GB652812A - Rotary piston engine or compressor - Google Patents

Rotary piston engine or compressor

Info

Publication number
GB652812A
GB652812A GB2256248A GB2256248A GB652812A GB 652812 A GB652812 A GB 652812A GB 2256248 A GB2256248 A GB 2256248A GB 2256248 A GB2256248 A GB 2256248A GB 652812 A GB652812 A GB 652812A
Authority
GB
United Kingdom
Prior art keywords
engine
compressor
passages
fluid
abutments
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
GB2256248A
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 GB2256248A priority Critical patent/GB652812A/en
Publication of GB652812A publication Critical patent/GB652812A/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
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/40—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member
    • F01C1/44—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and having a hinged member with vanes hinged to the inner member

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

652,812. Rotary engines and compressors. SCHNABEL, E. F. J. M. Aug. 26, 1948, No. 22562. '[Class 110(ii)] [Also in Group XIII] The engine or compressor comprises one or more rotors 2 each carrying rocking vanes 8 having tip portions t which bear on the bore of an annular working chamber 21 and flattened portions f which co-act with one or more abutments 20. Lightening holes 30 cause the tip portions to be forced outwards under centrifugal force. A common rotor may have several working chambers and several' compression chambers, arranged axially, and may be used in a refrigeration apparatus. Each vane has axial extensions 35a which engage segmented-shaped grooves in end rings 35, 36, attached to the rotor 2. The vanes run with slight clearances between them and the stator bore. Where combustion gases are used in the engine part, the gases are filtered before being used. Covers 18, 19 may be provided with stuffing boxes. In Fig. 1 working fluid is admitted at a and exhausted through ports b. Fig. 4 shows a compressor 43 and engine 44 having six and five pistons respectively. The compressor, Fig. 5, has abutments 48, 49, 50 and fluid enters through passages 83 and is discharged through inclined passages 84. Operating fluid for the engine enters and leaves through similar passages 83, 84. Fig. 7 shows a plant with gas compressor 85 supplying a combustion chamber 88 and two engine rotors 86, 87 being driven by heated fluid supplied from a condenser 90 by means of a pump 91 through a pipe 92. Air and gas are supplied through pipes 94. Relative sizes of the engine parts are given in the Specification.
GB2256248A 1948-08-26 1948-08-26 Rotary piston engine or compressor Expired GB652812A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2256248A GB652812A (en) 1948-08-26 1948-08-26 Rotary piston engine or compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2256248A GB652812A (en) 1948-08-26 1948-08-26 Rotary piston engine or compressor

Publications (1)

Publication Number Publication Date
GB652812A true GB652812A (en) 1951-05-02

Family

ID=10181439

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2256248A Expired GB652812A (en) 1948-08-26 1948-08-26 Rotary piston engine or compressor

Country Status (1)

Country Link
GB (1) GB652812A (en)

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