GB1218392A - Engine-compressor type machine - Google Patents

Engine-compressor type machine

Info

Publication number
GB1218392A
GB1218392A GB314368A GB314368A GB1218392A GB 1218392 A GB1218392 A GB 1218392A GB 314368 A GB314368 A GB 314368A GB 314368 A GB314368 A GB 314368A GB 1218392 A GB1218392 A GB 1218392A
Authority
GB
United Kingdom
Prior art keywords
compressor
framework
pair
pistons
crankshaft
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
GB314368A
Inventor
James Stouffer Campbell
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.)
BRAUN CAMPBELL ENGINEERING Ltd
Original Assignee
BRAUN CAMPBELL ENGINEERING Ltd
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 BRAUN CAMPBELL ENGINEERING Ltd filed Critical BRAUN CAMPBELL ENGINEERING Ltd
Priority to GB314368A priority Critical patent/GB1218392A/en
Publication of GB1218392A publication Critical patent/GB1218392A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F02B75/00—Other engines
    • F02B75/28—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • F02B75/282—Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders the pistons having equal strokes

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)

Abstract

1,218,392. Direct acting compressors. BRAUN-CAMPBELL ENG. Ltd. Jan. 20, 1968, No. 3143/68. Heading F1B. A direct acting compressor comprises a framework 15, a combustion cylinder 14 in the framework a pair of opposed engine pistons 16 reciprocably dispersed in the combustion cylinder, a pair of compressor cylinders 12, 13 aligned one at each end of the combustion cylinder, a pair of compressor pistons 17, 18 slidably disposed one in each compressor cylinder and a pair of piston rods 19 one extending from each end of the combustion cylinder and each connecting one of the engine pistons to one of the compressor pistons. A synchronizing mechanism includes a crankshaft 24 having throws spaced at substantantially 180 degrees, the crankshaft being mounted in the framework for rotation about an axis extending perpendicularly with respect to the axis of the combustion cylinder, a pair of rocker beams 21 each pivotally connected to the framework for oscillation about an axis parallel to the axis of the crankshaft, means pivotally joining each one of the engine pistons to a respective one of the rocker beams at a point on the rocker beam spaced from the connection 55 of the rocker beam to the framework and a pair of connecting rods 25, rotatably connected one to each of the opposite throws of the crankshaft and each pivotally connected to a respective one of the rocker beams at a point 64 between the connection of the rocker beam to the framework and the point of connection on the rocker beam of the means joining the rocker beam to the engine piston. The compressor may comprise a high pressure stage 13, as shown, or may comprise two low pressure stages. The two stage compressor can also be twinned to increase the delivery and thus may be achived by placing two units side by side and utilizing a common crankshaft. Means for varying the stoke of the pistons, is described.
GB314368A 1968-01-20 1968-01-20 Engine-compressor type machine Expired GB1218392A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB314368A GB1218392A (en) 1968-01-20 1968-01-20 Engine-compressor type machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB314368A GB1218392A (en) 1968-01-20 1968-01-20 Engine-compressor type machine

Publications (1)

Publication Number Publication Date
GB1218392A true GB1218392A (en) 1971-01-06

Family

ID=9752762

Family Applications (1)

Application Number Title Priority Date Filing Date
GB314368A Expired GB1218392A (en) 1968-01-20 1968-01-20 Engine-compressor type machine

Country Status (1)

Country Link
GB (1) GB1218392A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5126903U (en) * 1974-08-19 1976-02-27
GB2345517A (en) * 1999-01-09 2000-07-12 Alan Paul Liebing Free piston i.c. engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5126903U (en) * 1974-08-19 1976-02-27
GB2345517A (en) * 1999-01-09 2000-07-12 Alan Paul Liebing Free piston i.c. engine
GB2345517B (en) * 1999-01-09 2002-08-28 Alan Paul Liebing Engine

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