GB645298A - Improvements in hot gas engines - Google Patents
Improvements in hot gas enginesInfo
- Publication number
- GB645298A GB645298A GB897348A GB897348A GB645298A GB 645298 A GB645298 A GB 645298A GB 897348 A GB897348 A GB 897348A GB 897348 A GB897348 A GB 897348A GB 645298 A GB645298 A GB 645298A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cylinder
- fins
- burner
- cylinder head
- ducts
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02G—HOT GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS; USE OF WASTE HEAT OF COMBUSTION ENGINES; NOT OTHERWISE PROVIDED FOR
- F02G1/00—Hot gas positive-displacement engine plants
- F02G1/04—Hot gas positive-displacement engine plants of closed-cycle type
- F02G1/043—Hot gas positive-displacement engine plants of closed-cycle type the engine being operated by expansion and contraction of a mass of working gas which is heated and cooled in one of a plurality of constantly communicating expansible chambers, e.g. Stirling cycle type engines
- F02G1/053—Component parts or details
- F02G1/057—Regenerators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B77/00—Component parts, details or accessories, not otherwise provided for
- F02B77/11—Thermal or acoustic insulation
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
645,298. Hot gas engines. SHELL REFINING & MARKETING CO., Ltd., LUBBOCK, I., and TIPLER, W. March 30, 1948, No. 8973. [Class 7(i)] [Also in Group XIII] The outer face of the or each cylinder head is exposed to radiation from a burner and an annular space surrounds the cylinder wall and contains a number of ducts for the flow of working gas into and out of the cylinder alternating with a number of separate ducts for the egress of combustion products from the burner and a plurality of radial passages or channels are formed in or on the interior face of the cylinder head and connect the ducts for the flow of the working gas with the interior of the cylinder. Each cylinder 1 of the engine (one cylinder only being shown) is provided with a combustion chamber 2 above a cylinder head 3. The products of combustion from a burner 4 pass into spaces 9 between fins 8 arranged in an annular space around the cylinder and after leaving the spaces 9 flow through a combustion air preheater 11 to a duct 12 leading to atmosphere. As shown (Fig. 2) there are a number of sets of fins 8 in the annular space and each set is separated from the next by a radial pocket 10 having fins 10a projecting into it. The upper end of the cylinder has an inturned lip 24 and fins 25 on the underside of the cylinder head 3 extend to this lip. In between the fins 25 streamlined fins 22 also carried by the cylinder head are located. Thus working medium in the interior of the cylinder can flow through spaces 26 between the fins into the pockets 10 and thus to a regenerator 19. Below the regenerator is located a cooler comprising tubes 20 for the passage of the working medium, which are cooled by fluid e.g. water circulated by a pump (not shown) from a tank 21. Below the cooler is a space 29 connected by a pipe 30 with the space below the piston of the next cylinder of the engine. The pipe 30 of the last cylinder (not shown) is connected to the space at the underside of the piston 18. Combustion air for the burner 4 enters at 13 passes through the preheater 11 and then through an annular space 15 between a refractory lining 14 and the combustion chamber. The preheater comprises a corrugated metal sheet having corrugations running parallel to, the axis of the combustion chamber. The fins 22, 25 assist in cooling the cylinder head. In a modification a large number of fine radial bores or channels in the cylinder head are provided instead of passages defined by a series of fins and connect the interior of the cylinder, with the gas ducts so as to provide cooling of the cylinder head by the working gas. If desired the head may be provided both with a system of fins and with a series of fine bores or channels. An air bleed 16 is provided for cooling the burner and preventing carbon deposits. The burner is ignited by an igniter 5.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB897348A GB645298A (en) | 1948-03-30 | 1948-03-30 | Improvements in hot gas engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB897348A GB645298A (en) | 1948-03-30 | 1948-03-30 | Improvements in hot gas engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB645298A true GB645298A (en) | 1950-10-25 |
Family
ID=9862876
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB897348A Expired GB645298A (en) | 1948-03-30 | 1948-03-30 | Improvements in hot gas engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB645298A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0037206A2 (en) * | 1980-03-28 | 1981-10-07 | Perry Edward Miles | A thermodynamic rotary engine |
-
1948
- 1948-03-30 GB GB897348A patent/GB645298A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0037206A2 (en) * | 1980-03-28 | 1981-10-07 | Perry Edward Miles | A thermodynamic rotary engine |
EP0037206A3 (en) * | 1980-03-28 | 1983-07-20 | Perry Edward Miles | A thermodynamic rotary engine |
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