GB1064733A - Improvements in and relating to thermo-dynamic reciprocating machines - Google Patents

Improvements in and relating to thermo-dynamic reciprocating machines

Info

Publication number
GB1064733A
GB1064733A GB46223/63A GB4622363A GB1064733A GB 1064733 A GB1064733 A GB 1064733A GB 46223/63 A GB46223/63 A GB 46223/63A GB 4622363 A GB4622363 A GB 4622363A GB 1064733 A GB1064733 A GB 1064733A
Authority
GB
United Kingdom
Prior art keywords
pistons
pump
spaces
space
piston
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
Application number
GB46223/63A
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.)
Koninklijke Philips NV
Original Assignee
Philips Gloeilampenfabrieken NV
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 Philips Gloeilampenfabrieken NV filed Critical Philips Gloeilampenfabrieken NV
Publication of GB1064733A publication Critical patent/GB1064733A/en
Expired legal-status Critical Current

Links

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
    • 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
    • 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
    • F02G2244/00Machines having two pistons
    • 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
    • F02G2244/00Machines having two pistons
    • F02G2244/50Double acting piston machines
    • 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
    • F02G2270/00Constructional features
    • F02G2270/85Crankshafts

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)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Compressor (AREA)

Abstract

1,064,733. Refrigerating. PHILIPS' GLOEILAMPENFABRIEKEN N.V. Nov. 22, 1963 [Nov. 26, 1962], No. 46223/63. Heading F4H. [Also in Division F1] In a thermo-dynamic reciprocating machine, e.g. a hot-gas engine or a cold-gas refrigerator, comprising at least two pairs of units which each include a compression piston, a cooler, a regenerator, a freezer or heater and an expansion piston, the pistons are reciprocated by fluid pressure transmitted thereto from at least two pump units. A cold-gas refrigerating machine is described. As shown, two pump units I and II are mounted in V-formation on a common crankcase 1, each pump unit comprising pistons 8 and 13 reciprocating in separate closed cylinders. Two pairs of cooling units are provided, of which one pair A1, A2 is shown, and each cooling unit comprises a compression piston 26, a cooler 24, a regenerator 23, a freezer 22 and an expansion piston 21. The spaces 31 of units A1 and A2 on the sides of pistons 26 remote from the working spaces are connected by ducts 32 and 33 respectively to the spaces on opposite sides of piston 13 of pump unit I while the corresponding spaces 30 adjacent pistons 21 are connected by respective ducts 34 and 35 to the spaces on opposite sides of the piston 8 of pump unit II. Each of the pistons 21 and 26 is connected by a shaft 49 to a valve member 50 having longitudinal bores 52 which is arranged to reciprocate in a cylinder 51 having fluid inlets connected to pipes 54 and 55 and fluid outlets connected to pipes 53 and 56. The pistons 8, 13, 21 and 26 of the machine are positioned ready for starting by moving a valve member 57 to a position in which the discharge of an oil pump 63 is connected via line 73, ports 71 and 69 to lines 55 and via line 73, ports 72 and 68 to a line 18 which communicates with chambers 16 on the ends of the cylinders containing the pistons 13 of pump units I and II. Thus, oil under pressure is delivered via bores 52 to the spaces 30 and 31 of the units to urge the pistons 21 and 26 inwardly such inward movement being terminated when the valve element 50 uncovers the fluid outlets connected to pipes 56 which communicate via ports 70 and 75 and line 76 with an oil reservoir 66 to which the inlet 65 of pump 63 is connected. The oil also acts to force pistons 8 and 13 of the pump units downwardly; the pistons 8, 13, 21 and 26 are shown in their starting positions in Fig. 4. To start the machine valve member 57 is moved to close ports 68, 69, 70, 71, 72 and 75 and a motor (not shown) is energized to drive a crank-shaft 19 to drive pump pistons 8 and 13 which in turn act on the oil contained in spaces 30 and 31, ducts 32-35 and the cylinders of pistons 8 and 13, to reciprocate pistons 21 and 26. On starting, the working spaces of the cooling units communicate freely through a duct 80 which is subsequently closed by a valve 81 operated in dependence on the speed of the crank-shaft 19. If, during operation, the pistons move too far outwardly, the valve members 50 uncover fluid inlets connected via pipes 54 and line 73 to pump 63 so that oil is admitted to space 30 or 31 to prevent further outward movement of the pistons. Similarly, should the pistons move too far inwardly the valve elements 50 uncover fluid outlets connected via pipes 53 and line 76 to the oil reservoir 66 so that oil flows from the spaces 30 or 31 and further inward movement of the pistons is prevented. The seal between pistons 21 and 26 and their surrounding cylinders is provided by rolling diaphragms 84 and a substantially constant pressure difference between the working space and a space 90 on the side of the seal 84 remote from the working space is achieved by a control unit 85 comprising a piston 87 disposed in a cylinder 86 which is connected by pipes 89 and 91 with spaces 90 and 31 respectively. Oil from space 31 flows between the piston and cylinder to space 90 and thence via pipe 89 to a space 88 on one side of piston 87 which is arranged, when the desired pressure difference between spaces 31 and 90 obtains, to uncover a port 93 so that the oil is discharged. Should the pressure in space 31 increase piston 87 will move to close port 93 and thus increase the pressure in space 90. Since the pressure in space 31 is substantially equal to that in the working space the arrangement results in the desired constant pressure difference between the latter space and space 90. Each cooling unit is provided with a control unit 85. The second pair of cooling units (Figs. 1 to 3, not shown) is arranged so that the compression pistons are adjacent pump II and the expansion pistons adjacent pump I. The spaces 31 of these units are connected to opposite sides of piston 13 of pump II and the spaces 30 to opposite sides of piston 8 of pump I. In a modification (Figs. 5 and 6, not shown) the pump units are mounted in parallel on the crank-case with one pair of cooling units in front of and the other pair behind the plane of the pump units.
GB46223/63A 1962-11-26 1963-11-22 Improvements in and relating to thermo-dynamic reciprocating machines Expired GB1064733A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL285957 1962-11-26

Publications (1)

Publication Number Publication Date
GB1064733A true GB1064733A (en) 1967-04-05

Family

ID=19754246

Family Applications (1)

Application Number Title Priority Date Filing Date
GB46223/63A Expired GB1064733A (en) 1962-11-26 1963-11-22 Improvements in and relating to thermo-dynamic reciprocating machines

Country Status (12)

Country Link
US (1) US3200582A (en)
AT (1) AT241912B (en)
BE (1) BE640436A (en)
CH (1) CH424828A (en)
DE (1) DE1260494B (en)
DK (1) DK122474C (en)
ES (1) ES293813A1 (en)
FR (1) FR1383207A (en)
GB (1) GB1064733A (en)
NL (1) NL285957A (en)
OA (1) OA00905A (en)
SE (1) SE305222B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2450342A1 (en) * 1979-02-28 1980-09-26 Girodin Marius Hot air reciprocating engine - has hydraulic connection between piston and displacement vessel to give large volume ratio

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4526008A (en) * 1983-03-21 1985-07-02 Texas Instruments Incorporated Pneumatically controlled split cycle cooler
JPS61226546A (en) * 1985-03-29 1986-10-08 Aisin Seiki Co Ltd Driving device for stirling engine
WO2014005229A1 (en) 2012-07-04 2014-01-09 Kairama Inc. Temperature management in gas compression and expansion

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2484392A (en) * 1945-08-30 1949-10-11 Hartford Nat Bank & Trust Co Hot-air engine actuated refrigerating apparatus
US2567637A (en) * 1947-01-31 1951-09-11 Hartford Nat Bank & Trust Co Hot gas piston apparatus with flexible crank coupling
US2590519A (en) * 1948-01-21 1952-03-25 Hartford Nat Bank & Trust Co Hot-gas engine or refrigerator
NL69322C (en) * 1948-10-12 1952-01-15
US2657528A (en) * 1948-12-24 1953-11-03 Hartford Nat Bank & Trust Co Hot gas engine enclosing two thermodynamic cycles
US2616248A (en) * 1949-01-27 1952-11-04 Hartford Nat Bank & Trust Co Hot-gas reciprocating engine
US2657552A (en) * 1950-06-10 1953-11-03 Hartford Nat Bank & Trust Co Hot gas engine refrigerator
US2664699A (en) * 1950-11-24 1954-01-05 Hartford Nat Bank & Trust Co Multicylinder double-acting hotgas reciprocating engine
BE530595A (en) * 1953-07-24
FR1128275A (en) * 1955-07-28 1957-01-03 Hermetic oleo-pneumatic compressor
US3117414A (en) * 1961-07-14 1964-01-14 Wisconsin Alumni Res Found Thermodynamic reciprocating apparatus

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2450342A1 (en) * 1979-02-28 1980-09-26 Girodin Marius Hot air reciprocating engine - has hydraulic connection between piston and displacement vessel to give large volume ratio

Also Published As

Publication number Publication date
FR1383207A (en) 1964-12-24
DK122474B (en) 1972-03-06
DK122474C (en) 1972-07-31
DE1260494B (en) 1968-02-08
NL285957A (en)
AT241912B (en) 1965-08-25
BE640436A (en) 1964-05-26
CH424828A (en) 1966-11-30
US3200582A (en) 1965-08-17
SE305222B (en) 1968-10-21
OA00905A (en) 1968-03-22
ES293813A1 (en) 1964-01-16

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