US3166911A - Hot-gas reciprocating apparatus - Google Patents

Hot-gas reciprocating apparatus Download PDF

Info

Publication number
US3166911A
US3166911A US349113A US34911364A US3166911A US 3166911 A US3166911 A US 3166911A US 349113 A US349113 A US 349113A US 34911364 A US34911364 A US 34911364A US 3166911 A US3166911 A US 3166911A
Authority
US
United States
Prior art keywords
regenerator
cooler
elements
housing
cylinder
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
US349113A
Inventor
Meijer Roelf Jan
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.)
US Philips Corp
North American Philips Co Inc
Original Assignee
US Philips Corp
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 US Philips Corp filed Critical US Philips Corp
Application granted granted Critical
Publication of US3166911A publication Critical patent/US3166911A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/14Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the cycle used, e.g. Stirling cycle
    • 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
    • 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
    • F02G1/053Component parts or details
    • F02G1/057Regenerators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/002Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant
    • F25B9/004Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant the refrigerant being air
    • 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
    • F02G2243/00Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes
    • F02G2243/02Stirling type engines having closed regenerative thermodynamic cycles with flow controlled by volume changes having pistons and displacers in the same cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2309/00Gas cycle refrigeration machines
    • F25B2309/003Gas cycle refrigeration machines characterised by construction or composition of the regenerator

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

Jan. 26, 1965 R. J. MEIJER HOT-GAS RECIPROCATING APPARATUS 3 Sheets-Sheet 1 Filed March 5, 1964 FIG.2
INVENTOR.
ROELF J. MEUER AGENT Jan. 26, 1965 R. .1. MEIJER HOT-GAS RECIPROCATING APPARATUS 3 Sheets-Sheet 2 Filed March 3,
INVENTOR.
ROELF MAEUER AGENT Jan. 26, 1965 R. AMELIER Q 3,166,911
HOT-GAS REdiPRocATING APPARATUS Filed March :5, 1964 5 Sheets-Sheet s INVENTOR ROELF J. MEUER .5; Awe. K. AGENT United States Patent 3,166,911 HOT-GASRECIPROCATING APPARATUS Roelf-Jan Meiier, Emmasingel, Eindhoven, Netherlands, assignor to North American Philips Company, Inc,
New York, N.Y., a corporation or Delaware Filed Mar.'3,1'964, SerkNo. 349,113 Claims'priority, application Netherlands, Mar. 11, 1963,
290,975 6 Glaims. (Cl. 62- '6) Theinvention relates'to a hot-gas reciprocating apparatus comprising one ortmore cylinder spaces in each of which a displaceriand a piston are adapted to reciprocate with arelative phase difference so as to vary the volumes of an expansion space anda compression'space. In the operation of the machine, 'these spaces have difierent mean temperatures andcommunicate with each other by meansof a'first heat exchanger (heater), a regenerator and asecond heat exchanger (cooler). Theregenerator is subdivided into a:plurality of regeneratorelements arranged parallel toeach other, while the second heat exchanger is subdivided into a number of-parallel-arranged elements equal to thatof the regenerator.
For the purpose ofthis-specification, the term hot-gas reciprocating apparatus is defined to include not only a hot-gas engine, but also a cold gas refrigerator and a heat pump operating according to the'reversed hot-gas engine principle.
In known apparatus of the said kind, the regenerator is. arranged with an 'initialntension'in arthin-walled housing which in turn is accommodated in a'further housing.
This construction suiiersfrom the limitation that, if no further precautions are taken, upon the passage of the Working medium through the regenerator alternately in one and in the other direction, the regenerator tends to -follow the movement of the medium and strikes the end faces of the housing.
housing. This-impairs the appearance and simplicity of the constructionywhile this spring increasesthe dead space. This adversely affects theefiiciency of the apparatus.
The invention has'for its object to obviate the above disadvantages'and the apparatus is characterized in that each element of the second heat' exchanger is accommodated together with a regener'atorfelement in one housing, the axial inner dimension of the-housing in which an element of the second heat exchanger, which'heat exchanger isconstructed rigidly in the axial direction, and the associated elastically compressible regenerator ele 'me'nt are accommodated, beingsmallerthan the sum of the axial dimensions of the two elements when disassembled.
In the construction in accordance with the invention, the regenerator is consequently compressed more strongly while being mountedtin the housing, while after mounting the regenerator filler material itself ensures that the regenerator does not move in the housing.
'Anadvantageous embodiment of the hot-gas reciprocating apparatus in accordance with'the invention is characterized in that 'each' regenerator element consists'of a filler material accommodated in a further housing which, at its 'sidefacing the associated element of the second heat' exchanger, embraces a rim of the said-element in a flexibility to these pipes. :stresses occurring-in the structure are absorbed by the ice apparatuscomprises more than-one cylinder space, is
characterized in that the-housings associated with a given cylinderspace, in eachof which a regenerator element and an element of the associated secondheat exchanger are accommodated, arearranged in two groups around the-cylinder space concerned, one group being situated on onerside and'the other; group on the other side of the plane, passing through the longitudinalaxes of the cylinder'space concerned. This embodiment is of particular importance. when the-hot-gas reciprocating apparatus is to be accommodated in a small space. The distance between the longitudinal-axesof two adjacent cylinder spaces can then be smaller than in the case of a regular arrangement .of the cooler-regenerator units around the cylinder spaces.
An even more compact structure of the hot-gas reciprocatingapparatus in'accordance-with the invention is characterized infthat, while the housings of the two groups are situated pairwise diametrically opposite each other, the two housings ofeachgroup farthest remote from each other are alt-different distances from the plane passing through the longitudinal axes-of the cylinder spaces.
these pipesabeing connected'to an "annular duct to which further. pipes are, connected through which this duct communicates with the expansion space, is characterizedin that each of the pipes of the first heat exchanger'contains an expansion member which imparts a certain axial As a result the temperature expansion member.
According to. a further favourable embodiment, the expansion member is constituted by a'portion of the pipe which extends transversely to the longitudinal axis of the relevant cylinder space.
In order that the invention may be readily carried into efr'ect;embodimentsxthereof, will now-be 'described;by way ofexample, With'reierence tothe accompanying drawings, in which:
FIGS. 1 and 2 are-an axial section and-a cross-section taken'on. the line 'IL-II, respectively, of a-hot-gas reciprocating apparatus in accordance with'the invention only that part of the apparatus being shown which consists of the-cylinder and the piston and displacer adapted toreciprocateither'ein, and of the first heat exchanger and the second-heat exchanger'with the interposed regenerator,
FlGS.3a andBb show a cooler-regenerator unit inthe demollnted state and in the mounted state, respectively.
FIG. 4Sl'1OWS diagrammatically a possible arrangement of the cooler-regeneratoraunits' around :the cylinder spaces.
FIGSJS and6 are an elevation and-aycross-section taken on the 'line'-VIVI respectively, of a further embodiment of a' hot gas reciprocating apparatus.
In the embodiment'shown .in FIGS. 1 and 2, reference numeral 1 denotes the cylinder wall the upper side of which terminates in an end face 2. Pipe portions 3 of the :heater open-into the conicalpart of'the head'face.
The upper ends of these pipe portions 3 are connected to anannular duct 4. This annular duct 4 constitutes the connection" between the pipe portions 3 and heater pipe 3 portions 5. For the sake of clarity, only two sets of the heater pipes 3 and 5 are shown; in actual fact together they enclose a cylindrical space 6 which serves as a combustion chamber. A burner is placed in or above this space.
With the aid of means (not shown}, a displacer 8 and piston 9 are adapted to reciprocate in the cylinder 1. The heater pipes 5 are also connected to the coolerregenerator units 10. The structure of these units will be described more fully with reference to FIGS. 3a and 31:. Through a connection pipe ll, the cooler-regenerator units 1% communicate with the cylinder 1. As is apparent from the figures, the heater pipes S are provided with a portion 12 extending transversely to the longitudinal axis of the cylinder. This heater pipe portion 12 imparts a certain flexibility to the heater pipes 5, so that, when the distance between the upper ends of the cooler units 16 and the annular duct 4- is increased as a result of temperature differences, no fracture will occur in the apparatus.
FIG. 3a shows a cooler-regenerator unit comprising a cooler portion 13 and a regenerator portion 14. The cooler portion '13 comprises a plurality of pipes 15 the lower ends of which are secured in a flange plate lid and the upper ends in a plate 17 the upper side of which is provided with a flanged rim 18. The regenerator portion 14 comprises a thin-walled housing l? which is closed at its upper end by a plate 2%) provided with a plurality of holes 21. The housing 19 further comprises filler material 22. This filler material may consist, for example, of a plurality of stacked gauzes. The filler material 22 is bounded on its lower side by a sieve plate 23. The lower end of the housing 1% is crimped over a the flanged rim 1?. The filler material 22 and the sieve plate 23 are accommodated in the housing 19 so that a slight movement in the axial direction with respect to the housing is possible. The housing is can slide over the flanged rim 18. In the demounted state shown in FIG. 3a, the assembly of cooler and regenerator has an axial length A PEG. 3b shows the cooler-regenerator unit in the mounted state. The cooler-regenerator unit is accommodated in a housing 4% to the upper end of which one or more heater pipes 5 are connected. The plate of the regenerator -14 engages the shoulder 24 of the housing 4%. The housing 40 is closed at its lower end by a closing member 25 which in the embodiment shown in FIG. 3b is soldered in the housing. The closing member 25 may also be connected to the housing 4G by a screwed connection or in a difierent manner. The cooler- regenerator unit 13, 14 is enclosed between the shoulder 24 and the upper edge of the closing member 25, the distance between the shoulder 24 and the upper edge of the closing member 25 having a dimension A which is smaller than the length A of the cooler-regenerator unit in the demounted state. As a result of this smaller dimension A the filler material 22 is slightly compressed, while the housing 19 has slid over the rim 1%, so that, as is apparent from figure, there is a certain amount of clearance between the crimped edge of the housing 19 and the lower surface of the rim 18. An inlet 26 and an outlet 27 for the cooling liquid also communicate with the housing 4! Consequently, the cooling liquid flows around the pipes 15, while O-shaped rings 28 ensure satisfactory sealing. The closing member 25 has a recess 30 through which the pipes 15 communicate with the connection pipe 11 which connects the coolerregenerator .unit to the space in the cylinder 1.
'The compression of the filling mass 22 can be increased or decreased at will by interposing one or more rings between the upper edge of the closing member 25 and the plate 16 of the cooler 13. It should be appreciated that these rings may also be provided between the shoulder 24. and the plate 25? of the regenerator 14. FIG. 4 shows diagrammatically an embodiment of a hot-gas reciprocating apparatus in which the cooler, re generator units i are arranged in two groups of three, one group on either side of the plane passing throughthe longitudinal axes of the cylinder spaces. The figure clearly shows that the distance B between the longitudinal axes of the two cylinders is smaller ban in case the units 3.3 are arranged arbitrarily around the cylinders, as shown in H63. 1 and 2. A further decrease of this distance is obtained when the units it? are arranged around the cylinders in the manner shown in F185. 5 and 6. In these figures, two cylinders 3i and 32 are shown. Two groups of regenerator-cooler units are arranged around the cylinder 31. The regenerator-cooier units 33, 342-, 35 are located on one side of the plane passing through the longitudinal axes of the cylinders 31 and 32, whilst the other group of re enerator- cooler units 36, 37, 38 co-operating with cylinder 3!; are located on the other side of that plane. it is apparent from the drawing that the regenerator-ccoler units of each group most remote from each other are located at different distances from the plane passing through the longitudinal axes of the cylinders. The units 33 and 33 located diametrically opposite each other are closer to the plane passing through the longitudinal axes of the cylinders than the units 35 and 36 likewise located diametrically opposite each other. The same holds for the units connected with the cylinder 32. in this manner, an extraordinarily compact, s tort structure of a hot-gas reciprocating apparatus is obtained.
Finally, it is again clearly apparent from FIG. 5 that the heater pipes 5 for part of their lengths extend transversely to the longitudinal axis of the cylinder with which they co-operate. From this figure also appears the advantage that the length of the transversely extending portions of the heater pipes is greater according as the heater pipe has a larger dimension between the point at which it communicates the annular duct 4 and its connecting point to the coolcr-regenerator unit.
What is claimed is:
l. A hot-gas reciprocating apparatus comprising at least one cylinder having a compression space and an expansion space, a displacer and a piston adapted to reciprocate in said cylinder with a relative phase difference and to vary the Volumes of said compression and expansion spaces, said spaces being at different mean temperatures during operation of said apparatus, means connecting said spaces and including a heater, a cooler a regenerator, said regenerator being subdivided into a plurality of substantially parallel-arranged regenerator elements, resiliently compressible in the axial direction, said cooler also being subdivided into a plurality of substantially parallel-arranged axially rigid elements equal in number to the number of said regenerator elements, a main housing, each element of said cooler being accorn modated together with a regenerator element in said housing, the axial inner dimension of the housing containing said rigid cooler elements and compressible regenerator elements being smaller than the sum of the axial dimensions of any of said cooler elements and corresponding regenerator elements in their demounted state.
2. A hot gas reciprocating apparatus as claimed in claim 1 wherein each regenerator element is constituted of a filler material and said cooler element is provided with a rim, a second housing enclosing said regenerator element, said second housing on its side facing the associated cooler element embraces said rim on the cooler element in a manner such that said second housing located in said main housing and cooler element are movable with respect to each other under the influence of axial forces thereon.
3. A hot gas reciprocating apparatus as claimed in claim 1 wherein regenerator elements and associated cooler elements are arranged in two groups around said Cylinder space, one group being located on one side 5 and the other group on the other side of the plane passing through the longitudinal axis of said cylinder space.
4. A hot gas reciprocating apparatus as claimed in claim 3 wherein the housings of said two groups are located pairwise diametrically opposite to each other while the housin s of each group most remote from each other are located at different distances from the plane passing through the longitudinal axes of said cylinder spaces.
5. A hot gas reciprocating apparatus comprising at least one cylinder having a compression space and an expansion space, a displacer and a piston adapted to reciprocate in said cylinder with a relative phase difference and to vary the volumes of said compression and expansion spaces, said spaces being at diiferent mean temperatures during operation of said apparatus, means connecting said spaces and including a heater, a cooler and a regenerator, said regenerator being subdivided into a plurality of substantially parailel-arranged regenerate: elements, resiliently compressible in the axial direction, said cooler also being subdivided into a plurality of substantially parallel-arranged axially rigid elements equal in number to the number of said regenerator elements,
a main housing, each element of said cooler being accommodated together with a regenerator element in said housing, the axial inner dimension of the housing containing said rigid cooler elements and compressible regenerator elements being smaller than the sum of the axial dimensions of any of said cooler eiernenta and corresponding regenerator elements in their dernounted state, an annular duct, a plurality of pipes being part or" said heater, one end of each of said pipes being in communication with said housing, the other end of each of said pipes being in communication with said annular duct, said annular duct being provided with further ducts for communication with said expansion space, and each of said pipes or" said heater including an expansion member.
6. A hot gas reciprocating apparatus as claimed in claim 5 wherein said expansion member is constituted by a portion of the pipe extending transversely to the longitudinai axis of said cylinder space.
References Cited in the file of this patent UNITED STATES PATENTS 2,963,871 Meijer Dec. 13, 1969

Claims (1)

1. A HOT-GAS RECIPROCATING APPARATUS COMPRISING AT LEAST ONE CYLINDER HAVING A COMPRESSION SPACE AND AN EXPANSION SPACE, A DISPLACER AND A PISTON ADAPTED TO RECIPROCATE IN SAID CYLINDER WITH RELATIVE PHASE DIFFERENCE AND TO VARY THE VOLUMES OF SAID COMPRESSION AND EXPANSION SPACES, SAID SPACES BEING AT DIFFERENT MEANS TEMPERATURES DURING OPERATION OF SAID APPARATUS, MEANS CONNECTING SAID SPACES AND INCLUDING A HEATER, A COOLER AND A REGENERATOR, SAID REGENERATOR BEING SUBDIVIDED INTO A PLURALITY OF SUBSTANTIALLY PARALLEL-ARRANGED REGENERATOR ELEMENTS RESILIENTLY COMPRESSIBLE IN THE AXIAL DIRECTION, SAID COOLER ALSO BEING SUBDIVIDED INTO A PLURALITY OF SUBSTANTIALLY PARALLEL-ARRANGED AXIALLY RIGID ELEMENTS EQUAL IN NUMBER TO THE NUMBER OF SAID REGENERATOR ELEMENTS, A MAIN HOUSING, EACH ELEMENT OF SAID COOLER BEING ACCOMMODATED TOGETHER WITH A REGENERATOR ELEMENT IN SAID HOUSING, THE AXIAL INNER DIMENSION OF THE HOUSING CONTAINING SAID RIGID COOLER ELEMENTS AND COMPRESSIBLE REGENERATOR ELEMENTS BEING SMALLER THAN THE SUM OF THE AXIAL DIMESIONS OF ANY OF SAID COOLER ELEMENTS AND CORRESPONDING REGENERATOR ELEMENTS IN THEIR DEMOUNTED STATE.
US349113A 1963-03-11 1964-03-03 Hot-gas reciprocating apparatus Expired - Lifetime US3166911A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL290075 1963-03-11

Publications (1)

Publication Number Publication Date
US3166911A true US3166911A (en) 1965-01-26

Family

ID=19754508

Family Applications (1)

Application Number Title Priority Date Filing Date
US349113A Expired - Lifetime US3166911A (en) 1963-03-11 1964-03-03 Hot-gas reciprocating apparatus

Country Status (5)

Country Link
US (1) US3166911A (en)
BE (1) BE644930A (en)
DE (1) DE1265494B (en)
GB (1) GB1053052A (en)
NL (1) NL290075A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3310954A (en) * 1964-09-11 1967-03-28 Philips Corp Arrangement for converting mechanical energy into caloric energy or conversely
DE2238960A1 (en) * 1971-08-28 1973-03-08 Philips Nv HOT GAS ENGINE
US3817036A (en) * 1971-08-27 1974-06-18 United Stirling Ab & Co Arcuate shaped heat transfer pipes
US4298057A (en) * 1979-04-06 1981-11-03 Kommanditbolaget United Stirling Ab & Co Tubular heat-exchanger
EP0625683A1 (en) * 1993-05-16 1994-11-23 Daido Hoxan Inc. Pulse tube regrigerator
US20140182311A1 (en) * 2012-12-28 2014-07-03 Hyundai Motor Company Rectification unit for stirling refrigerator

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2963871A (en) * 1958-02-28 1960-12-13 Philips Corp Thermo-dynamic reciprocating apparatus

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1879563A (en) * 1930-03-27 1932-09-27 Gas Res Co Heat engine
DE1082772B (en) * 1957-02-05 1960-06-02 Daimler Benz Ag Cylinder head with cooling fins

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2963871A (en) * 1958-02-28 1960-12-13 Philips Corp Thermo-dynamic reciprocating apparatus

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3310954A (en) * 1964-09-11 1967-03-28 Philips Corp Arrangement for converting mechanical energy into caloric energy or conversely
US3817036A (en) * 1971-08-27 1974-06-18 United Stirling Ab & Co Arcuate shaped heat transfer pipes
DE2238960A1 (en) * 1971-08-28 1973-03-08 Philips Nv HOT GAS ENGINE
US4298057A (en) * 1979-04-06 1981-11-03 Kommanditbolaget United Stirling Ab & Co Tubular heat-exchanger
EP0625683A1 (en) * 1993-05-16 1994-11-23 Daido Hoxan Inc. Pulse tube regrigerator
US5481878A (en) * 1993-05-16 1996-01-09 Daido Hoxan Inc. Pulse tube refrigerator
US20140182311A1 (en) * 2012-12-28 2014-07-03 Hyundai Motor Company Rectification unit for stirling refrigerator
CN103913021A (en) * 2012-12-28 2014-07-09 现代自动车株式会社 Rectification unit for stirling refrigerator
JP2014129995A (en) * 2012-12-28 2014-07-10 Hyundai Motor Company Co Ltd Rectification unit for stirling refrigerator

Also Published As

Publication number Publication date
NL290075A (en)
BE644930A (en) 1964-09-09
DE1265494B (en) 1968-04-04
GB1053052A (en)

Similar Documents

Publication Publication Date Title
US2486081A (en) Multicylinder refrigerating machine
US4183214A (en) Spring and resonant system for free-piston Stirling engines
US4404802A (en) Center-porting and bearing system for free-piston stirling engines
US2480525A (en) Multicylinder hot-gas engine
US3166911A (en) Hot-gas reciprocating apparatus
GB1108097A (en) Heat energised refrigerator
GB1391787A (en) Oscillating or reciprocating device
US4498298A (en) Stirling cycle piston engine
US4069671A (en) Stirling engine combustion assembly
US3157024A (en) Regenerative thermal device
US2963871A (en) Thermo-dynamic reciprocating apparatus
US3310954A (en) Arrangement for converting mechanical energy into caloric energy or conversely
US3074229A (en) Hot-gas reciprocating machine and system composed of a plurality of these machines
US3355882A (en) Leakage prevention arrangment for hot-gas reciprocating apparatus
US2784570A (en) Hot-gas reciprocating engine for refrigerating
US2828601A (en) Hot-gas reciprocating engine
US2596051A (en) Hot-gas piston apparatus having cylinder means and axially arranged piston bodies, heat exchangers, and regenerator therein
US2616250A (en) Cylinder head for hot-gas reciprocating engines
US10352272B2 (en) Dome for a thermodynamic apparatus
US3845626A (en) Hot gas stirling cycle engine with in-line cylinders
US2990681A (en) High compression externally fired laminal displacer engine
US4010621A (en) Stirling cycle heat pump
US3863452A (en) Hot-gas engine heater
US2643507A (en) Hot-gas reciprocating engine in which a plurality of closed thermodynamic cycles are performed simultaneously and which includes a compressor means
US2857220A (en) Hot-gas reciprocating engine