US2828601A - Hot-gas reciprocating engine - Google Patents

Hot-gas reciprocating engine Download PDF

Info

Publication number
US2828601A
US2828601A US345984A US34598453A US2828601A US 2828601 A US2828601 A US 2828601A US 345984 A US345984 A US 345984A US 34598453 A US34598453 A US 34598453A US 2828601 A US2828601 A US 2828601A
Authority
US
United States
Prior art keywords
pipes
space
hot
groups
reciprocating 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
US345984A
Inventor
Meijer Hugo Hubertus Mettivier
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 US2828601A publication Critical patent/US2828601A/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
    • 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

Definitions

  • the present invention has for its object to provide a difierent construction of a thermodynamic reciprocating apparatus in which the elements of the heat exchanger may be located in the aforesaid manner while the heat exchanger may be manufactured in a simple manner.
  • both the working cylinders of the apparatus and the spaces containing the regenerators and coolers are juxtaposed substantially in the form of an annulus, each working cylinder being situated adjacent the space containing the regenerator and cooler associated with the hot space in this cylinder and each hot space being connected with the regenerator space through a number of juxtaposed pipes.
  • the pipes may be arranged in several different ways. Thus, for example, they may be bent over part of their length in a plane extending parallel with the working surfaces of the pistons reciprocating in the working cylinders.
  • the pipes extend substantially in the direction of length of the working cylinders.
  • each pipe has substantially equal sections.
  • the cycles performed in the thermodynamic reciprocating apparatus should be identical.
  • the pipes are preferably of equal length and width of passage.
  • flame retaining devices will be provided internally or externally of the groups of pipes in order to compel the combustion gases to follow a given path.
  • the groups of pipes are provided with a plating both at the inner and at the outer side of the space bounded by the groups of pipes in such a manner as to compel the combustion gases to pass along the pipes in a longitudinal direction.
  • Fig. 1 is a vertical section taken on the line II in 2,828,691 l atenteii 1, 1 9 5 8 ice
  • Fig. 2 is a plan heater.
  • thermodynamic reciprocating apparatus is a four-cylinder engine whose cylinders 1, 2, 3 and 4 are connected through groups of pipes 9, 10, 11 and 12 respectively with the spaces for the regenerators 5, 6, 7 and 8 respectively.
  • the working spaces and the spaces for the regenerators and coolers are arranged substantially in the form of an annulus.
  • Fig. l the engine shown herein is doubleacting.
  • Fig. 1 shows a cross-section of the cylinder 2 and the space 6 for the regenerator 15 and the cooler 16 while a piston 13 is adapted to reciprocate in the cylinder 2.
  • the working space 14 above said piston is connected through pipes of the group 10 with the space 6 containing said regenerator 15 and cooler 16.
  • the space 6 is connected with the working space below the piston (not shown) of the cylinder 3.
  • the space 14 above the piston 13 is the hot space of the engine, the space below the piston in the cylinder 3 is the cold space.
  • the cold space 27 below the piston 13 is connected through a duct 18 with a space 5 of the regenerator and the cooler associated with the group of pipes 9.
  • the pistons of the working cylinders 1, 2, 3 and 4 reciprocate with a constant phase difference and drive a swash plate mechanism (not shown in the drawing).
  • the piston rods may alternatively be coupled with a different mechanism, for example a crank shaft mechanism.
  • the groups of heater pipes all occupy an equal surface area of the wall of the space 19.
  • a burner 20 supplying its heat energy to the groups of heating pipes.
  • a plating 21 At the inner side of the pipes in the space 19 is provided a plating 21, and at the outer side a plating 22 furnished with local apertures 23.
  • the combustion gases pass over the pipes in their direction of length and leave the thermodynamic reciprocating engine through apertures 23.
  • all the pipes of each group Preferably, all the pipes of each group have substantially the same length and Width of passage.
  • the sections of the individual pipes have the same length but sections spaced wider apart from one another are shorter.
  • a hot-gas reciprocating apparatus comprising a plurality of working cylinders, each cylinder having at least one reciprocatingpiston defining therewith a hot space,

Landscapes

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

Description

April 1, 1958 H. H. M. MEIJER HOT-GAS RECIPROCATING ENGINE Filed March 31, 1955 HUGO AETTIVIER MEIJER M' AGETJ? HOT-GAS RECIPROCATING ENGINE Hugo Hubertus Mettivier Meijer, White Plains, N. Y., assignor, by mesne assignments, to North American Philips Company, Inc, New York, N. Y., a corporation of Delaware Application March 31, 1953, Serial No. 345,984
Claims priority, application Netherlands April 26, 1952 2 Claims. (Cl. 60-24) the heat exchanger in such a manner that the elements of the heat exchanger together form a wall for absorbing heat energy and the part of the wall surface which is occupied by the elements associated with one cycle is at least substantially equal to the part of the wall surface occupied by the elements associated with other cycles. Such a construction results in that the quantity of energy given oil to each individual group of elements is substantially equal.
The present invention has for its object to provide a difierent construction of a thermodynamic reciprocating apparatus in which the elements of the heat exchanger may be located in the aforesaid manner while the heat exchanger may be manufactured in a simple manner.
In accordance with the invention, both the working cylinders of the apparatus and the spaces containing the regenerators and coolers are juxtaposed substantially in the form of an annulus, each working cylinder being situated adjacent the space containing the regenerator and cooler associated with the hot space in this cylinder and each hot space being connected with the regenerator space through a number of juxtaposed pipes.
The pipes may be arranged in several different ways. Thus, for example, they may be bent over part of their length in a plane extending parallel with the working surfaces of the pistons reciprocating in the working cylinders.
In a suitable embodiment of the invention the pipes extend substantially in the direction of length of the working cylinders.
In a further advantageous embodiment of the inventio each pipe has substantially equal sections.
As a rule the cycles performed in the thermodynamic reciprocating apparatus should be identical. In this regard the pipes are preferably of equal length and width of passage.
As a rule, flame retaining devices will be provided internally or externally of the groups of pipes in order to compel the combustion gases to follow a given path. In a further embodiment of the invention, the groups of pipes are provided with a plating both at the inner and at the outer side of the space bounded by the groups of pipes in such a manner as to compel the combustion gases to pass along the pipes in a longitudinal direction.
In order that the invention may be readily carried into effect it will now be described with reference to the accompanying drawing, given by way of example, in which Fig. 1 is a vertical section taken on the line II in 2,828,691 l atenteii 1, 1 9 5 8 ice Fig. 2 is a plan heater.
As shown in Fig. 2, the thermodynamic reciprocating apparatus is a four-cylinder engine whose cylinders 1, 2, 3 and 4 are connected through groups of pipes 9, 10, 11 and 12 respectively with the spaces for the regenerators 5, 6, 7 and 8 respectively. The working spaces and the spaces for the regenerators and coolers are arranged substantially in the form of an annulus. Referring more particularly to Fig. l the engine shown herein is doubleacting. Fig. 1 shows a cross-section of the cylinder 2 and the space 6 for the regenerator 15 and the cooler 16 while a piston 13 is adapted to reciprocate in the cylinder 2. The working space 14 above said piston is connected through pipes of the group 10 with the space 6 containing said regenerator 15 and cooler 16. Through a duct 17 the space 6 is connected with the working space below the piston (not shown) of the cylinder 3. The space 14 above the piston 13 is the hot space of the engine, the space below the piston in the cylinder 3 is the cold space. Similarly, the cold space 27 below the piston 13 is connected through a duct 18 with a space 5 of the regenerator and the cooler associated with the group of pipes 9. The pistons of the working cylinders 1, 2, 3 and 4 reciprocate with a constant phase difference and drive a swash plate mechanism (not shown in the drawing). The piston rods may alternatively be coupled with a different mechanism, for example a crank shaft mechanism. The groups of heater pipes all occupy an equal surface area of the wall of the space 19. At the top is provided a burner 20 supplying its heat energy to the groups of heating pipes. At the inner side of the pipes in the space 19 is provided a plating 21, and at the outer side a plating 22 furnished with local apertures 23. The combustion gases pass over the pipes in their direction of length and leave the thermodynamic reciprocating engine through apertures 23. Preferably, all the pipes of each group have substantially the same length and Width of passage. The sections of the individual pipes have the same length but sections spaced wider apart from one another are shorter.
While I have shown and described the preferred embodiment of my invention, it will be understood that the latter may be embodied otherwise than as herein specifiview of the groups of wpipes-ofithe cally illustrated or described and that in the illustrated.
embodiment certain changes in the details of construction and in the arrangement of parts may be made without departing from the underlying idea or principle of the invention within the scope of the appended claims.
What I claim is:
1. A hot-gas reciprocating apparatus comprising a plurality of working cylinders, each cylinder having at least one reciprocatingpiston defining therewith a hot space,
a plurality of containers each having a regenerator and one reciprocating piston defining therewith a hot space, I a plurality of containers each having a regenerator and a cooler therein, said cylinders and containers being juxtaposed to form substantially an annulus, a plurality of groups of similarly shaped and adjacent pipes, a burner supplying heat energy to said groups of pipes, each group j a a ,of pipes connecting each of 'said hot spaces with its asso- References Cited in the file of this patent ciated regenerator space, a plurality of upstanding walls UNITED STATES PATENTS on the inner sides of said groups of pipes, and a plurality of substantially parallel walls being provided with aper- 3251640 woOdburY et Sept 1885 tunes on the outer sides of said groups of pipes, said walls 5 3341153 Babcock 121 1886 substantially enclosing said pipes to thereby form alconduit which compels the combustion gases of said burner to pass over said pipes and leave said conduit through said apertures.
US345984A 1952-04-26 1953-03-31 Hot-gas reciprocating engine Expired - Lifetime US2828601A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL2828601X 1952-04-26

Publications (1)

Publication Number Publication Date
US2828601A true US2828601A (en) 1958-04-01

Family

ID=19875910

Family Applications (1)

Application Number Title Priority Date Filing Date
US345984A Expired - Lifetime US2828601A (en) 1952-04-26 1953-03-31 Hot-gas reciprocating engine

Country Status (1)

Country Link
US (1) US2828601A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3248870A (en) * 1960-07-29 1966-05-03 Morgenroth Henri Stirling cycle engine divided into a pressure generating unit and energy converting unit
DE2164522A1 (en) * 1971-12-24 1973-06-28 Maschf Augsburg Nuernberg Ag HOT GAS PISTON MACHINE
US3817036A (en) * 1971-08-27 1974-06-18 United Stirling Ab & Co Arcuate shaped heat transfer pipes
US3822553A (en) * 1972-08-22 1974-07-09 United Stirling Ab & Co Hot gas engine heater heads
US3845626A (en) * 1971-12-18 1974-11-05 Kg United Stirling Ab & Co Hot gas stirling cycle engine with in-line cylinders
US4195613A (en) * 1977-05-20 1980-04-01 Kommanditbolaget United Stirling (Sweden) Ab & Co. Double-acting four-cylinder hot gas engine
US4665700A (en) * 1984-01-18 1987-05-19 United Stirling Ab Hot gas engine heater head

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US325640A (en) * 1885-09-01 Hot-air engine
US334153A (en) * 1886-01-12 George h
US1508522A (en) * 1923-11-21 1924-09-16 Automatic Refrigerating Compan Refrigerating machine
US2272925A (en) * 1936-06-26 1942-02-10 Gen Motors Corp Refrigerating apparatus

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US325640A (en) * 1885-09-01 Hot-air engine
US334153A (en) * 1886-01-12 George h
US1508522A (en) * 1923-11-21 1924-09-16 Automatic Refrigerating Compan Refrigerating machine
US2272925A (en) * 1936-06-26 1942-02-10 Gen Motors Corp Refrigerating apparatus

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3248870A (en) * 1960-07-29 1966-05-03 Morgenroth Henri Stirling cycle engine divided into a pressure generating unit and energy converting unit
US3817036A (en) * 1971-08-27 1974-06-18 United Stirling Ab & Co Arcuate shaped heat transfer pipes
US3845626A (en) * 1971-12-18 1974-11-05 Kg United Stirling Ab & Co Hot gas stirling cycle engine with in-line cylinders
DE2164522A1 (en) * 1971-12-24 1973-06-28 Maschf Augsburg Nuernberg Ag HOT GAS PISTON MACHINE
US3795112A (en) * 1971-12-24 1974-03-05 Maschf Augsburg Nuernberg Ag Hot gas cylinder-piston apparatus
US3822553A (en) * 1972-08-22 1974-07-09 United Stirling Ab & Co Hot gas engine heater heads
US4195613A (en) * 1977-05-20 1980-04-01 Kommanditbolaget United Stirling (Sweden) Ab & Co. Double-acting four-cylinder hot gas engine
US4665700A (en) * 1984-01-18 1987-05-19 United Stirling Ab Hot gas engine heater head

Similar Documents

Publication Publication Date Title
US2817950A (en) Hot-gas reciprocating engine construction
US3861146A (en) Hot-gas reciprocating engine
GB136195A (en) Method and Apparatus for Inducing Heat-changes.
US2480525A (en) Multicylinder hot-gas engine
US2828601A (en) Hot-gas reciprocating engine
US3717993A (en) Preheater assembly for stirling engine
US4365474A (en) Module for constructing a double-acting four-cylinder Stirling engine
US4069671A (en) Stirling engine combustion assembly
JP2662612B2 (en) Stirling engine
US2664699A (en) Multicylinder double-acting hotgas reciprocating engine
US3157024A (en) Regenerative thermal device
US2611235A (en) Multicylinder hot gas reciprocating piston engine of the doubleacting type
SU1617173A1 (en) Multicylinder stirling engine of double action
US3940934A (en) Stirling engines
US3802198A (en) Double-acting hot gas multi-cylinder piston engine
US3822552A (en) Pipe configuration for hot gas engine
US2175448A (en) Engine cooling system
US3898841A (en) External combustion hot gas piston engine
US3862542A (en) Hot-gas engine burner-heater
US1824528A (en) Internal combustion engine
US2657528A (en) Hot gas engine enclosing two thermodynamic cycles
US3845626A (en) Hot gas stirling cycle engine with in-line cylinders
US3852961A (en) Heat exchanger pre-heating combustion air in a stirling cycle engine
US3817036A (en) Arcuate shaped heat transfer pipes
US2616672A (en) Heat exchanger