GB734359A - Improvements in internal combustion engines - Google Patents

Improvements in internal combustion engines

Info

Publication number
GB734359A
GB734359A GB3040152A GB3040152A GB734359A GB 734359 A GB734359 A GB 734359A GB 3040152 A GB3040152 A GB 3040152A GB 3040152 A GB3040152 A GB 3040152A GB 734359 A GB734359 A GB 734359A
Authority
GB
United Kingdom
Prior art keywords
shaft
cylinders
cranks
engine
pistons
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
GB3040152A
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.)
HARRY ROBERT MAYES
Original Assignee
HARRY ROBERT MAYES
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 HARRY ROBERT MAYES filed Critical HARRY ROBERT MAYES
Priority to GB3040152A priority Critical patent/GB734359A/en
Publication of GB734359A publication Critical patent/GB734359A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B9/00—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
    • F01B9/04—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft
    • F01B9/042—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the connections comprising gear transmissions

Abstract

734,359. Motor power plant; jet propulsion plant. MAYES, H. R. Dec. 1, 1953 [Dec. 1, 1952], No. 30401/52. Class 110 (3). [Also in Group XXVII] In a motor power plant including an internalcombustion engine with two or more cylinders 1 disposed parallel to and spaced equally around the drive shaft 5, the pistons 2 actuating cranks 4 connected to the shaft 5 to transmit power thereto, a turbine wheel 13 is fixed to or connected by gearing with the shaft 5 and arranged concentrically with said shaft to be driven by the exhaust gases from the cylinders 1 so as to impart power to the shaft 5. As shown the cranks 4 are geared to a common gear wheel 6 on the shaft 5 which drives an air screw 10 and the power plant, arranged inside a cowling 11, exhausts through a jet orifice 15. The engine has four cylinders 1 arranged 90 degrees apart around the shaft 5 and rotary valves 14 for the cylinders are driven by a gear wheel 8 on the shaft 5, the pistons of each pair of diametrically opposite cylinders being arranged to work in the same phase. A fly wheel 16 and cooling fan or supercharging compressor 12 may also be provided on the shaft 5. Each cylinder 1 may be arranged to contain two pistons connected to the same crank 4, all of the cranks being geared to the same gear wheel 6, and this bank of cylinders may be duplicated to form a sixteencylinder engine, each bank of cylinders being geared to a separate wheel 6 on the shaft 5. Alternatively each cylinder 1 may contain opposed pistons acting on separate cranks and similar arrangements are possible in an engine having six cylinders 60 degrees apart in each bank.
GB3040152A 1952-12-01 1952-12-01 Improvements in internal combustion engines Expired GB734359A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3040152A GB734359A (en) 1952-12-01 1952-12-01 Improvements in internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3040152A GB734359A (en) 1952-12-01 1952-12-01 Improvements in internal combustion engines

Publications (1)

Publication Number Publication Date
GB734359A true GB734359A (en) 1955-07-27

Family

ID=10307108

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3040152A Expired GB734359A (en) 1952-12-01 1952-12-01 Improvements in internal combustion engines

Country Status (1)

Country Link
GB (1) GB734359A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3574997A (en) * 1969-03-26 1971-04-13 Gerald H Syrovy High pressure hot gas generator for turbines
GB2201467A (en) * 1987-02-24 1988-09-01 Teledyne Ind A turbocharged compound cycle ducted fan engine
WO2004074653A1 (en) * 2003-02-24 2004-09-02 Pratt & Whitney Canada Corp. Compact compound engine package
EP2503129A1 (en) * 2011-02-07 2012-09-26 Nasser Saeed B ALGhamdi Gear Engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3574997A (en) * 1969-03-26 1971-04-13 Gerald H Syrovy High pressure hot gas generator for turbines
GB2201467A (en) * 1987-02-24 1988-09-01 Teledyne Ind A turbocharged compound cycle ducted fan engine
WO2004074653A1 (en) * 2003-02-24 2004-09-02 Pratt & Whitney Canada Corp. Compact compound engine package
WO2004074654A1 (en) * 2003-02-24 2004-09-02 Pratt & Whitney Canada Corp. Integral cooling system for rotary engine
US7412831B2 (en) 2003-02-24 2008-08-19 Pratt & Whitney Canada Corp. Integral cooling system for rotary engine
US7654087B2 (en) 2003-02-24 2010-02-02 Pratt & Whitney Canada Corp. Compact compound engine package
EP2503129A1 (en) * 2011-02-07 2012-09-26 Nasser Saeed B ALGhamdi Gear Engine

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