sides supports respectively the bearings 9, l0 and I] of shaft 2.
  • the sides 5 and 7 made fast with each other by the bearing 10 constitute a volume containing ducts and the hub of which descriptions are given further on.
  • the existence of the blade 12 constituting a wall common to two contiguous chambers and in the cylindrical body 4, the existence of the blade 13 fulfilling, in the body 4, the same function as the blade 12, will be observed.
  • the blade I2 bears rims l4 and I5 and the blade 13 bears the rims l6 and 17.
  • Flexible elements I8 and 19 put the rims l5 and 16 of the blades 12 and 13 in contact respectively with the sides 5 and 7.
  • a pipe 2] enabling the drive fluid to be drawn off at the instant when the chamber reaches the minimum volume is arranged between the sides 5 and 7.
  • a pipe 22 enables the fluid to be re-injected after its pass at the hot source (not shown in this figure).
  • a pipe 23 enabling a part of the fluid to be drawn off towards the cold source (not shown in that 25 and to the cold source 25'.
  • the tubes 27 and 28 are welded along two generating lines to tubes 40 greatly flattened and wound in a spiral.
  • Each flat tube 40 is reinforced by oblique steel wires 40' arranged in a regular pitch. These wires are fixed to the flat tubes 40.
  • the spiral of the flat tubes such as 40 ends at the centre of the hot source in a central tubing 29 whence other flat tubes such as 40 wound in the reverse direction leave.
  • the burner 31 is arranged at one end of the central tubing 29.
  • the liquid fuel is sent by the sprayer 32 towards a heating grill 33 constituted by a metallic strip 66 insulated by ceramic elements 67. That spiral coil is heated when the engine is started up by Joule effect by means of a storage cell battery (not shown).
  • the spiral winding vapourizes the fuel.
  • the air sucked in by the nozzle 34, flowing between the collar 30 and the casing 26 is heated and burns with the fuel.
  • the combustion gases escape through the tubing 35 after having heated the drive fluid flowing in the flat tubes 27 and 28.
  • the device acting as a heat source enables the use of very thin tubes 27 and 28 making thermal exchanges with the hot source easier. Indeed, the pressures brought into play are retransmitted by means of the steel wires up to the outside collar 30 made of a metal which is sufficiently thick to bear the whole of the pressure obtained in the tubing by means of the hot source.
  • the cold source 25' constituted in the same way as the hot source 25, is fed with cooling fluid.
  • the pipes 23 and 24 widen out respectively into the tubes 37 and 38 to form, subsequently, flat spiral tubes as in the hot source. They are connected up by the central duct 36.
  • a by-pass valve 41 whose shutter 41' is linked with the adjusting of the combustion discharge is arranged between the tubes 21 and 22. That arrangement enables the hot source 25 to be maintained at a high temperature when the burner and the engine operate at low speed and cancels, simultaneously. the effects of thermal inertia.
  • FIG. 2 makes it possible to understand the principle of the feeding of the chambers by the hot source 25 and the cold source 25'.
  • the lateral rim 15 does not bear with all its surface against the left-hand face of the side 5. A certain gap appears on the peripherical part although the spring 18 may tend to press the blade wheel against the wall 7. Indeed, the wall 5 has, at its central part, a hub 20 drilled at certain places with circular ports 6].
  • Each of the circular ports such as 61 is in relation with one of the pipes such as 21, 22, 23 or 24 (FIG. 1 or 2).
  • a port such as 71 of the lateral rim comes opposite a port of a boss such as 61, a communication between the source and the chamber of the engine is established.
  • a port such as 72 in the rim 16 does not establish any contact with a source.
  • FIG. 3 shows a cross-section of the engine; a profile of one of the blades [2 driving the liquid contained in the cylindrical body limited by a circle 4 shown in dotted lines may be seen therein.
  • the liquid forms. in its turn, a cylindrical wall whose inside face is limited by the dotted line 45.
  • the blades 12, 46, 47 and 48 limit, with the wall of the liquid ring 45, four chambers 51, 52, 53 and 54, the two lateral faces of these chambers being limited by rims such as 14 and 15 (HO. 1 or FIG. 2).
  • Circular ports formed in the boss 20, connected up respectively to the pipes 21 and 22 feeding the hot source have been shown at 61 and 62.
  • Ports formed in the boss 20, connected up respectively to the pipes 23 and 24 have been shown at 63 and 64.
  • the circular port 72 drilled in the lateral rim is seen in the chamber 52.
  • One such feed port exists per chamber, the chamber 53 being provided with the opening 73.
  • four circular ports are drilled in the boss 20, in constant communication with one of the four feed pipes of the two sources.
  • four circular ports are drilled in the lateral rims in contact with the central sides 5 and 7, each port in turn putting the chamber to which it corresponds in communication, during a short period, with the hot gas inlet, the cold gas outlet, the cold gas inlet, the hot gas outlet.
  • the chamber having a variable volume receives, by the port 63, a certain quantity of fluid cooled by the cold source 25'.
  • a part of the fluid is drawn off by the port 64 in the chamber having a variable volume is pointed towards the cold source by the pipe 23.
  • the fluid supplies, in each chamber having a variable volume, a drive force during the whole of the expansion of the fluid, that is, from the pressing of the port of the chamber in front of the fixed port 62 until it passes in front of the fixed port 63.
  • the pressure in the chamber is higher than in the chamber which preceeds it the result of this is an action on the wall of the liquid ring which tends to move the latter in the rotating direction of the engine.
  • a part of the energy thus supplied is recuperated by means of fins such as 12' (FIG. 3) or 46' (FIGS. land 3) which produce a drive of the wheel in the direction of its rotation.
  • the device according to the invention has been described hereinabove with two cylindrical bodies installed on the same shaft. It is self-evident that it is also possible to install only one or more than two, for example, four, six or eight, without going beyond the scope of the invention. Likewise, bodies comprising four blades limiting four chambers have been described. The inventor has also made experiments on cylindrical bodies containing six and eight chambers, which could be a greater advantage if it is required to drive a device having low inertia which must nevertheless be actuated with a very regular movement. Applications for such an engine are particularly numerous. This engine gives high power for a low volume moreover, it adapts itself very well to a variable speed rate.
  • a cylindrical rotating thermal engine comprising: a cylindrical casing, a quantity of liquid within said casing, a source of heat exterior of said cylindrical casing, a source of cold exterior of said cylindrical casing, a plurality of wheels inside said casing mounted for rotation therein, each of said wheels bearing radial vanes fitted with lateral rims, the axis of said wheels being parallel and eccentric in relation to the axis of the cylindrical casing,
  • said propellant directing means includes first means communicating said chambers with the source of heat during a predetermined interval of time.
  • said propellant directing means includes a second communication means for placing a fraction of the propellant in communication with the cold source during a predetermined time interval.
  • thermo engine of the closed circuit type according to claim 2 wherein the heat source communicating means includes means for drawing off at least a part of the gases from each chamber at the in stant when the latter takes up minimum volume and putting said gases into contact with the source of heat and reinjecting them into a chamber whose volume is increasing.
  • said second communication means includes means for drawing off a part of the gases from the chambers having a variable volume during compression and putting them into contact with said cold source and means for reinjecting said gases into a chamber whose volume at that moment is maximum.
  • the propellent directing means enabling a part of the gas system to be drawn off from or injected into chambers having a variable volume, comprises: a hub, four bores formed in the casing sides in the vicinity of the hub, heat exchangers external to the casing forming said hot and cold sources and ducts communicating the heat exchangers with said bores, and wherein a lateral rim of each chamber is provided in the vicinity of the hub with a circular portion communicating said chambers with said heat exchangers when the circular port comes in alignment with a corresponding bore formed within the side of the cylindrical casing.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
US407129A 1972-10-19 1973-10-17 Rotary thermal engine Expired - Lifetime US3905198A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US05/518,119 US3972370A (en) 1972-10-19 1974-10-25 Hot source having slight bulk

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7237041A FR2204214A5 (cg-RX-API-DMAC7.html) 1972-10-19 1972-10-19

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US05/518,119 Division US3972370A (en) 1972-10-19 1974-10-25 Hot source having slight bulk

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US (1) US3905198A (cg-RX-API-DMAC7.html)
JP (1) JPS4973549A (cg-RX-API-DMAC7.html)
DE (1) DE2351370A1 (cg-RX-API-DMAC7.html)
FR (1) FR2204214A5 (cg-RX-API-DMAC7.html)
GB (1) GB1422817A (cg-RX-API-DMAC7.html)
IT (1) IT995729B (cg-RX-API-DMAC7.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140147244A1 (en) * 2010-11-23 2014-05-29 The Ohio State University Liquid ring heat engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008010059A1 (de) * 2008-02-20 2009-08-27 Peter Holl Vorrichtung und Verfahren zur Gewinnung von mechanischer Energie aus der Temperaturdifferenz zwischen einer Wärmequelle und einer Wärmesenke

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1429044A (en) * 1921-02-23 1922-09-12 Nash Lewis Hallock Turbo displacement motor
US3190072A (en) * 1964-10-20 1965-06-22 Berryer Pierre Turbine engine
US3495402A (en) * 1968-01-18 1970-02-17 John W Yates Power system
US3589126A (en) * 1969-04-04 1971-06-29 Theodore Zotto Power system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1429044A (en) * 1921-02-23 1922-09-12 Nash Lewis Hallock Turbo displacement motor
US3190072A (en) * 1964-10-20 1965-06-22 Berryer Pierre Turbine engine
US3495402A (en) * 1968-01-18 1970-02-17 John W Yates Power system
US3589126A (en) * 1969-04-04 1971-06-29 Theodore Zotto Power system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140147244A1 (en) * 2010-11-23 2014-05-29 The Ohio State University Liquid ring heat engine
US9540936B2 (en) * 2010-11-23 2017-01-10 Ohio State Innovation Foundation Liquid ring heat engine

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Publication number Publication date
FR2204214A5 (cg-RX-API-DMAC7.html) 1974-05-17
JPS4973549A (cg-RX-API-DMAC7.html) 1974-07-16
GB1422817A (en) 1976-01-28
IT995729B (it) 1975-11-20
DE2351370A1 (de) 1974-05-09

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