GB653185A - Improvements in or relating to rotary engines, pumps and the like - Google Patents

Improvements in or relating to rotary engines, pumps and the like

Info

Publication number
GB653185A
GB653185A GB1349348A GB1349348A GB653185A GB 653185 A GB653185 A GB 653185A GB 1349348 A GB1349348 A GB 1349348A GB 1349348 A GB1349348 A GB 1349348A GB 653185 A GB653185 A GB 653185A
Authority
GB
United Kingdom
Prior art keywords
rotor
disc
engine
rotors
vane
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
GB1349348A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB1349348A priority Critical patent/GB653185A/en
Publication of GB653185A publication Critical patent/GB653185A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/002Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
    • F01C11/004Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle and of complementary function, e.g. internal combustion engine with supercharger
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C3/00Rotary-piston machines or engines with non-parallel axes of movement of co-operating members
    • F01C3/02Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged at an angle of 90 degrees
    • F01C3/025Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged at an angle of 90 degrees of intermeshing engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
    • F02C6/20Adaptations of gas-turbine plants for driving vehicles

Abstract

653,185. Rotary engines and pumps. GOODYEAR, J. W. May 19, 1948, No. 13493. [Class 110(ii)] In an engine of the worm and worm-wheel type the rotor vane 25 is of gradually varying inclination relatively to the axis of the rotor 11 the rotor being curved longitudinally to conform to the peripheral curvature of the abutment disc 17, the rotor being of increased diameter towards at least one end. The cross-sectional area of the working space 24 may be constant or vary towards one or both ends to give compression or expansion of a fluid. One of two relatively moving parts such as 29 may be of rubber or the like, or lined therewith. Fig. 1 shows a pump with inlet port 21 and outlet port 23, though the pump may be reversed. The apparatus may act as an engine. Sealing members 30, 31 isolate the working chamber from the disc chamber 16. Fig. 4 shows a compressor in which fluid flows from an inlet 21 through a working chamber to an outlet 23. The rotor may be reversed and the apparatus used as an engine. The vane 25 meshes with slots 26 in a disc 17 and, the vane tip runs closely to the casing periphery 27. In Fig. 5 a vaned rotor 11 meshes with a disc 17 and working fluid enters an inlet 27, Fig. 1, is compressed and fuel infected at 39. The gases expand to drive the rotor and are exhausted through a duct 23 after flowing between turbine blades 49, 50 on the rotor and fixed guide blades 52. In addition, inlet moving blades 48 co-act with fixed blades 51. The rotor may carry more than one vane, and a rotor may co-act with two or more discs. An engine drive may be taken off the disc shaft. In a modification two axially-displaced discs of different diameters, Fig. 14 (not shown), mesh with vanes on one rotor to form an internalcombustion engine. Fig. 15 shows a further form in which the rotor 11 is shaped as an annulus with a convolute vane 25 which operates in a working chamber 38 and meshes with a slotted wheel 17. A cone 42, on the shaft 10, maintains the crosssectional area of the discharge channel 23 constant from the end of the rotor. A modified engine has two rotors axially spaced on the same shaft, each meshing with a slotted disc, fluid entering the rotors from the ends and being discharged through a common central outlet, this arrangement balances end thrust on the shaft. In a final example there are four rotors on two shafts with two discs between the shafts each meshing with two rotors arranged diametrically opposite each other. The fluid flows through the four rotors in series.
GB1349348A 1948-05-19 1948-05-19 Improvements in or relating to rotary engines, pumps and the like Expired GB653185A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1349348A GB653185A (en) 1948-05-19 1948-05-19 Improvements in or relating to rotary engines, pumps and the like

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1349348A GB653185A (en) 1948-05-19 1948-05-19 Improvements in or relating to rotary engines, pumps and the like

Publications (1)

Publication Number Publication Date
GB653185A true GB653185A (en) 1951-05-09

Family

ID=10023968

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1349348A Expired GB653185A (en) 1948-05-19 1948-05-19 Improvements in or relating to rotary engines, pumps and the like

Country Status (1)

Country Link
GB (1) GB653185A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3083529A (en) * 1959-03-24 1963-04-02 Charles W F Hemilton Hydraulic jet propulsion apparatus for water-borne craft
DE1244012B (en) * 1962-08-10 1967-07-06 Alexander Nikolaus Karawias Water jet propulsion for ships
GB2419382A (en) * 2004-10-21 2006-04-26 Richard See Rotary device for processing compressible fluids
US7650871B2 (en) 2003-06-17 2010-01-26 Turnstile Technology Limited Rotary compressor and expander, and rotary engine using the same

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3083529A (en) * 1959-03-24 1963-04-02 Charles W F Hemilton Hydraulic jet propulsion apparatus for water-borne craft
DE1244012B (en) * 1962-08-10 1967-07-06 Alexander Nikolaus Karawias Water jet propulsion for ships
US7650871B2 (en) 2003-06-17 2010-01-26 Turnstile Technology Limited Rotary compressor and expander, and rotary engine using the same
GB2419382A (en) * 2004-10-21 2006-04-26 Richard See Rotary device for processing compressible fluids
GB2419382B (en) * 2004-10-21 2010-03-31 Richard See Rotary device

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