US3538706A - Multicylinder hot gas engine with power control - Google Patents
Multicylinder hot gas engine with power control Download PDFInfo
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- US3538706A US3538706A US749768A US3538706DA US3538706A US 3538706 A US3538706 A US 3538706A US 749768 A US749768 A US 749768A US 3538706D A US3538706D A US 3538706DA US 3538706 A US3538706 A US 3538706A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H23/00—Wobble-plate gearings; Oblique-crank gearings
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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
- F02G1/045—Controlling
-
- 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
- F02G2244/00—Machines having two pistons
- F02G2244/50—Double acting piston machines
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- Combustion & Propulsion (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Description
y H9? R. R. TOEPEL 3,538,706
MULTICYLINDER HOT GAS ENGINE WITH POWER CONTROL Filed Aug. 2, 1968 2 Sheets-Sheet 1 fizz/1611 32 590296! ATTORNEY R. R. TOEPEL Nov. 10, 1970 MULTICYLINDER HOT GAS ENGINE WITH POWER CONTROL 2 Sheets-Sheet 2 Filed Aug. 2, 1968 HORSEPOWER EFFICIENCY 4O 8O 90 I00 VOLUME PHASE ANGLE l uz'chargz' kel United States Patent 3,538,706 MULTICYLINDER HOT GAS ENGINE WITH POWER CONTROL Richard R. Toepel, Warren, Mich., assignor to General Motors Corporation, Detroit, Mich., a corporation of Delaware Filed Aug. 2, 1968, Ser. No. 749,768 Int. Cl. F03g 7/08; F04d 15/00 US. Cl. 6024 7 Claims ABSTRACT OF THE DISCLOSURE FIELD OF THE INVENTION My invention relates to hot gas engines and more particularly to means for controlling the power output in certain multicylinder engines of the hot gas type.
DESCRIPTION OF THE PRIOR ART It is known in the art relating to certain types of hot gas engines to vary the power output by adjusting the phase relationships of the pistons which act upon the working gas so as to carry out a thermodynamic work producing cycle. Such an arrangement is, for example, shown in US. Pat. No. 2,465,139 Van Weenen et al. as applied to a single cylinder engine having a power piston which varies the volume of the working space and a displacer piston which moves the gas between the cold and hot zones of the working space.
It is obvious that such phase changing arrangements could be applied to multi-cylinder engines of the type shown in the aforementioned patent merely by changing the phase relationships of all the similar pistons in the same manner. There are, however, other multicylinder engine constructions, for example, those disclosed in the various figures of U8. Pat. No. 2,480,525 Van Weenen to which such phase changing concepts are not obviously applicable. In these latter engines, there is no single displacer piston, but two pistons acting together serve the dual functions of controlling the volume of the working space and transferring the working gas back and forth between the hot and cold zones or chambers.
Further, in most of these designs, a single piston is made to act upon the working gas in two separate working spaces giving what is known as a double acting piston or a double acting engine arrangement. In these double acting arrangements, each cylinder is interconnected with two others so that it is impossible to adjust the phase relationships of all the working cycles in the same manner. This results from the fact that movement of one piston to bring it more in phase with a second piston with which it acts to define one working space will move the first piston further out of phase with a third piston with which it acts to define a second working space.
SUMMARY OF THE INVENTION The present invention provides arrangements by which the power output of a hot gas engine having one or more double acting piston may be controlled by varying the phase relationships of the engine pistons. While the in- 3,538,706 Patented Nov. 10, 1970 ice vention is broadly applicable to many types of engines in which two pistons acting together control the volume of each working space, an engine arrangement is proposed which is especially suitable for use with the fundamental inventive concepts.
The basis for the present invention was the discovery, proven by theoretical studies, that the horsepower and efiiciency curves for a hot gas engine follow relatively uniform patterns from their maximum to zero as the phase angle between the hot and cold chambers of the Working spaces is adjusted in either direction from one-quarter cycle degrees) out of phase to either an in phase condition or to a one-half cycle degrees) out of phase condition. This was found to be true even though the pressure and volume conditions differ when moving in the two opposite directions and this discovery led to the realization that adjusting the phase of one piston of a multicylinder double acting engine away from the conventional one-quarter cycle out of phase relationship between the pistons of its connecting cylinders would act to reduce the power output in both its connected working spaces in about the same degree.
The present invention, therefore, makes use of this phenomenon by providing drive means which permit adjusting the phase relationships of alternate pistons of the interconnected cylinders of a double acting engine so as to control the power output. As a preferred embodiment, a four-cylinder axial piston arrangement utilizing dual swash plate drive is proposed for advantageous application of the novel concept.
These and other advantages of the invention will be more apparent from the following description of the preferred embodiment taken together with the drawings.
BRIEF DESCRIPTION OF THE DRAWINGS In the drawings:
FIG. 1 is a side elevational view, partially in cross section, of a preferred embodiment of a hot gas engine formed according to the invention;
FIG. 2 is a cross-sectional view of the hot gas engine of FIG. 1 taken generally in the plane indicated by the line 22 of the figure;
FIG. 3 is a diagrammatic view of the hot gas engine of FIGS. 1 and 2 showing the interrelationship of the various components making up the engine working spaces and FIG. 4 is a graph indicating the curves of horsepower and efficiency at various phase angles between the volurnes of the hot and cold chambers of a working space.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring now to the figures of the drawings in detail, numeral 10 generally indicates a four-cylinder axial piston hot gas engine having a drive housing 12 to which are attached four seal retainers 14 secured by collars 16 to four cylinder members 18, 20. 22 and 24 annularly arranged on parallel axes. The cylinders terminate in closed ends 26 and may include liners 28 in which are reciprocably disposed four pistons 30, 32, 34 and 36. The pisto'ns carry suitable seal rings 38 and are connected by rods 40 to follower members 42 and 43 which reciprocate in sleeves 44 provided in the housing 12. Rolling seals 46 are provided between the seal retainers 14 and rods 40 to prevent the escape of working gas from the cylinders into the drive housing.
Within the drive housing are a pair of swash plates 48 and 50 carried for rotation on concentric shaft members 52 and 54 respectively. Swash plate 48 is connected to a first group of two pistons 32 and 36 by sliding engagement with pivotable bearing members 56 which and seated on the sides of slots 58 of the follower members 43 connecting with these pistons. Swash plate 50 connects to a second group of two pistons 30 and 34 in a similar manner through their respective bearing members 56 and follower members 42. Additional elongated slots 60 are provided in follower members 42 and 43 to provide clearance for the rotation of the swash plates 48 and 50 within the follower members to which they are not connected.
Shaft members 52 and 54 extend into a gear box 62 which contains suitable phase changing mechanism for varying the rotative portions of swash plates 48 and 50. By the phase changer 62, shaft members 52, 54 are interconnected with one another and are both connected so as to supply power to an output shaft 64.
The interiors of the engine cylinders 18, 22 and 24 are separated by their respective pistons into hot chambers 66, 68 70 and 72 formed at the ends 26 of the cylinders and cold chambers 74, 76, 78 and 80 formed at the opposite ends thereof. Annularly disposed intermediate the cylinders are four canister-like members 82 each of which includes a suitable cooler 84 and a regenerator 86. A heater 88, which may be a burner or other suitable heating device, is located outboard of the ends 26 of the engine cylinders. A plurality of tubes 90 extend from the ends 26 of the cylinders through heater 88 to the regenerator 86 of the adjacent canister. Short connectors 92 con nect the cooler ends of the canisters with the cold chamber ends of the adjacent cylinders.
Thus, four separate gas containing working spaces A, B, C and D are formed, each made up of the hot and cold chambers of adjacent cylinders connected through certain heater tubes 90, a regenerator 86 and its connecting cooler 84 and one of the short connectors 92. The volume of each working space varies as determined by the positions of the two pistons which define it, one of these pistons varying the volume of the hot chamber and the other varying the volum of the cold chamber. Each double acting piston, in turn, defines both a hot and a cold chamber which form parts of two separate working spaces.
FIG. 4 shows the calculated effects on horsepower and efficiency of changing the volume phase angle of the hot and cold chambers of one working space. That these relationships are not completely obvious is apparent from a consideration of the differing results obtained from changing the phase angle in opposite directions from the nominal 90 degrees.
The normal working cycle includes events of compression, heating, expansion and cooling. The heating and cooling events take place by the transfer of gas from the cold chamber through the cooler, regenerator and heater r to the hot chamber and vice versa. Reducing the phase angle of the volume changes of the hot and cold chambers to zero increases both compression and expansion but substantially eliminates gas transfer between the chambers. Increasing the phase angle to 180 degrees increases gas transfer but eliminates compression and expansion. While both acts reduce power output to zero, the differences in the method of reduction make surprising the similarity in the shape of the two halves of the power curves. Possibly even more surprising is the relatively high efficiency indicated for all but the lower power levels.
In normal full output operation of the engine, the four pistons are reciprocated continuously but with adjacent pistons having a 90 degree or one-quarter cycle phase difference from one another. As shown in FIG. 3, the pistons follow one another in the sequence 36, 34, 32,
with one-quarter cycle between them. This results in the cycle of volume changes of the respective hot chambers leading the volume changes of their connected cold chambers by 90 degrees or one-quarter cycle which gives a positive work outputat a maximum power level for each working space. This work output is transferred by the pistons to their connected swash plates 48, 50 and thence through the phase changer 62 to the output shaft 64.
In order to reduce the engine power output, the phase changer 62 is operated by control means, not shown, so as to rotate either one or both of the swash plates as described through an angle of up to degrees with respect to one another. This changes the phase relationships of the various pistons.
Thus, for example, the position of piston 36 may be retarded one-quarter cycle or 90 degrees which will put this piston in phase with piston 34. At the same time, piston 32 will be moved 90 degrees in a retarding direction so that it is in phase with piston 30 and degrees or one-half cycle out of phase with piston 34. Pistons 36 and 30 will also be 180 degrees or one-half cycle out of phase with one another. By this adjustment, the hot and cold chambers of working spaces B and D change from 90 degree phase angles to phase angles of zero. This reduces the power output of these working spaces as shown in the left hand portion of the curve of FIG. 4 from a maximum to zero. At the same time, the hot and cold chambers of working spaces A and C have their phase angles increased from 90 degrees to 180 degrees, which reduces the power of these working spaces as shown in the right hand side portion of the curve of FIG. 4 from a maximum to zero. It should be obvious that any intermediate adjustment of the phase angle will result in an intermediate power output from the engine with approximately equal power outputs being obtained from each of the working spaces as indicated by the uniform shape of both sides of the horsepower curve of FIG. 4.
While the invention has been described by reference to a preferred embodiment chosen for purposes of illustration, it should be apparent that the concepts involved are equally applicable to other hot gas engines in which double acting cylinder arrangements may be used. For example, the phase changing concepts disclosed herein could equally well be applied to any of the engines shown in the various figures of the previously mentioned US. Pat. No. 2,480,525, the disclosure of which is hereby incorporated herein by reference. Many other modifications of the invention within the spirit and scope of the inventive concepts presented should also be obvious to those skilled in the art.
What is claimed is:
1. A hot gas engine adapted to operate with a gaseous working fluid and comprising a plurality of cylinders,
a plurality of pistons not less than three in said engine cylinders and defining therewith at least two hot chambers and at least two cold chambers, the volume of each of said chambers being determined by the operative position of one of said pistons,
passage means connecting each hot chamber detfined by one of said pistons with a cold chamber defined by another of said pistons to form a plurality of working spaces each having the volume thereof determined by the operative positions of two pistons,
said pistons being classifiable into first and second groups each consisting of one only of the pistons determining the volume of each of said working space, each group defining at least one hot chamber and at least one cold chamber,
first and second drive means connected with the pistons of said first and second groups respectively and opperative to maintain predetermined phase relationships between the pistons of said first group and between the pistons of said second group, said drive means being adapted to maintain a controlled phase relation between said pistons for operation at maximum engine power such that the volume change of each hot chamber leads the volume change of the cold chamber of its respective working space by one-quarter of a cycle,
said second drive means being adjustable with respect to said first drive means to reduce engine power by unidirectionally changing the phase relations of the pistons of said second group with respect to the pistons of said first group by an amount up to onequarter of a cycle, said one-quarter cycle change resulting in the volume changes of the hot chambers of certain working spaces being in phase with the volume changes of the respective cold chambers thereof while the volume changes of the hot chambers of the remaining working spaces are one-half cycle out of phase with the volume changes of the respective cold chambers thereof, each such condition resulting in no power output from the pistons of the various working spaces.
2. The combination of claim 1 wherein said engine has four cylinders each having one double acting piston therein, two of said pistons being connected to said first drive means and two of said pistons being connected to said second drive means.
3. The combination of claim 2 wherein said engine cylinders are annularly arranged on parallel axes and said drive means comprise first and second swash plates.
4. A hot gas engine adapted to operate with a gaseous working fluid and comprising four cylinders,
a double acting piston in each cylinder and defining therewith a hot chamber at one end and a cold chamber at the other, the volume of each of said chambers being determined by the operative position of said piston,
passage means connecting the hot chamber of each cylinder with the cold chamber of another to form a plurality of working spaces each having the volume thereof determined by the operative positions of the two pistons,
said pistons being classifiable into first and second groups each consisting of two pistons which together determine, in part, the volume of all of said working spaces,
first and second drive means connected with the pistons of said first and second groups respectively and operative to maintain an out of phase relationship between the pistons of said first group and between the pistons of said second group, said drive means being adapted to maintain a one-quarter cycle phase angle between the pistons of said first and second groups for operation at maximum engine power such that the volume change of each hot chamber leads the volume change of the cold chamber of its respective working space by one-quarter of a cycle,
said second drive means being adjustable with respect to said first drive means to reduce engine power by unidirectionally changing the phase relations of the pistons of said second group with respect to the pistons of said first group by an amount up to onequarter of a cycle, said change resulting in a decrease in the phase angle between the hot and cold chambers of two of said working spaces and a comparable increase in the phase angle between the hot and cold chambers of the other two of said working spaces.
5. The combination of claim 4 wherein said engine cylinders are annularly arranged on parallel axes and said working spaces are formed by connection together of adjacent cylinders, said first and second groups consisting of oppositely disposed pistons.
6. The combination of claim 5 wherein said drive means comprise first and second swash plates rotatable on a common axis, and relatively rotatable to vary the phase relationships of the tfirst and second groups of pistons.
7. The method of controlling the power output of a multicylinder hot gas engine having a plurality of pistons and a plurality of working spaces each including a hot chamber defined in part by one of said pistons in a cold chamber defined in part by another of said pistons, said method comprising the steps of controlling the phase relations of said pistons during reciprocation thereof to obtain a leading phase angle of one-quarter cycle for the volume variations of the hot chamber of each working space over the cold chamber thereof for maximum engine power and reducing engine power by changing the phase relations of the pistons to decrease the leading phase angles of the hot chambers over the cold chambers of certain of the engine working spaces up to a maximum decrease of one-quarter cycle to an in-phase condition, While concurrently increasing the leading phase angles of the hot chambers over the cold chambers of the remaining engine working spaces in a comparable amount up to a maximum increase of onequarter cycle to a one-half cycle out-of-phase condition.
References Cited UNITED STATES PATENTS 970,640 9/ 1910 McClintock 91175 XR 2,445,281 7/1948 Rystrom 91l75 XR 2,468,293 4/1949 Du Pre 24 XR 2,480,525 8/1949 Van Weenen 60--24 2,583,311 1/ 1952 Van Heeckerson 6024 2,611,235 9/1952 Van Weenen 6024 2,664,699 1/1954 Kohler 6024 2,691,350 10/1954 Greer 103-37 3,117,414 1/1964 Daniels et al. 6024 3,191,542 6/1965 Hughes l0337 XR 3,315,465 4/1967 Wallis 6024 FOREIGN PATENTS 336,810 10/1930 Great Britain. 812,83 6 5/ 1959 Great Britain.
MARK M. NEWMAN, Primary Examiner I. PAYNE, Assistant Examiner U.S. Cl. X.R.
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Application Number | Priority Date | Filing Date | Title |
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US74976868A | 1968-08-02 | 1968-08-02 |
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US3538706A true US3538706A (en) | 1970-11-10 |
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US749768A Expired - Lifetime US3538706A (en) | 1968-08-02 | 1968-08-02 | Multicylinder hot gas engine with power control |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3746475A (en) * | 1971-02-03 | 1973-07-17 | Gen Motors Corp | Double-acting swashplate compressor |
US4019322A (en) * | 1975-01-22 | 1977-04-26 | U.S. Philips Corporation | Hot-gas reciprocating engine |
US4090430A (en) * | 1974-10-09 | 1978-05-23 | The Japan Steel Works | Swash plate type compressor |
EP0005566A1 (en) * | 1978-05-10 | 1979-11-28 | Koninklijke Philips Electronics N.V. | Balanced variable displacement drive |
US4387566A (en) * | 1981-03-11 | 1983-06-14 | Mechanical Technology Incorporated | Independently variable phase and stroke control for a double acting Stirling engine |
US4395880A (en) * | 1981-03-11 | 1983-08-02 | Mechanical Technology Incorporated | Double acting stirling engine phase control |
US4532855A (en) * | 1984-04-04 | 1985-08-06 | Stirling Thermal Motors, Inc. | Two-part drive shaft for thermal engine |
US20100281861A1 (en) * | 2009-05-07 | 2010-11-11 | Emigh S Grant | Linear roller bearing assembly and sub-assembly and reciprocating machinery incorporating the same |
US8881520B2 (en) | 2009-05-07 | 2014-11-11 | S. Grant Emigh | Linear roller bearing assembly and sub-assembly and reciprocating machinery incorporating the same |
Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US970640A (en) * | 1909-08-04 | 1910-09-20 | Samuel Russell Bogue | Power-transmitting mechanism. |
GB336810A (en) * | 1929-10-29 | 1930-10-23 | G & J Weir Ltd | Improvements in pumps |
US2445281A (en) * | 1945-10-04 | 1948-07-13 | Charles H Rystrom | Hydraulic pump |
US2468293A (en) * | 1946-02-04 | 1949-04-26 | Hartford Nat Bank & Trust Co | Refrigerating apparatus actuated by a hot-gas engine |
US2480525A (en) * | 1943-01-23 | 1949-08-30 | Hartford Nat Bank & Trust Co | Multicylinder hot-gas engine |
US2583311A (en) * | 1943-05-25 | 1952-01-22 | Hartford Nat Bank & Trust Co | Hot-gas motor with means for controling the heat supply therefor |
US2611235A (en) * | 1948-10-12 | 1952-09-23 | Hartford Nat Bank & Trust Co | Multicylinder hot gas reciprocating piston engine of the doubleacting type |
US2664699A (en) * | 1950-11-24 | 1954-01-05 | Hartford Nat Bank & Trust Co | Multicylinder double-acting hotgas reciprocating engine |
US2691350A (en) * | 1951-09-10 | 1954-10-12 | Greer Hydraulics Inc | Hydraulic equipment |
GB812836A (en) * | 1957-01-08 | 1959-05-06 | Candy Filter Company Ltd | Improvements in or relating to positive displacement pumps |
US3117414A (en) * | 1961-07-14 | 1964-01-14 | Wisconsin Alumni Res Found | Thermodynamic reciprocating apparatus |
US3191542A (en) * | 1962-06-04 | 1965-06-29 | Kenneth D Hughes | Metering pump |
US3315465A (en) * | 1965-07-09 | 1967-04-25 | Gen Motors Corp | Phase relation control |
-
1968
- 1968-08-02 US US749768A patent/US3538706A/en not_active Expired - Lifetime
Patent Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US970640A (en) * | 1909-08-04 | 1910-09-20 | Samuel Russell Bogue | Power-transmitting mechanism. |
GB336810A (en) * | 1929-10-29 | 1930-10-23 | G & J Weir Ltd | Improvements in pumps |
US2480525A (en) * | 1943-01-23 | 1949-08-30 | Hartford Nat Bank & Trust Co | Multicylinder hot-gas engine |
US2583311A (en) * | 1943-05-25 | 1952-01-22 | Hartford Nat Bank & Trust Co | Hot-gas motor with means for controling the heat supply therefor |
US2445281A (en) * | 1945-10-04 | 1948-07-13 | Charles H Rystrom | Hydraulic pump |
US2468293A (en) * | 1946-02-04 | 1949-04-26 | Hartford Nat Bank & Trust Co | Refrigerating apparatus actuated by a hot-gas engine |
US2611235A (en) * | 1948-10-12 | 1952-09-23 | Hartford Nat Bank & Trust Co | Multicylinder hot gas reciprocating piston engine of the doubleacting type |
US2664699A (en) * | 1950-11-24 | 1954-01-05 | Hartford Nat Bank & Trust Co | Multicylinder double-acting hotgas reciprocating engine |
US2691350A (en) * | 1951-09-10 | 1954-10-12 | Greer Hydraulics Inc | Hydraulic equipment |
GB812836A (en) * | 1957-01-08 | 1959-05-06 | Candy Filter Company Ltd | Improvements in or relating to positive displacement pumps |
US3117414A (en) * | 1961-07-14 | 1964-01-14 | Wisconsin Alumni Res Found | Thermodynamic reciprocating apparatus |
US3191542A (en) * | 1962-06-04 | 1965-06-29 | Kenneth D Hughes | Metering pump |
US3315465A (en) * | 1965-07-09 | 1967-04-25 | Gen Motors Corp | Phase relation control |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3746475A (en) * | 1971-02-03 | 1973-07-17 | Gen Motors Corp | Double-acting swashplate compressor |
US4090430A (en) * | 1974-10-09 | 1978-05-23 | The Japan Steel Works | Swash plate type compressor |
US4019322A (en) * | 1975-01-22 | 1977-04-26 | U.S. Philips Corporation | Hot-gas reciprocating engine |
EP0005566A1 (en) * | 1978-05-10 | 1979-11-28 | Koninklijke Philips Electronics N.V. | Balanced variable displacement drive |
US4235116A (en) * | 1978-05-10 | 1980-11-25 | U.S. Philips Corporation | Balanced variable wobble plate drive |
US4387566A (en) * | 1981-03-11 | 1983-06-14 | Mechanical Technology Incorporated | Independently variable phase and stroke control for a double acting Stirling engine |
US4395880A (en) * | 1981-03-11 | 1983-08-02 | Mechanical Technology Incorporated | Double acting stirling engine phase control |
US4532855A (en) * | 1984-04-04 | 1985-08-06 | Stirling Thermal Motors, Inc. | Two-part drive shaft for thermal engine |
US20100281861A1 (en) * | 2009-05-07 | 2010-11-11 | Emigh S Grant | Linear roller bearing assembly and sub-assembly and reciprocating machinery incorporating the same |
US8220258B2 (en) * | 2009-05-07 | 2012-07-17 | Emigh S Grant | Linear roller bearing assembly and sub-assembly and reciprocating machinery incorporating the same |
US8881520B2 (en) | 2009-05-07 | 2014-11-11 | S. Grant Emigh | Linear roller bearing assembly and sub-assembly and reciprocating machinery incorporating the same |
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