US1968113A - Rotary engine or the like - Google Patents

Rotary engine or the like Download PDF

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US1968113A
US1968113A US472715A US47271530A US1968113A US 1968113 A US1968113 A US 1968113A US 472715 A US472715 A US 472715A US 47271530 A US47271530 A US 47271530A US 1968113 A US1968113 A US 1968113A
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rotors
rotor
pockets
teeth
casing
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US472715A
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Eastman A Weaver
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Comstock and Wescott Inc
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Comstock and Wescott Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/008Driving elements, brakes, couplings, transmissions specially adapted for rotary or oscillating-piston machines or engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/08Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/10Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member
    • F01C1/103Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing of internal-axis type with the outer member having more teeth or tooth-equivalents, e.g. rollers, than the inner member the two members rotating simultaneously around their respective axes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00Sealing arrangements in rotary-piston machines or engines
    • F01C19/08Axially-movable sealings for working fluids

Definitions

  • This invention relates to improved forms of fluid pressure apparatus, such as'compressors, pumps, and pressure fluid motors or engines. Certain aspects of the invention pertain generally to the improvement of fluid pressure apparatus of a type wherein fluid is pocketed and compressed and/or expanded, while a further aspect of the invention pertains to the provision and arrange.- ment of improved pressure fluid apparatus of this general character for use as an internal combustion motor. y
  • the present invention provides fluid pressure I apparatus having a plurality of rotors which cooperate in aifording fluid pockets movable from a region of maximum capacity to a region of minimum or substantially no capacity.
  • these pockets may be provided between a plurality of eccentrically disposed toothed rotors,
  • each tooth is constantly in engagement with a portion of the adjoining rotor.
  • an outer rotor or casing may be provided with internal teeth which intermesh with the teeth of a smaller eccentrically mounted inner rotor, the latter preferably being in the form of a tortuous annular shell, the tortuosities of which form internal as well as-external teeth, and preferably having its internal teeth in engagement with the external teeth of a still smaller rotor.
  • This arrangement permits the employment of several rotors arranged one within the other and each having teeth in mutual engagement with an adjoining rotor or rotors, thereby providing a fluid apparatus of given size with a comparatively large-volumetric capacity, despite the limited size of the fluid pockets formed between the points of contact of the tooth portions of adjoining rotors; furthermore, the rotors thus arranged provide a series of pockets, each pocket moving in a substantially annular circuit between a region of maximum capacity and a region of minimum or substantially nil capacity. .All of the moving parts of the apparatus may have a true rotary motion,
  • the apparatus is'adapted to have a substantially uniform torque whether used as a compressor or pump or as a motor, and the parts of the apparatus may be free from sudden changes in pressure or shoclrs, and due to the relatively uniform and gradual changes in stresses, the apparatus may be relatively light.
  • the parts which determine the positioning of the rotational axes of the rotors preferably may be so disposed and mounted that a slight increase in the distance between the axes of the rotors may occur in response to heat expansion.
  • the rotors may be associated with substantially fixed end plates which assist in defining the fluid pockets and provide openings for the ingress and egress of fluid; preferably at least one of these end plates may be associated with means to maintain asubstantially constant frictional engagement between the same and the rotors, despite thermal expansion of the rotors, wear or other changes of dimensions.
  • one end plate or bearing part may have a slight rotational movement in response to the frictional drag of the rotors and may have a corresponding but much smaller outward movement so that as the frictional drag between the rotors and bearing part tends to increase the bearing'part or wall may have a slight movement anally away from the rotors, tending to decrease its frictional engagement therewith.
  • Fluid apparatus of this character may be particularly advantageously employed as an internal combustion motor which, for example, may employ a Diesel or semi-Diesel cycle.
  • Air may be introduced into the fluid pockets at or near their region of substantially maximum capacity, the air being compressed as the pockets pass toward the region of minimum capacity and being emitted into-a stationary combustion chamber which communicates with the pockets at both sides oi the plane of the eccentric axes.
  • the compressed air is mixed with combustible material, such as a suitable liquid hydrocarbon mixture, and the burning gases are emitted from this chamber into the expanding pockets, thereby tending to increase the. volume of the latter and converting the gas pressure energy into energy of rotational movement of the rotors.
  • the end walls may be broken away adjoining the region of maximum pocket capacity, thus permitting cooling of the rotors and the ready movement of the burnt gases out of the pockets and the replacement of the same by fresh air.
  • the apparatus preferably may .be associated with blast inducing me, such as a blower or an' airreciprocating movement results in a substantiallyv constant torque, which may be more umiorm than attainable even from multi-cylinder engines of the reciprocating type.
  • the movement of an airblast over and between the rotors is efiective not only in thoroughly scavenging burnt gases, filling the pockets with fresh sir and giving the elsperetus a high volumetric csoscity, but the air bio. is also effective in cooling the rotors without the necessity for special cooling; means.
  • Fig. l. is e. side elevotiomel View oi my improved fluid pressure spporotus
  • Fig. s is e sectional vies. of the rotors end at coo'giereting driven seer;
  • Fig. i is so elevetionol of a eorticn of one of the end pistes
  • Fig. 5 is s. sectioned detell showing the orrsngemcnt of the mes-es for holding the end plates in proper eiigesement with the rotors;'
  • Fig. d is e. dios'remmstic view showing the rmer in which the rotor teeth may be laid out.
  • the raw merol l desigriotes e. suitelole support for tire rotors and related psrts, which may include s plsner upper portion 2, that may be secured to any suit able supporting port, and psrellel depending pistes 7 and t which preferably may loe integral with the planar 2.
  • a suitable sxiol member 9, extending; between pistes 7 end s, may carry an inner rotor id which may be substantially in the ml of a. pinion lievlmj external teeth 12.
  • the apparatus ll provide one or more intermediate rotors in the former? tortuous sd'lriuler shells, one of which is shown in tlie ecccmperiyiris end lsdesigneted Toy the numeral l5. This shell preferably pro vides internal end external tee-til l6 end 17, which mesh with. the testis. l2 end M, respectively, oi
  • the teeth t the rotors are designed continually to emsege eocli other throughout their movement. Iii other words, each tooth lies e substantially con tinsel line contact with the adjoining rotor, the teeth holes in deeply or closely meshed e2igsgemeet at the region. of minimum pocket capacity, i. e. in the plene of the sizes oi the rotors. Since the teeth contact in this monitor, it is evi dent the shell 15 mew ice held in position oetween the rotor ill end time casing 25 Without need for any additional support.
  • Suitable means is provided to support and detlie oi rotation oi the outer casing 25, such mes-sis comprising a. plurality of pairs on? rollers Ell sod Elliv/liicli lisve extensions 21. end 1239 supported by the plates '3 8.
  • sheit 129 is carried in bearing clocks 12d slidololy mounted in slots 127 in the plates 'l and 8, heavy coil springs being disposed in the support 1 to urge the blocks 12% and the slisit 129 downwardly, thereby yieldsloly holding the rotors in closely meshed engagement seed yield ably determining the relative position or spacing of their eccentric axes.
  • the rotors may directly engage one ol the depemliris plates of the support 1, such as the plate l, while the plate s may be spaced from the other ends of the rotors, and s. special form oi. end plate 31 having e. rotary mounting upon the shafts may be disposed between the plate t and the rotors.
  • a tension spring 3 3 preferably connects en extension or eer 33 imam the plots fill and s fixed part of the support 1, thereby tending to oppose end restrain the rotational movement oi piste 31 about exiel support 9 in response to the frictions].
  • the outer time of the piste 3i met" be provided with one or more circumierentielly inclined recessed portions or surfaces 32 which incline outwardly in the di rectlcri of rotor movement.
  • a bell 38 mounted.
  • e recess 35 in the plots 3 may be engaged by the socket oi. a. retaining out so, the bell time being held against the inclined surface 32, end time tending to hold the plate 39 amidst the ro tors.
  • the bell 88 is pressed outwardly into erreasement with s deeper portion oi the recess 32, and the pressure of time spring 3% is less; eccord ingly the force with which the piste 31 is held against the rotors is eutometicelly rediii'sed es the piste turns against the sctlon of spring 3% iii resnonse to frictional dr es.
  • a circle I) of similar diameter is then rolled about the hypocycloidal figure B to define the internal teeth of the shell 15.
  • a circle of larger diameter, designated E, is then rolled about the same hypocycloidal figure B to define the external teeth of the rotor 15. It is thus evident that the rotor 15 may be made in the form of a tortuous annular member having constant thickness and that the diameters of the circles D and E difier by the desired thickness of the shell.
  • the circle E is then rolled about the outer hypocycloidal figure A to define the internal teeth of the casing 15. Obviously the same method of procedure may be employed when more than one intermediate shell is provided.
  • the apparatus as thus far described may be adapted for a wide variety of purposes by the provision oi suitable ports in one or both of the end plates. It is evident, for example, that the device may be used as a pump or a compressor, or as a motor driven by pressure fluid, such as steam or compressed air. an especially vantageous arrangement of the apparatus, however, permits its employment as an eiflcient, compact,light, internal combustion engine having easy starting characteristics and uniform torque.
  • a combustion chamber t1 which preferably may be lined with refractory material 42, may be disposed in the end plate '7, this chamber preferably having an open side communicating with the fluid pockets in the region oi their minimum capacity and having a limited extent at the side of the plane of the axes of the rotors where the pockets are contracting in volume and having a greater extent at the opposite side of this plane, the shape of the pocket being shown, for example, in Figs. 1 and 3.
  • the pocket does not extend inwardly beyond the pitch circle for the shell 15.
  • the lower parts of the plates 7, 8 and 31 may be broken away, as designated by numeral so, so that the ends of the fluid pockets are open to the atmosphere when maximum capacity.
  • the out-away portion of the walls extends farther in the direction of pocket contraction than in the direction of pocket expansion, as shown in Fig. 1, although this arrangement may be diminished or reversed to provide a superchanging effect, if desired.
  • the cut-away portion may be arranged so that a much higher maximum compression of the charge could be attained than would be the case with the arrangement or its edge adjoining the contracting pocket portions in the position shown in Fig. l.
  • a suitable may continuously supply iuel such as a suitable oil through a duct 44 to the combustion chamber. A valve they are in their region of.
  • a blower 53 may be arranged to supply a blast of air to the open ends of the pockets .at the lower part of. the apparatus. Under these conditions the pockets will be filled with air when they are in their regions ofmaximum capacity and then will contract, compressing the air until the air can pass into the charge chamber 41.
  • The-pressure existing in the charge chamber may be suflicient to ensure ignition oi. the mixture of fuel and air, and accordingly the same may pass out of the larger opening at the right of the axial plane, as viewed in Fig. 3, into the expanding pocket.
  • the pressure to which the pockets are subjected is thus greater upon the expansion side of the device and produces a net torque moving the rotors and abstracting work from the combustion gases.
  • the pockets come into communication with the openings provided by the broken-away portions of the end walls and the burnt gases are free to escape.
  • the force of the air blower 50, the propeller or the like aids in scavenging the pockets of gas, and ensures filling of the same with fresh air, which is again compressed as the pockets contract and pass between the closed wall portions, and the cycle is repeated.
  • timing means need be provided for such a spark plug but that it may be supplied with high tension current in any suitable manner, for example, by any make and break-systern. Starting of the motor may be readily ef-- which it may be delivered to any suitable point.
  • the yieldable mounting of the shafts 9 and 129 is particularly advantageous when the apparatus is to be employed as a motor due to the high temperatures developing in the device and consequent heat expansion. Furthermore, this arrangement ensures the correct tghtness of engagement of the rotor teeth at the high pressure portion of their cycle whether new or worn, and whether copiously or sparingly lubricated.
  • the yieldable mounting of the end plate 31 is also advantageous to permit the device efllciently to operate under various thermal conditions and have its'high pressure portions remain substantially fluid tight. Furthermore, the cooling of the rotors is ensured by the constant blast 0! cool air supplied to their exposed portions at the low pressure part of the apparatus.
  • the cooled rotors accordingly are effective in receiving heat from the hot end walls and thus especially in cooling these portions of the device, although it is evident that these parts oi the apparatus may advantageously reach a relatively high temperature, thus aiding thethermal emciency of the engine without interiering with its mechanical efliciency.
  • Apparatusof the class described comprising a rotatable casing having internal teeth, a rotor eccentrically mounted in the casing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and cas-' ing respectively, said shell being disposed eccentrically between. the rotor and the casing, and side-walls at the end of the casing, said walls cooperating with the rotor and shell in providing one set of fluid pockets and with the casing and shell in providing another set of fluid pockets.
  • Apparatus of the class described comprising a rotatable casing having internal teeth, a rotor eccentrically mounted in the casing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and casing respectively, said shell being disposed eccentrically between the rotor and the casing,
  • Apparatus of the class described comprising a rotatable casinghaving internal teeth, a rotor eccentrically mounted in the casing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and casing respectively, said shell being disposed eccentrically between the rotor and the casing with its central axis disposed in the plane of the axes of rotation of the rotor and easing, the teeth of the rotor meshing with the internal teeth of the shell and the teeth of the casing meshing with the external teeth of the shell in the"region of said plane, and side walls at end of the casing, said walls cooperating with the rotor and shell in providing one set of fluid pockets and with the casing and shell in providing another set of fluid pockets.
  • Apparatus of the class described comprising a rotatable casing having internal teeth, a rotor eccentrically mounted in thecasing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and casing respectively, said shell being eccentrically mounted in relation to the rotor and the casing with its central axis disposed in the plane of the axes of rotation of the rotor and easing, the teeth of the rotor closely meshing with the internal teeth of the shell and the teeth of the casing closely meshing with the external teeth of the rotor in the region of said plane, and side walls at end of the casing, said walls cooperating with the rotor and shell in providing one set of fluidpockets and with the casing and shell in providing another set of fluid pockets, a combustion chamber adjoining the region where the teeth mesh. closely, and said chamber communicating with the pockets at each side of said plane.
  • a motor comprising an outer rotatable casing, an inner rotor, and an intermediate annular member, said casing, rotor and annular member each having axes of rotation eccentric in relation to each other and in substantially the same plane, the rotor, annular member, and casing cooperating in providing pockets successively moving through a continuous circuit between a region of minimum volume and a region of maximum volume, a combustion chamber communicating with the pockets in the region of minimum volume on each side of said plane and means for supplying fuel to said chamber, and means to supply fresh air to the pockets in their region of maximum capacity and to permit the movement of gases of combustion therefrom.
  • a motor comprising an outer rotatable casing, an inner rotor, and an intermediate annular member, said casing, rotor, and annular member each having axes of rotation eccentric in relation to each other and in substantially the same plane, the rotor, annular member and casing cooperating in providing pockets successively moving through a continuous circuit from a region of minimum volume to a region of maximum volume, a combustion chamber communicating with the pockets in the region of minimum volume on each side of said plane, and means for supplying fuel to said chamber, end walls cooperating with casing, shell and rotor in providing said pockets, said walls having opposite openings to permit the exhaustion of burnt gases from the pockets and inflow of air thereto in the region of maximum pocket capacity.
  • a motor comprising an outer rotatable casing, an inner rotor, and an intermediate annular member, said casing, rotor and annular member each having axes of rotation eccentric in relation to each other and in substantially the same plane, the rotor annular member and casing cooperating in providing a series of pockets successively moving through a continuous circuit from a region of minimum volume to a region of maximum volume, a combustion chamber communicating with the pockets in the region of minimum volume on each side of said plane, and means for supplying fuel to said chamber, end walls cooperating with casing, shell and rotor in providing said pockets, said walls having opposite openings to permit the exhaust of burnt gases and inflow of air in the region of'maximum pocket capacity, and draft inducing means for purging the pockets of burnt gases and filling them with fresh air.
  • Apparatus of the class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation suband the regions of minimum capacity of each of the series of pockets being at one side of the eccentric axes and their regions of maximum caproviding an opening for fluid flow in the regionof maximum pocket capacity.
  • Apparatus oithe class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation substantially in a common plane, and cooperating with each other in providing a plurality of series of fluid pockets, each series of pockets moving between a region of maximum capacity and a region of minimum capacity, and wall elements cooperating with said rotors in enclosing the pockets and a combustion chamber communicating with each of said series of pockets at both sides of the common plane in the region of minimum pocket capacity, said wall elements being broken away at each end or the rotors in the region oil-maximum pocket capacity.
  • Apparatus or the class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation substantially in a common plane, and cooperating with each other in providing a plurality of series of fluid pockets, each series oi pockets moving between a region of maximum capacity and a region of minimum capacity, and wall elements cooperating with said rotors in enclosing the pockets, and a combustion chamber communicating with each of said series of pockets atboth sides of the common plane in the region of minimum pocket capacity, and means for igniting the charge in said chamber.
  • Apparatus of the class described comprising a plurality of rotors disposed eccentrically one tooth upon each or the inner rotors than the number of intermeshing internal teeth upon the adjoining rotor, each of teeth having a line contact with. a tooth upon an adjoining rotor, and end walls cooperating with said teeth in providing livid pockets and openings communicating with said pockets.
  • Apparatus of the class described comprising a plurality of eccentrically disposed rotors, said rotors cooperating with each other in providing a series of fluid pockets, the pockets moving between a region of maximum capacity and. a, region of minimum capacity, wall elements cooperating with said rotors in enclosing the pockets, a wall element providing a fluid inlet, and a wall element providing for fluid outlet, one of said wall elements having a limited rotational movement in response to its frictional engagement with the rotors, yieldable means opposing the rotational movement of said wall element, and holding means retaining the wall element in engagement with the rotors, but permitting'its slight outward movement in response to rotational movement against the yieldable means, whereby tendency of the friction between the rotors and wall element to increase is automatically compensated.
  • Apparatus of the class described comprising a'rotor, a bearing member in frictional engagement therewith, supporting and holding means for the rotor and bearing member constructed to permit the rotor to rotate freely and the bearing member to rotate slightly, said means including a yieldable element permitting and opposing such a movement of the bearing member, said means also including a part .en'-

Description

July 31-, 1934.
E. A. WEAVER ROTARY ENGINE THE LIKE Filed Aug. 211950- 3 Sheets-Sheet 1 3 9 3 I E. A. WEAVER w fl ROTARY ENGINE OR THE LIKE Filed Aug. 2. 1930 3 Sheets-Sheet 2 July 31, 1934- E. A. WEAVER 1 ROTARY ENGINEOR THE; LIKE Filed Aug. 2. 19:50 s Sheets-sheaf. 3
Patented July 31, I934 STA res
1,968,113 ROTARY ENGINE 0R '1 Eastman A. Weaver,
Winchester, Mass, as-
signorto Comstock & Westcott, inc atom,
Mass, a corporation 0! husetts Application August 2, 1930, Serial No. 472,715
17 Claims.
This invention relates to improved forms of fluid pressure apparatus, such as'compressors, pumps, and pressure fluid motors or engines. Certain aspects of the invention pertain generally to the improvement of fluid pressure apparatus of a type wherein fluid is pocketed and compressed and/or expanded, while a further aspect of the invention pertains to the provision and arrange.- ment of improved pressure fluid apparatus of this general character for use as an internal combustion motor. y
The present invention provides fluid pressure I apparatus having a plurality of rotors which cooperate in aifording fluid pockets movable from a region of maximum capacity to a region of minimum or substantially no capacity. Preferably these pockets may be provided between a plurality of eccentrically disposed toothed rotors,
the teeth of the rotors being arranged so that.
each tooth is constantly in engagement with a portion of the adjoining rotor. Preferably an outer rotor or casing may be provided with internal teeth which intermesh with the teeth of a smaller eccentrically mounted inner rotor, the latter preferably being in the form of a tortuous annular shell, the tortuosities of which form internal as well as-external teeth, and preferably having its internal teeth in engagement with the external teeth of a still smaller rotor. This arrangement permits the employment of several rotors arranged one within the other and each having teeth in mutual engagement with an adjoining rotor or rotors, thereby providing a fluid apparatus of given size with a comparatively large-volumetric capacity, despite the limited size of the fluid pockets formed between the points of contact of the tooth portions of adjoining rotors; furthermore, the rotors thus arranged provide a series of pockets, each pocket moving in a substantially annular circuit between a region of maximum capacity and a region of minimum or substantially nil capacity. .All of the moving parts of the apparatus may have a true rotary motion,
' thus avoiding the objectionable noise, vibration and wear which accompanies the employment of reciprocating parts. Furthermore, the apparatus is'adapted to have a substantially uniform torque whether used as a compressor or pump or as a motor, and the parts of the apparatus may be free from sudden changes in pressure or shoclrs, and due to the relatively uniform and gradual changes in stresses, the apparatus may be relatively light.
for thermal expansion. Thus, for example, the
parts which determine the positioning of the rotational axes of the rotors preferably may be so disposed and mounted that a slight increase in the distance between the axes of the rotors may occur in response to heat expansion. The rotors may be associated with substantially fixed end plates which assist in defining the fluid pockets and provide openings for the ingress and egress of fluid; preferably at least one of these end plates may be associated with means to maintain asubstantially constant frictional engagement between the same and the rotors, despite thermal expansion of the rotors, wear or other changes of dimensions. For this purpose one end plate or bearing part may have a slight rotational movement in response to the frictional drag of the rotors and may have a corresponding but much smaller outward movement so that as the frictional drag between the rotors and bearing part tends to increase the bearing'part or wall may have a slight movement anally away from the rotors, tending to decrease its frictional engagement therewith.
Fluid apparatus of this character may be particularly advantageously employed as an internal combustion motor which, for example, may employ a Diesel or semi-Diesel cycle. Air may be introduced into the fluid pockets at or near their region of substantially maximum capacity, the air being compressed as the pockets pass toward the region of minimum capacity and being emitted into-a stationary combustion chamber which communicates with the pockets at both sides oi the plane of the eccentric axes. In the chamber the compressed air is mixed with combustible material, such as a suitable liquid hydrocarbon mixture, and the burning gases are emitted from this chamber into the expanding pockets, thereby tending to increase the. volume of the latter and converting the gas pressure energy into energy of rotational movement of the rotors. Preferably the end walls may be broken away adjoining the region of maximum pocket capacity, thus permitting cooling of the rotors and the ready movement of the burnt gases out of the pockets and the replacement of the same by fresh air. To aid this desirable result, the apparatus preferably may .be associated with blast inducing me, such as a blower or an' airreciprocating movement results in a substantiallyv constant torque, which may be more umiorm than attainable even from multi-cylinder engines of the reciprocating type. Furthermore, the movement of an airblast over and between the rotors is efiective not only in thoroughly scavenging burnt gases, filling the pockets with fresh sir and giving the elsperetus a high volumetric csoscity, but the air bio. is also effective in cooling the rotors without the necessity for special cooling; means.
In the accompanying drawings:
, Fig. l. is e. side elevotiomel View oi my improved fluid pressure spporotus;
2 is c. section, indicated by line 2-2 of Fig. l, the fuel pump and blower also being shown in this ilsore;
Fig. s is e sectional vies. of the rotors end at coo'giereting driven seer;
Fig. i is so elevetionol of a eorticn of one of the end pistes;
Fig. 5 is s. sectioned detell showing the orrsngemcnt of the mes-es for holding the end plates in proper eiigesement with the rotors;'
Fig. d is e. dios'remmstic view showing the rmer in which the rotor teeth may be laid out.
Referring to the eccompenylns drawings, and first more psrtlculorly to l. and 2, the raw merol l desigriotes e. suitelole support for tire rotors and related psrts, which may include s plsner upper portion 2, that may be secured to any suit able supporting port, and psrellel depending pistes 7 and t which preferably may loe integral with the planar 2. A suitable sxiol member 9, extending; between pistes 7 end s, may carry an inner rotor id which may be substantially in the ml of a. pinion lievlmj external teeth 12.
Am outer rotor or casing met" its cccentricsily disposed in relstiori to the inner rotor it end rosy be provided with lriterriel teeth it. I
Prefereloly, however, in order to izicrees the volumetric capacity oi" the apparatus ll provide one or more intermediate rotors in the former? tortuous sd'lriuler shells, one of which is shown in tlie ecccmperiyiris end lsdesigneted Toy the numeral l5. This shell preferably pro vides internal end external tee-til l6 end 17, which mesh with. the testis. l2 end M, respectively, oi
. the irmer end outer rotors, shown, the teeth t the rotors are designed continually to emsege eocli other throughout their movement. Iii other words, each tooth lies e substantially con tinsel line contact with the adjoining rotor, the teeth holes in deeply or closely meshed e2igsgemeet at the region. of minimum pocket capacity, i. e. in the plene of the sizes oi the rotors. Since the teeth contact in this monitor, it is evi dent the shell 15 mew ice held in position oetween the rotor ill end time casing 25 Without need for any additional support.
Suitable means is provided to support and detlie oi rotation oi the outer casing 25, such mes-sis comprising a. plurality of pairs on? rollers Ell sod Elliv/liicli lisve extensions 21. end 1239 supported by the plates '3 8. As shown, the exiel extensions 21 or the lower roll== ers rosy lie cerried on deeen'ding pests of the plates "l and losing mounted upon bearing blocks 2% which slideloly engage slots 25 in the extensions 23, tire bearing blocks loeirss retained in position log; adjusting screws 2d which. ere thresded iotoplstes 27 secured to tide estem stores 23.
Preierelely the rollers so may be stressed in sgosced oeirs end mes; engage spaced peripheral lflflNiOlid oi the casing or outer rotor 25. Between persilel portions the rotor may cs orevideo" with external seer teeth 29 which mesh with the teeth of e seer it'd mounted upon the shaft 129 which cerries the upper pelioi rollers Lessors the rotors under host and to maintain the rotor teeth in substantially constantly meshed ensese= merit despite hest expansion. For this purpose the sheit 129 is carried in bearing clocks 12d slidololy mounted in slots 127 in the plates 'l and 8, heavy coil springs being disposed in the support 1 to urge the blocks 12% and the slisit 129 downwardly, thereby yieldsloly holding the rotors in closely meshed engagement seed yield ably determining the relative position or spacing of their eccentric axes.
Preferably the rotors may directly engage one ol the depemliris plates of the support 1, such as the plate l, while the plate s may be spaced from the other ends of the rotors, and s. special form oi. end plate 31 having e. rotary mounting upon the shafts may be disposed between the plate t and the rotors. A tension spring 3 3 preferably connects en extension or eer 33 imam the plots fill and s fixed part of the support 1, thereby tending to oppose end restrain the rotational movement oi piste 31 about exiel support 9 in response to the frictions]. drag of the rotors. The outer time of the piste 3i met" be provided with one or more circumierentielly inclined recessed portions or surfaces 32 which incline outwardly in the di rectlcri of rotor movement. A bell 38 mounted.
in e recess 35 in the plots 3 may be engaged by the socket oi. a. retaining out so, the bell time being held against the inclined surface 32, end time tending to hold the plate 39 amidst the ro tors. As the plate 31 moves against the action of the spring 34% due to the frictionsl oi the rotors, the bell 88 is pressed outwardly into erreasement with s deeper portion oi the recess 32, and the pressure of time spring 3% is less; eccord ingly the force with which the piste 31 is held against the rotors is eutometicelly rediii'sed es the piste turns against the sctlon of spring 3% iii resnonse to frictional dr es. Thus the piste lies s slislit outvvsrd movement axially of time rotors to compensate for oriy tendency toward era increases in friction between these ports, said besides Plots 3i irisy engege the rotors with a, substsritiefl, or1-= stout force despite host expensive, varieties, in lubricating conditions or the like. Preferably the rotors eresrremged so that they lieve free erid= Wise movement in relation to the ordeal support ii. thus permitting e. similar maintenance of sectio factory frictional engagement between the rotors and the fixed plate 7. I
While various designs of teeth me}; he ezeizoloved to permit the attainment of the desired result. Fig. it shows, the preferred memes of out the teeth of the verious rotors. As previously stoted, eecli rotor lies one less tooth them the adjoining outer rotor. Nous the rotor it sees have five teeth, the rotor or shell have six teeth, end the rotor or casing 25 have seven teetli. Accordingly in letting; out the teeth pitch circles A, E and C, corresponding to the rotors 35, iii end ill, may be arranged within one another end tangent to each other, the diameters oi these cir= cles being propombioried in accordance with the respective number of teeth of the rotors. Hypo cycloids are their inscribed Within each oi the circles, the limocyclcids within each circle contect= ass fuel pump. as
ing with each other and the circle at nodes or points corresponding in number with the number oi teeth which the corresponding rotor is to possess. Thusthere will be seven points oi contact upon the pitch circle A. It is evident that the inscribed hypocycloidal figures contact with one another at the points of intersection or contact with the pitch circles. Furthermore, these figures, ii rotated about their respective pitch circle I centers at speeds proportional to the diameters of these circles, would continue to contact with each other, thus simulating the continualrcontacting engagement of the rotors. The gear teeth are then designed by rolling circles upon the hypocycloidal figures, a circle oil a given diameter D being rolled about the inner hypo'cycloidal figure C"within the circle C to define the contour of the rotor 10. A circle I) of similar diameter is then rolled about the hypocycloidal figure B to define the internal teeth of the shell 15. A circle of larger diameter, designated E, is then rolled about the same hypocycloidal figure B to define the external teeth of the rotor 15. It is thus evident that the rotor 15 may be made in the form of a tortuous annular member having constant thickness and that the diameters of the circles D and E difier by the desired thickness of the shell. The circle E is then rolled about the outer hypocycloidal figure A to define the internal teeth of the casing 15. Obviously the same method of procedure may be employed when more than one intermediate shell is provided.
The apparatus as thus far described may be adapted for a wide variety of purposes by the provision oi suitable ports in one or both of the end plates. It is evident, for example, that the device may be used as a pump or a compressor, or as a motor driven by pressure fluid, such as steam or compressed air. an especially vantageous arrangement of the apparatus, however, permits its employment as an eiflcient, compact,light, internal combustion engine having easy starting characteristics and uniform torque. To permit these desirable results, a combustion chamber t1, which preferably may be lined with refractory material 42, may be disposed in the end plate '7, this chamber preferably having an open side communicating with the fluid pockets in the region oi their minimum capacity and having a limited extent at the side of the plane of the axes of the rotors where the pockets are contracting in volume and having a greater extent at the opposite side of this plane, the shape of the pocket being shown, for example, in Figs. 1 and 3. Preferably the pocket does not extend inwardly beyond the pitch circle for the shell 15.
The lower parts of the plates 7, 8 and 31 may be broken away, as designated by numeral so, so that the ends of the fluid pockets are open to the atmosphere when maximum capacity. Preferably the out-away portion of the walls extends farther in the direction of pocket contraction than in the direction of pocket expansion, as shown in Fig. 1, although this arrangement may be diminished or reversed to provide a superchanging effect, if desired. In other words, the cut-away portion may be arranged so that a much higher maximum compression of the charge could be attained than would be the case with the arrangement or its edge adjoining the contracting pocket portions in the position shown in Fig. l. A suitable may continuously supply iuel such as a suitable oil through a duct 44 to the combustion chamber. A valve they are in their region of.
us may be associated with duct 44 to regulate the amount of fuel supplied to the motor. A blower 53 may be arranged to supply a blast of air to the open ends of the pockets .at the lower part of. the apparatus. Under these conditions the pockets will be filled with air when they are in their regions ofmaximum capacity and then will contract, compressing the air until the air can pass into the charge chamber 41. The-pressure existing in the charge chamber may be suflicient to ensure ignition oi. the mixture of fuel and air, and accordingly the same may pass out of the larger opening at the right of the axial plane, as viewed in Fig. 3, into the expanding pocket. At opposite sides of the axial plane and at equal distances therefrom the pressure to which the pockets are subjected is thus greater upon the expansion side of the device and produces a net torque moving the rotors and abstracting work from the combustion gases. As the expansion continues the pockets come into communication with the openings provided by the broken-away portions of the end walls and the burnt gases are free to escape. The force of the air blower 50, the propeller or the like, aids in scavenging the pockets of gas, and ensures filling of the same with fresh air, which is again compressed as the pockets contract and pass between the closed wall portions, and the cycle is repeated.
Under many conditions it may be desirable to provide means such as a spark plug 56 to aid in heating the charge in the combustion chamber,
such means being employed continuously or upon starting, as may be necessary. It is evident that no accurate timing means need be provided for such a spark plug but that it may be supplied with high tension current in any suitable manner, for example, by any make and break-systern. Starting of the motor may be readily ef-- which it may be delivered to any suitable point.
It is evident that the yieldable mounting of the shafts 9 and 129 is particularly advantageous when the apparatus is to be employed as a motor due to the high temperatures developing in the device and consequent heat expansion. Furthermore, this arrangement ensures the correct tghtness of engagement of the rotor teeth at the high pressure portion of their cycle whether new or worn, and whether copiously or sparingly lubricated. The yieldable mounting of the end plate 31 is also advantageous to permit the device efllciently to operate under various thermal conditions and have its'high pressure portions remain substantially fluid tight. Furthermore, the cooling of the rotors is ensured by the constant blast 0! cool air supplied to their exposed portions at the low pressure part of the apparatus. The cooled rotors accordingly are effective in receiving heat from the hot end walls and thus especially in cooling these portions of the device, although it is evident that these parts oi the apparatus may advantageously reach a relatively high temperature, thus aiding thethermal emciency of the engine without interiering with its mechanical efliciency.
From the foregoing it is evident that I have provided a new type of fiuid ,pressure apparatus which is characterized by the employment of rotatable parts defining'pockets. which expand and contract in response to the rotating movement of the rotors, thus providing the device with substantially uniform torque and freedom from vibration or tendency to be noisy. A device of this character is. particularly advantageous when employed as an internal combustion engine due to the high volumetric efficiency permitted, the fact'that the fluid receiving portions of the de vice perform useful work for a very large proportion of their circuits, and particularly due to the fact that the torque may be substantially uniform and free from explosive shocks.
It should be understood that the present disclosure is for the purpose of illustration only and that this invention includes all modifications and equivalents which fall within the scope of the appended claims.
I claim:' I
1. Apparatusof the class described comprising a rotatable casing having internal teeth, a rotor eccentrically mounted in the casing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and cas-' ing respectively, said shell being disposed eccentrically between. the rotor and the casing, and side-walls at the end of the casing, said walls cooperating with the rotor and shell in providing one set of fluid pockets and with the casing and shell in providing another set of fluid pockets.
2. Apparatus of the class described comprising a rotatable casing having internal teeth, a rotor eccentrically mounted in the casing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and casing respectively, said shell being disposed eccentrically between the rotor and the casing,
and side walls at the end of the casing, said walls cooperating with the rotor and shell in providing one set of fluid pockets and with the casing and shell in providing another set of fluid pockets, one of said walls being provided with a port communicating with said fluid pockets.
3. Apparatus of the class described comprising a rotatable casinghaving internal teeth, a rotor eccentrically mounted in the casing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and casing respectively, said shell being disposed eccentrically between the rotor and the casing with its central axis disposed in the plane of the axes of rotation of the rotor and easing, the teeth of the rotor meshing with the internal teeth of the shell and the teeth of the casing meshing with the external teeth of the shell in the"region of said plane, and side walls at end of the casing, said walls cooperating with the rotor and shell in providing one set of fluid pockets and with the casing and shell in providing another set of fluid pockets.
4. Apparatus of the class described comprising a rotatable casing having internal teeth, a rotor eccentrically mounted in thecasing and having external teeth, an intermediate annular shell providing internal and external teeth, which are received between the teeth of the rotor and casing respectively, said shell being eccentrically mounted in relation to the rotor and the casing with its central axis disposed in the plane of the axes of rotation of the rotor and easing, the teeth of the rotor closely meshing with the internal teeth of the shell and the teeth of the casing closely meshing with the external teeth of the rotor in the region of said plane, and side walls at end of the casing, said walls cooperating with the rotor and shell in providing one set of fluidpockets and with the casing and shell in providing another set of fluid pockets, a combustion chamber adjoining the region where the teeth mesh. closely, and said chamber communicating with the pockets at each side of said plane.
5. A motor comprising an outer rotatable casing, an inner rotor, and an intermediate annular member, said casing, rotor and annular member each having axes of rotation eccentric in relation to each other and in substantially the same plane, the rotor, annular member, and casing cooperating in providing pockets successively moving through a continuous circuit between a region of minimum volume and a region of maximum volume, a combustion chamber communicating with the pockets in the region of minimum volume on each side of said plane and means for supplying fuel to said chamber, and means to supply fresh air to the pockets in their region of maximum capacity and to permit the movement of gases of combustion therefrom.
6. A motor comprising an outer rotatable casing, an inner rotor, and an intermediate annular member, said casing, rotor, and annular member each having axes of rotation eccentric in relation to each other and in substantially the same plane, the rotor, annular member and casing cooperating in providing pockets successively moving through a continuous circuit from a region of minimum volume to a region of maximum volume, a combustion chamber communicating with the pockets in the region of minimum volume on each side of said plane, and means for supplying fuel to said chamber, end walls cooperating with casing, shell and rotor in providing said pockets, said walls having opposite openings to permit the exhaustion of burnt gases from the pockets and inflow of air thereto in the region of maximum pocket capacity.
7. A motor comprising an outer rotatable casing, an inner rotor, and an intermediate annular member, said casing, rotor and annular member each having axes of rotation eccentric in relation to each other and in substantially the same plane, the rotor annular member and casing cooperating in providing a series of pockets successively moving through a continuous circuit from a region of minimum volume to a region of maximum volume, a combustion chamber communicating with the pockets in the region of minimum volume on each side of said plane, and means for supplying fuel to said chamber, end walls cooperating with casing, shell and rotor in providing said pockets, said walls having opposite openings to permit the exhaust of burnt gases and inflow of air in the region of'maximum pocket capacity, and draft inducing means for purging the pockets of burnt gases and filling them with fresh air.
8. Apparatus of the class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation suband the regions of minimum capacity of each of the series of pockets being at one side of the eccentric axes and their regions of maximum caproviding an opening for fluid flow in the regionof maximum pocket capacity.
9. Apparatus or the class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation substantially in a common plane, and cooperating with each other in providing a plurality of series of fluid pockets, each series of. pockets moving between a region of maximum capacity and a region of minimum capacity, and wall elements cooperating with said rotors in enclosing the pockets, and a combustion chamber communicate ing with each of said series of pockets at both sides of the common plane inthe region of mini= mum pocket capacity.
10. Apparatus oithe class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation substantially in a common plane, and cooperating with each other in providing a plurality of series of fluid pockets, each series of pockets moving between a region of maximum capacity and a region of minimum capacity, and wall elements cooperating with said rotors in enclosing the pockets and a combustion chamber communicating with each of said series of pockets at both sides of the common plane in the region of minimum pocket capacity, said wall elements being broken away at each end or the rotors in the region oil-maximum pocket capacity.
11. Apparatus or the class described comprising a plurality of eccentrically disposed rotors, said rotors having their eccentric axes of rotation substantially in a common plane, and cooperating with each other in providing a plurality of series of fluid pockets, each series oi pockets moving between a region of maximum capacity and a region of minimum capacity, and wall elements cooperating with said rotors in enclosing the pockets, and a combustion chamber communicating with each of said series of pockets atboth sides of the common plane in the region of minimum pocket capacity, and means for igniting the charge in said chamber.
12. Apparatus oi the class described comprising a plurality of eccentrically disposed rotors, said rotors having their axes of rotation substantially in a common plane, the rotors providing mutually intermeshing teeth, and thus cooperating with each other in providing a plurality of series oi fluid pockets each series of pockets moving between a region of maximum capacity and a region of minimum capacity, and wall elements cooper= ating with said rotors in enclosing the pockets, a wall element providing an opening for fluid fiow adjoining the region of minimum pocket ca pacity, and a wall element providing an opening for fluid flow in the region of maximum pocket capacity. 4
13. Apparatus of the class described comprising a plurality of rotors disposed eccentrically one tooth upon each or the inner rotors than the number of intermeshing internal teeth upon the adjoining rotor, each of teeth having a line contact with. a tooth upon an adjoining rotor, and end walls cooperating with said teeth in providing livid pockets and openings communicating with said pockets.
14. Apparatus oi the class described comprising a plurality of rotors disposed ecoentrically one within the other, each rotor having teeth engaging with another rotor, the outer rotor having internal teeth meshing with external teeth upon the adjoining rotor, the latter also having internal teeth engaging with external teethupon the adjoining inner rotor, =there being one less external tooth upon each of the inner rotors than the number of intermeshing internal teeth upon the adjoining rotor, each of teeth having a line contact, with a tooth upon an adjoining rotor, and end walls cooperating with said teeth in providing fluid pockets and providing openings communicating with said pockets, and means yieldably holding the teeth of the rotors in intermeshed'engagement, but permitting limited variation in the spacing of the axes of the rotors.
15. Apparatus of the class described comprising a plurality of eccentrically disposed rotors, said rotors cooperating with each other in providing a series of fluid pockets, the pockets moving between a region of maximum capacity and. a, region of minimum capacity, wall elements cooperating with said rotors in enclosing the pockets, a wall element providing a fluid inlet, and a wall element providing for fluid outlet, one of said wall elements having a limited rotational movement in response to its frictional engagement with the rotors, yieldable means opposing the rotational movement of said wall element, and holding means retaining the wall element in engagement with the rotors, but permitting'its slight outward movement in response to rotational movement against the yieldable means, whereby tendency of the friction between the rotors and wall element to increase is automatically compensated.
16. Apparatus of the class described comprising a'rotor, a bearing member in frictional engagement therewith, supporting and holding means for the rotor and bearing member constructed to permit the rotor to rotate freely and the bearing member to rotate slightly, said means including a yieldable element permitting and opposing such a movement of the bearing member, said means also including a part .en'-
gageable with a part of the bearing member, one of said parts having an inclined surface engaging a bearing surface on the other part to per' within the other, a fixed axial mounting for the inner rotor, supporting means for'the outer rotor including a rotatable element, and yieldable means pressing said element against the outer rotor and toward the inner rotor in the direction of a plane including the axes of the inner and outer rotors, whereby the rotors are yieldably pressed toward each other in the region where the pockets have their minimum volumes.
EASTMAN A. WEAVER.
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Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2482713A (en) * 1944-06-27 1949-09-20 Bergen Engineering And Sales C Rotary internal gear pump
US2822760A (en) * 1958-02-11 Rotary pump
US2956554A (en) * 1957-03-18 1960-10-18 Nsu Werke Ag Method of cooling rotary piston internal combustion engines
US2989951A (en) * 1959-04-29 1961-06-27 Germane Corp Rotary fluid pressure device
US3081753A (en) * 1960-03-10 1963-03-19 Curtiss Wright Corp Rotary combustion engines
US3117561A (en) * 1960-04-26 1964-01-14 Bonavera Victor Rotor type power generating or work performing means
US3156220A (en) * 1960-08-22 1964-11-10 Jr Lloyd E Miller Rotary internal combustion engine
US3280755A (en) * 1964-05-04 1966-10-25 Borg Warner Ring gear type pump
US3291062A (en) * 1966-02-21 1966-12-13 Hermary Maurice Rotary fluid pressure device
US3367275A (en) * 1965-08-18 1968-02-06 Reginald A. Workman Fluid pump or motor
US3387772A (en) * 1965-02-04 1968-06-11 Leybold Heraeus Gmbh & Co Kg Rotary vacuum pump
US3396668A (en) * 1965-11-23 1968-08-13 Danfoss As Rotary devices
US3431863A (en) * 1965-03-05 1969-03-11 Danfoss As Guide means
US3979167A (en) * 1975-01-27 1976-09-07 Grove Leslie H Internal gear set having roller teeth
DE3346519A1 (en) * 1982-12-24 1984-07-05 Mannesmann Rexroth GmbH, 8770 Lohr Positive displacement machine, in particular lobed rotor machine
US4629399A (en) * 1984-10-09 1986-12-16 Robert Bosch Gmbh Aggregate for delivering fuel from a fuel supply tank to an internal combustion engine of a motor vehicle
WO1996001372A1 (en) * 1994-07-02 1996-01-18 T & N Technology Limited Gerotor-type pump
US5720251A (en) * 1993-10-08 1998-02-24 Round; George F. Rotary engine and method of operation
US6195990B1 (en) * 1999-01-13 2001-03-06 Valeo Electrical Systems, Inc. Hydraulic machine comprising dual gerotors
WO2004007963A1 (en) * 2002-07-17 2004-01-22 Elthom Enterprises Limited Volume screw machine of rotary type
WO2005078240A1 (en) * 2004-01-14 2005-08-25 Elthom Enterprises Limited Method of transforming energy in a rotary screw machine of volumetric type
DE102011089528B3 (en) * 2011-12-22 2013-04-11 Continental Automotive Gmbh Pump for pumping air used in motor vehicle, has pump casings and internally toothed external rotor located in pump housing, where external rotor is mounted at external side of radial bearings, and inner rotor is engaged with external rotor
US20180347362A1 (en) * 2017-06-05 2018-12-06 The Texas A&M University System Gerotor apparatus
RU2781726C1 (en) * 2022-03-28 2022-10-17 Павел Сергеевич Гук Rotary piston engine and method of its operation
US20230287884A1 (en) * 2022-03-09 2023-09-14 Mahle International Gmbh Gerotor and pump apparatus having a gerotor device

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2822760A (en) * 1958-02-11 Rotary pump
US2482713A (en) * 1944-06-27 1949-09-20 Bergen Engineering And Sales C Rotary internal gear pump
US2956554A (en) * 1957-03-18 1960-10-18 Nsu Werke Ag Method of cooling rotary piston internal combustion engines
US2989951A (en) * 1959-04-29 1961-06-27 Germane Corp Rotary fluid pressure device
US3081753A (en) * 1960-03-10 1963-03-19 Curtiss Wright Corp Rotary combustion engines
US3117561A (en) * 1960-04-26 1964-01-14 Bonavera Victor Rotor type power generating or work performing means
US3156220A (en) * 1960-08-22 1964-11-10 Jr Lloyd E Miller Rotary internal combustion engine
US3280755A (en) * 1964-05-04 1966-10-25 Borg Warner Ring gear type pump
US3387772A (en) * 1965-02-04 1968-06-11 Leybold Heraeus Gmbh & Co Kg Rotary vacuum pump
US3431863A (en) * 1965-03-05 1969-03-11 Danfoss As Guide means
US3367275A (en) * 1965-08-18 1968-02-06 Reginald A. Workman Fluid pump or motor
US3396668A (en) * 1965-11-23 1968-08-13 Danfoss As Rotary devices
US3291062A (en) * 1966-02-21 1966-12-13 Hermary Maurice Rotary fluid pressure device
US3979167A (en) * 1975-01-27 1976-09-07 Grove Leslie H Internal gear set having roller teeth
DE3346519A1 (en) * 1982-12-24 1984-07-05 Mannesmann Rexroth GmbH, 8770 Lohr Positive displacement machine, in particular lobed rotor machine
US4629399A (en) * 1984-10-09 1986-12-16 Robert Bosch Gmbh Aggregate for delivering fuel from a fuel supply tank to an internal combustion engine of a motor vehicle
US5720251A (en) * 1993-10-08 1998-02-24 Round; George F. Rotary engine and method of operation
WO1996001372A1 (en) * 1994-07-02 1996-01-18 T & N Technology Limited Gerotor-type pump
US6195990B1 (en) * 1999-01-13 2001-03-06 Valeo Electrical Systems, Inc. Hydraulic machine comprising dual gerotors
WO2004007963A1 (en) * 2002-07-17 2004-01-22 Elthom Enterprises Limited Volume screw machine of rotary type
WO2004007967A1 (en) * 2002-07-17 2004-01-22 Elthom Enterprises Limited Volume screw machine of rotary type
WO2005078240A1 (en) * 2004-01-14 2005-08-25 Elthom Enterprises Limited Method of transforming energy in a rotary screw machine of volumetric type
US20070264147A1 (en) * 2004-01-14 2007-11-15 Elthom Enterprises Limited Method of Transforming Energy in a Rotary Screw Machine of Volumetric Type
DE102011089528B3 (en) * 2011-12-22 2013-04-11 Continental Automotive Gmbh Pump for pumping air used in motor vehicle, has pump casings and internally toothed external rotor located in pump housing, where external rotor is mounted at external side of radial bearings, and inner rotor is engaged with external rotor
US20180347362A1 (en) * 2017-06-05 2018-12-06 The Texas A&M University System Gerotor apparatus
US20230287884A1 (en) * 2022-03-09 2023-09-14 Mahle International Gmbh Gerotor and pump apparatus having a gerotor device
US11927188B2 (en) * 2022-03-09 2024-03-12 Mahle International Gmbh Gerotor and pump apparatus having a gerotor device
RU2781726C1 (en) * 2022-03-28 2022-10-17 Павел Сергеевич Гук Rotary piston engine and method of its operation

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