US2475770A - Revolver-type reciprocating piston engine - Google Patents

Revolver-type reciprocating piston engine Download PDF

Info

Publication number
US2475770A
US2475770A US662384A US66238446A US2475770A US 2475770 A US2475770 A US 2475770A US 662384 A US662384 A US 662384A US 66238446 A US66238446 A US 66238446A US 2475770 A US2475770 A US 2475770A
Authority
US
United States
Prior art keywords
shaft
cylinders
pistons
disc
engine
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US662384A
Inventor
Wijsman Johannes
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hartford National Bank and Trust Co
Original Assignee
Hartford National Bank and Trust Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hartford National Bank and Trust Co filed Critical Hartford National Bank and Trust Co
Application granted granted Critical
Publication of US2475770A publication Critical patent/US2475770A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02GHOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
    • F02G1/00Hot gas positive-displacement engine plants
    • F02G1/04Hot gas positive-displacement engine plants of closed-cycle type
    • F02G1/043Hot 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
    • F02G1/044Hot 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 having at least two working members, e.g. pistons, delivering power output

Definitions

  • This invention relates 'to a piston engine of the type in which the reciprocating movement of v the pistons is converted into a rotating movement by means of 'one or more sinusoidall arched tracks on a disc mounted normally to the shaft,
  • the cylinders are mounted in pairs in line with each other-between two discs fast on the shaft at some distance and the relative angular'positlon of these discs and also the variation of the pressure in the cyliners are adjusted in such manner that complete or else partial balancing of the axial pressure and/or acceleration forces is obtained.
  • the cylinders of each pair are caused to be in open communication and the pistons in said cylinders are given equal but opposite movements.
  • the pairs of cylinders are diametrically arranged by twos, for example by mounting an even number of pairs of cylinders uniformly around the shaft, and if also an even number of sinusoids is chosen on each disc, it may be ensured that at any one moment, in addition to the effective torsional stress, the shaft will only be subjected to longitudinal stresses which are moreover compensated in the said shaft.
  • the engine is thus enabled to run perfectly free from vibration and the bearings have no other pressure to absorb than the weight of the shaft and of the parts fixed thereto. It will appear hereinafter that even the said weight may still be neutralised, if desired.
  • this arrangement provides a compact design, saving in material and weight; and the use of one common distribution and ignition mechanism.
  • the construction according to the invention permits of the effective load forces being absorbed entirely or substantially entirely by the pistons so that the use of heavy collar blocks and the friction losses occurring therein, may be obviated, sinceit is possible to choose the mean piston force to be greater to any desired extent in one direction thanthat in the other direction, either by admitting a higher gauge pressure in the cylinders of one rim than in those of the other rim, or by giving a greater cross section to the first-mentioned cylinders than to the others.
  • This arrangement may also be used to advantage with an engine comprising a vertical shaft since the weight of the moving parts are compensated.
  • the resulting axial pressure depends on the mean gauge pressure on the pistons, hence automatic compensation of the axial load pressure (or load traction) may be obtained b causing the mean gauge pressure in the cylinders'to be regulated by the axial pressure.
  • An example of an engine having continuous gauge pressure is a hot-gas engine.
  • the use of the invention with such an engine offers particular advantages, apart from the general advantages mentioned before.
  • the reversal of movement with such an engine is particularly simple since with one sense of rotation the pistons of one of the two cylinder rims lead by a given phase angle relatively to the corresponding pistons of the other rim, and with the other sense of rotation, lag to the same extent.
  • the disc leading (in both directions of rotation) is preferably mounted on the shaft so as to be capable of rotating between two stationary stops, the other disc being in this case rigidly secured.
  • the angle through which one of the discs must be rotated depends not only on the desired phase difference between the pistons but also on the number of sinusoids on each disc. If this number is, for example 4, during each complete piston stroke the shaft makes one quarter of a revolution, and if the pistons of one rim have to lead by /4 cycle relatively to those of the other rim, reversal of the movement will require the adjustable disc to turn through an angle of 1/4.
  • the lead and hence also the angle of rotation is chosen to be slightly smaller.
  • Fig. 1 is a longitudinal sectional view of a hotgas engine in accordance with the invention.
  • Fig. 2 shows a diagram of the cylinders, pistons tracks of same in the developed condition.
  • Figure 2a shows a diagram of a modification of the arrangement shown in Figure 2.
  • the opposed cylinder sections are shown of different diameters, only two complete cylinders being shown for illustrative purposes.
  • Fig. 3 is an elevation of the disc whose position can be changed for the purpose of reversal of movement.
  • the hot-gas engine part of which is shown in longitudinal section in Fig. 1 comprises two rims of six cylinders I which are pair-wise in line with each other. Within each of these cylinders a piston 2 is adapted to move and its free end is provided with a roller 3. These rollers engage a sinusoidally arched track 4 which is carried by a disc 5.
  • One of these discs in the case shown the left hand one, is fast on the motor shaft.
  • the right hand disc 5 is so journalled that its boss 'I rotates through a given angle about a sleeve 8 rigidly secured to the shaft 6 and provided with two stops on which a projecting lug of the boss I is caused to bear in the two extreme positions of the disc. This is shown in Fig.
  • An energising coil II surrounding the shaft brings about a magnetic flux in the closed iron circuit formed by the shaft 6, the two discs 5 with their tracks 4, the rollers 3, the pistons 2 and the cylinders I.
  • the energisation flux is adjusted in such manner that under all conditions the rollers 3 continue to engage the tracks 4. If there is never a sub-atmospheric pressure in the cylinders I a low energization will therefore suffice.
  • the current required may be supplied on starting by the starting battery or by a small generator (not shown) to be assembled in known manner with the'engine. Use may also be made of a line voltage to energize the coil.
  • rollers 3 may be constructed in the form of bevel gears.
  • regenerator I 2 Between each pair of cylinders I in line with each other there is an aggregate comprising a regenerator I 2, a heater I3 and a cooler I4.
  • the regenerator must preferably be mad from porous material of good heat conductivity and of high heat capacity, which with a maximum surface offers a minimum resistance to the medium flowing through.
  • the heater I3 and the cooler I4 are shown in the form of metal drums having, in the axial direction, a large number of fine tubes I5 which are The interior of these drums communicates by inand outlet ports IS with the supply and discharge means (not shown) of a heating and cooling medium respectively.
  • the cooling medium may be, for example, air or water.
  • Fig. 2 is shown six pairs of cylinders with their pistons and rollers in the developed state, the rollers engaging th tracks, it being assumed that the pistons of one rim lead by exactly relatively to those of the other rim and in addition that each disc contains two complete sinusoids so that the shaft 6 makes one revolution only on every two complete piston strokes.
  • This ratio number may, of course, be greatly increased if desired, particularly when the cylinders are mounted in a wide rim around the shaft. This may be done, for example, in cases in which the speed of the shaft should be comparatively low such,-for example, as is the case of screw shafts of ships, driving shafts of locomotives, motorcars, and so forth.
  • the ratio 2:1 will generally be sufficient, there being in this case, if
  • the arrangement of a large number of cylinders in a wide rim around the shaft has still further advantages.
  • the slope. of the tracks 4 decreases in a radial sense so that the detrimental radial pressure towards the outside on the rollers 3 becomes little (and may be assisted also by making the rollers 3 as small as possible).
  • much annular space is available between the shaft 6 and the insides of the cylinders I so that the above-mentioned heating and/or cooling means can be housed in this space resulting in a construction which'is exceedingly compact.
  • the value of the resulting axial force is proportional to the mean pressure in the cylinders and this pressure may be regulated as desired.
  • the axial displacements which the shaft will perform may be used for so innuencing one or more of the said factors that equilibrium is restored.
  • a light collar block may suflice which must be strong enough for maximum conditions such as for example failure of any automatic control devices of the engine.
  • valves, the sparking plugs etc. can be arranged about the shaft in a rim so that they can be operated by one common set of cams by means of short and light connecting members with the avoidance of the need for separate cam shafts or the like.
  • a hot-gas engine comprising a shaft member, a plurality of cylinder means positioned about said shaft member and being arranged substantially parallel therewith, said cylinder means each having two sections, each said section containing a reciprocable piston slidably arranged therein, said pistons each having a roller means coupled thereto, a plurality of assembly means each comprising a heater, a cooler, and a regenerator interposed between said heater and said cooler, on" of said assembly means interposed between said two sections of each of said cylinder interposed between said-two sections of each of l means, and a pair of discs each having a sinusoidal arched track, one of said discs being fixed to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at one end of said cylinder means, the other of said discs being movably secured to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at the other end of said cylinder means and being further arranged
  • a hot-gas engine as claimed in claim 1 wherein all the cylinder sections arranged toward one end of said shaft member have a cylinder and piston diameter greater than the cylinder and piston diameter of all the cylinder sections arranged toward the opposite end of said piston member.
  • a hot-gas engine comprising a shaft member, a plurality of cylinder means positioned about said shaft member and being arranged substantially parallel therewith, said cylinder means each having two sections, each said section containing a reciprocable piston slidably arranged therein, said pistons each having a roller means coupled thereto, a plurality of assembly means each comprising a heater, a cooler, and a regenerator interposed between said heater and said cooler, one of said assembly means interposed between said two sections of each of said cylinder means, a pair of discs each' having a sinusoidal arched track, one of said discs being fixed to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at one end of said cylinder means, the other of said discs being movably secured to said shaft memher and being arranged to engage operatively the sinusoidal arched track of said disc with'said piston roller means at the other end of said cylinder means and being further arranged so that said disc can be rotated with respect to
  • a hot-gas engine comprising a shaft member, a plurality of cylinder means positioned about said shaft member and being arranged substantially parallel therewith, said cylinder means each having two sections, each said section containing a reciprocable piston slidably arranged therein, said pistons each having a roller means coupled thereto, said roller means having bevel gear type contact surfaces, a plurality of assembly means each comprising a heater, a cooler, and a regenerator interposed between said heater and said cooler, one of said assembly means said cylinder means, and a pair of discs having sinusoidal arched tracks in the form of bevel gear surfaces, one of.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

J y 1949. 7 J. WIJSMAN I I 2,475,770 REVOLVER-TYPE RECIPROCIVXTING PISTON ENGINE Filed April 15; 1946 llzg. 1. 2 15 12 J zmza JOHANNES. WIJSMAN INVENTOR.
AGENT Patented July 12, 1949 Johannes Wijsman, Eindhoven, Netherlands, as-
signor, by mesne assignments, to Hartford National Bank and Trust Company, Hartford,
Conn., as trustee Application April 15, 1946, Serial No. 662,384 In the Netherlands May 8, 1941 Section 1, Public Law 690, August 8, 1946 Patent expires May 8, 1961 4 Claims. 1
This invention relates 'to a piston engine of the type in which the reciprocating movement of v the pistons is converted into a rotating movement by means of 'one or more sinusoidall arched tracks on a disc mounted normally to the shaft,
the ends of the pistons rolling or sliding on these According to the invention, the cylinders are mounted in pairs in line with each other-between two discs fast on the shaft at some distance and the relative angular'positlon of these discs and also the variation of the pressure in the cyliners are adjusted in such manner that complete or else partial balancing of the axial pressure and/or acceleration forces is obtained.
Preferably, the cylinders of each pair are caused to be in open communication and the pistons in said cylinders are given equal but opposite movements.
If-the pairs of cylinders are diametrically arranged by twos, for example by mounting an even number of pairs of cylinders uniformly around the shaft, and if also an even number of sinusoids is chosen on each disc, it may be ensured that at any one moment, in addition to the effective torsional stress, the shaft will only be subjected to longitudinal stresses which are moreover compensated in the said shaft. The engine is thus enabled to run perfectly free from vibration and the bearings have no other pressure to absorb than the weight of the shaft and of the parts fixed thereto. It will appear hereinafter that even the said weight may still be neutralised, if desired.
Beside the advantage of quiet running, this arrangement provides a compact design, saving in material and weight; and the use of one common distribution and ignition mechanism.
In those cases in which longtiudinal stresses occur in the shaft, for example with air-craft or ships, the construction according to the invention permits of the effective load forces being absorbed entirely or substantially entirely by the pistons so that the use of heavy collar blocks and the friction losses occurring therein, may be obviated, sinceit is possible to choose the mean piston force to be greater to any desired extent in one direction thanthat in the other direction, either by admitting a higher gauge pressure in the cylinders of one rim than in those of the other rim, or by giving a greater cross section to the first-mentioned cylinders than to the others.
This arrangement may also be used to advantage with an engine comprising a vertical shaft since the weight of the moving parts are compensated. With a given difference in'diameter of the cylinders the resulting axial pressure depends on the mean gauge pressure on the pistons, hence automatic compensation of the axial load pressure (or load traction) may be obtained b causing the mean gauge pressure in the cylinders'to be regulated by the axial pressure.
In the engine according to the invention, care will have to be taken that the members, for ex-- amplerollers, forced by the pistons against the sinusoidal tracks at any one moment engage the said tracks at least with a slight force in order that beating may be avoided. In engines having a steady gauge pressure behind the piston this is ensured automatically, whereas in engines in which there is periodically no gauge pressure but even sub-atmopheric pressure, the above condition must be satisfied in some suitable manner unless the sub-atmospheric pressure periods coincide with the periods in which the pistons are subjected to an acceleration of sufficient value directed from the track.
Since this cannpt always be assured continuous engagement between the pistons and the tracks may be ensured electromagnetically in a simple manner by arranging an energizing coil between the discs to surround the shaft, the magnetic circuit being short-circuited across the two discs. the pistons and the cylinders. In this case, the shaft must of course be journalled with a nonmagnetic material so that a magnetic short-circuit across the frame as avoided.
An example of an engine having continuous gauge pressure is a hot-gas engine. The use of the invention with such an engine offers particular advantages, apart from the general advantages mentioned before.
For, example, the reversal of movement with such an engine is particularly simple since with one sense of rotation the pistons of one of the two cylinder rims lead by a given phase angle relatively to the corresponding pistons of the other rim, and with the other sense of rotation, lag to the same extent.
and sinusoidal essary to change the position of one disc relatively to the other through double the angle of lead or lag in order to reverse the direction of movement of the engine. The disc leading (in both directions of rotation) is preferably mounted on the shaft so as to be capable of rotating between two stationary stops, the other disc being in this case rigidly secured. The angle through which one of the discs must be rotated depends not only on the desired phase difference between the pistons but also on the number of sinusoids on each disc. If this number is, for example 4, during each complete piston stroke the shaft makes one quarter of a revolution, and if the pistons of one rim have to lead by /4 cycle relatively to those of the other rim, reversal of the movement will require the adjustable disc to turn through an angle of 1/4. Generally, the lead and hence also the angle of rotation is chosen to be slightly smaller.
In order that the invention may be clearly understood and readily carried into effect, it will now be described more fully with reference to the accompanying drawing, in which a hot-air engine is illustrated.
i open on both sides.
Fig. 1 is a longitudinal sectional view of a hotgas engine in accordance with the invention.
Fig. 2 shows a diagram of the cylinders, pistons tracks of same in the developed condition.
Figure 2a shows a diagram of a modification of the arrangement shown in Figure 2. In Figure 2a the opposed cylinder sections are shown of different diameters, only two complete cylinders being shown for illustrative purposes.
Fig. 3 is an elevation of the disc whose position can be changed for the purpose of reversal of movement.
The hot-gas engine part of which is shown in longitudinal section in Fig. 1 comprises two rims of six cylinders I which are pair-wise in line with each other. Within each of these cylinders a piston 2 is adapted to move and its free end is provided with a roller 3. These rollers engage a sinusoidally arched track 4 which is carried by a disc 5. One of these discs, in the case shown the left hand one, is fast on the motor shaft. The right hand disc 5 is so journalled that its boss 'I rotates through a given angle about a sleeve 8 rigidly secured to the shaft 6 and provided with two stops on which a projecting lug of the boss I is caused to bear in the two extreme positions of the disc. This is shown in Fig. 3 in which the projecting lug is designated 9 and the two stops are designated I II. For the sake of clearness the disc is shown in Figure 3 in its central position from which it can be moved by rotation to the left 'or to the right through an angle a equal to the angle of lead into the position ahead or back.
An energising coil II surrounding the shaft brings about a magnetic flux in the closed iron circuit formed by the shaft 6, the two discs 5 with their tracks 4, the rollers 3, the pistons 2 and the cylinders I. The energisation flux is adjusted in such manner that under all conditions the rollers 3 continue to engage the tracks 4. If there is never a sub-atmospheric pressure in the cylinders I a low energization will therefore suffice. The current required may be supplied on starting by the starting battery or by a small generator (not shown) to be assembled in known manner with the'engine. Use may also be made of a line voltage to energize the coil.
In order to avoid sliding friction the rollers 3 may be constructed in the form of bevel gears.
This has the disadvantage that apart from the tangentially directed reaction force, which of course is unavoidable, the rollers 3 also exert a pressure on the pistons, and hence on the cylinder wall, which is radially directed outwards. If desired, this pressure may be absorbed by special runways, as otherwise is the case with the tangential pressure referred to. It is essential that the pistons 2 have no lateral strain since, the cylinders would be worn out-of-round.
Between each pair of cylinders I in line with each other there is an aggregate comprising a regenerator I 2, a heater I3 and a cooler I4. The regenerator must preferably be mad from porous material of good heat conductivity and of high heat capacity, which with a maximum surface offers a minimum resistance to the medium flowing through.
The heater I3 and the cooler I4 are shown in the form of metal drums having, in the axial direction, a large number of fine tubes I5 which are The interior of these drums communicates by inand outlet ports IS with the supply and discharge means (not shown) of a heating and cooling medium respectively. The cooling medium may be, for example, air or water.
In Fig. 2 is shown six pairs of cylinders with their pistons and rollers in the developed state, the rollers engaging th tracks, it being assumed that the pistons of one rim lead by exactly relatively to those of the other rim and in addition that each disc contains two complete sinusoids so that the shaft 6 makes one revolution only on every two complete piston strokes. This ratio number may, of course, be greatly increased if desired, particularly when the cylinders are mounted in a wide rim around the shaft. This may be done, for example, in cases in which the speed of the shaft should be comparatively low such,-for example, as is the case of screw shafts of ships, driving shafts of locomotives, motorcars, and so forth. For high-speed shafts such, for example, as shafts of air-screws the ratio 2:1 will generally be sufficient, there being in this case, if
a four stroke cycle internal combustion engine is concerned, the supplementary advantage that the motor shaft itself can be used directly for driving the valveand ignition mechanism.
In addition to the advantage already mentioned of the possibility of a great reduction in speed the arrangement of a large number of cylinders in a wide rim around the shaft has still further advantages. First of all, the slope. of the tracks 4 decreases in a radial sense so that the detrimental radial pressure towards the outside on the rollers 3 becomes little (and may be assisted also by making the rollers 3 as small as possible). Secondly, at least in many cases, much annular space is available between the shaft 6 and the insides of the cylinders I so that the above-mentioned heating and/or cooling means can be housed in this space resulting in a construction which'is exceedingly compact.
Obviously, it is not necessary that the same section should be given to all cylinders, as shown. Wherever this method is adopted the forces acting axially on the discs 5 will be at any one moment equal but oppositely directed and thus neutralise each other in the shaft 6. If, however, in contradistinction to this a resulting axial force such, for example, as with a screw shaft is desired either the hot or the cold" cylinders may have a greater cross-sectional area than the other, according to circumstances. Such modification is tion of each cylinder is of smaller cross-section at 22' than is the other. A smaller roller 3' for the piston in section 22' is shown riding in track 4. In such a case the value of the resulting axial force is proportional to the mean pressure in the cylinders and this pressure may be regulated as desired. Hence, the axial displacements which the shaft will perform, may be used for so innuencing one or more of the said factors that equilibrium is restored. Thus a light collar block may suflice which must be strong enough for maximum conditions such as for example failure of any automatic control devices of the engine.
It will be observed that in the engine shown and described the phase difference of about 90 between the pistons of each pair is responsible for the compensation of the axial acceleration forces being incomplete, at least within each pair of cylinders. Due to this, vibrations may still occur at high speeds. This may be obviated by the cylinders in line with each other not being made in open communication with each other pairwise, but by having one of the cylinder rims and theassociated disc being turned relatively to the other to such extent that in the oppositely arranged cylinders the pistons are given opposite sense of movement. In this case, however, the construction of the engine becomes more complicated since it is necessary for regenerator to be housed in the inclined connecting pieces between the thermally associated cylinders. In addition, in this construction there is no longer within each pair of cylinders absolute compensation of the axial piston pressure on the discs. It will therefore depend on conditions as to which of the two systems is to be used.
In other engines, for example steam engines and internal combustion engines in which with each pair of pistons the phase difierence may be exactly 180, this difficulty is obviously not encountered and quiet running of such engines is obtained.
The use of the invention in steam engines and internal combustion engines avoids the need for more than one distribution and, as the case may be, for more than one ignition mechanism for each pair of cylinders, which are driven from an adequate set of cams on the middle of the shaft. In such a case, regulation of the degree of filling and of the sense of rotation may be effected by regulation of the angular position of the said cams on the shaft. In an internal combustion engine according to the invention, the valves, the sparking plugs etc., can be arranged about the shaft in a rim so that they can be operated by one common set of cams by means of short and light connecting members with the avoidance of the need for separate cam shafts or the like.
What I claim is:
l. A hot-gas engine comprising a shaft member, a plurality of cylinder means positioned about said shaft member and being arranged substantially parallel therewith, said cylinder means each having two sections, each said section containing a reciprocable piston slidably arranged therein, said pistons each having a roller means coupled thereto, a plurality of assembly means each comprising a heater, a cooler, and a regenerator interposed between said heater and said cooler, on" of said assembly means interposed between said two sections of each of said cylinder interposed between said-two sections of each of l means, and a pair of discs each having a sinusoidal arched track, one of said discs being fixed to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at one end of said cylinder means, the other of said discs being movably secured to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at the other end of said cylinder means and being further arranged so that said disc can be rotated with respect to said shaft member to either of two limiting positions.
2. A hot-gas engine as claimed in claim 1 wherein all the cylinder sections arranged toward one end of said shaft member have a cylinder and piston diameter greater than the cylinder and piston diameter of all the cylinder sections arranged toward the opposite end of said piston member.
3. A hot-gas engine comprisinga shaft member, a plurality of cylinder means positioned about said shaft member and being arranged substantially parallel therewith, said cylinder means each having two sections, each said section containing a reciprocable piston slidably arranged therein, said pistons each having a roller means coupled thereto, a plurality of assembly means each comprising a heater, a cooler, and a regenerator interposed between said heater and said cooler, one of said assembly means interposed between said two sections of each of said cylinder means, a pair of discs each' having a sinusoidal arched track, one of said discs being fixed to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at one end of said cylinder means, the other of said discs being movably secured to said shaft memher and being arranged to engage operatively the sinusoidal arched track of said disc with'said piston roller means at the other end of said cylinder means and being further arranged so that said disc can be rotated with respect to said shaft member to either of two limiting positions, and an electromagnetic coil surrounding said piston to establish a magnetic field maintaining engagement between said roller means and said sinusoidal arched track portions of said discs.
4. A hot-gas engine comprising a shaft member, a plurality of cylinder means positioned about said shaft member and being arranged substantially parallel therewith, said cylinder means each having two sections, each said section containing a reciprocable piston slidably arranged therein, said pistons each having a roller means coupled thereto, said roller means having bevel gear type contact surfaces, a plurality of assembly means each comprising a heater, a cooler, and a regenerator interposed between said heater and said cooler, one of said assembly means said cylinder means, and a pair of discs having sinusoidal arched tracks in the form of bevel gear surfaces, one of. saiddiscs being fixed to said shaft member and being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at one end of said cylinder means, the other of said discs being arranged to engage operatively the sinusoidal arched track of said disc with said piston roller means at the other end of said cylinder means and being further arranged so that said 7 8 disc can be rotated with respect to said shaft ITED memberto either of two limiting positions. UN STATES PATENTS .JOHANNES WIJSMAN. Number Name Date 1,669,976 De Leeuw May 15, 1928 REFERENCES CITED 5 2,095,255 Holmes Oct. 12, 1937 The following references are of record in the file of this patent:
US662384A 1941-05-08 1946-04-15 Revolver-type reciprocating piston engine Expired - Lifetime US2475770A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL2475770X 1941-05-08

Publications (1)

Publication Number Publication Date
US2475770A true US2475770A (en) 1949-07-12

Family

ID=19874330

Family Applications (1)

Application Number Title Priority Date Filing Date
US662384A Expired - Lifetime US2475770A (en) 1941-05-08 1946-04-15 Revolver-type reciprocating piston engine

Country Status (1)

Country Link
US (1) US2475770A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2616248A (en) * 1949-01-27 1952-11-04 Hartford Nat Bank & Trust Co Hot-gas reciprocating engine
US3508393A (en) * 1968-09-17 1970-04-28 Donald A Kelly Low friction stirling engines and chemical heating means
US5390496A (en) * 1994-03-04 1995-02-21 El Affaqui; Thami Stirling engine with annular cam
US5442913A (en) * 1992-12-29 1995-08-22 Goldstar Co., Ltd. Stirling cycle system driving device
US5533335A (en) * 1993-11-04 1996-07-09 Goldstar Co., Ltd. Cam driving apparatus for a stirling cycle module
US6701709B2 (en) 2001-08-18 2004-03-09 Tamin Enterprises Cylindrical cam stirling engine drive

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1669976A (en) * 1926-12-23 1928-05-15 Leeuw Adolph L De Pump
US2095255A (en) * 1934-11-30 1937-10-12 Sulivan Machinery Company Expansible chamber motor

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1669976A (en) * 1926-12-23 1928-05-15 Leeuw Adolph L De Pump
US2095255A (en) * 1934-11-30 1937-10-12 Sulivan Machinery Company Expansible chamber motor

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2616248A (en) * 1949-01-27 1952-11-04 Hartford Nat Bank & Trust Co Hot-gas reciprocating engine
US3508393A (en) * 1968-09-17 1970-04-28 Donald A Kelly Low friction stirling engines and chemical heating means
US5442913A (en) * 1992-12-29 1995-08-22 Goldstar Co., Ltd. Stirling cycle system driving device
US5533335A (en) * 1993-11-04 1996-07-09 Goldstar Co., Ltd. Cam driving apparatus for a stirling cycle module
US5390496A (en) * 1994-03-04 1995-02-21 El Affaqui; Thami Stirling engine with annular cam
US6701709B2 (en) 2001-08-18 2004-03-09 Tamin Enterprises Cylindrical cam stirling engine drive

Similar Documents

Publication Publication Date Title
US2313407A (en) Power transmission
US4077269A (en) Variable displacement and/or variable compression ratio piston engine
US3574424A (en) Axially loaded bearing
US4270395A (en) Motion translating mechanism
US2263561A (en) Variable compression ratio barreltype engine
US2475770A (en) Revolver-type reciprocating piston engine
US4173151A (en) Motion translating mechanism
US3385051A (en) Stirling cycle engine with two wave cam means, two piston banks and driveshaft
US5813229A (en) Pressure relief system for stirling engine
US1853563A (en) Internal combustion engine
US2141945A (en) Power transmission
US3538706A (en) Multicylinder hot gas engine with power control
US4274367A (en) Reciprocating piston beam engine
US1810017A (en) Variable stroke cam-engine
US1948526A (en) Parallel steam engine
US2353814A (en) Torque indicator
US1978762A (en) Engine
US1184651A (en) Gas-engine.
US2387467A (en) Internal-combustion engine
US2255963A (en) Hydraulic transmission
US1292597A (en) Rotary valve.
US2655014A (en) Flexible coupling with thrust link
US3521614A (en) Reciprocating machines
US1716020A (en) Motor
US2404615A (en) Brake for hydraulic motors