GB440493A - Improvements in and relating to internal-combustion turbines and compressor units - Google Patents

Improvements in and relating to internal-combustion turbines and compressor units

Info

Publication number
GB440493A
GB440493A GB1941534A GB1941534A GB440493A GB 440493 A GB440493 A GB 440493A GB 1941534 A GB1941534 A GB 1941534A GB 1941534 A GB1941534 A GB 1941534A GB 440493 A GB440493 A GB 440493A
Authority
GB
United Kingdom
Prior art keywords
compressor
turbine
wedges
vanes
rotor
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
GB1941534A
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.)
BERNARD SIDDONS
Original Assignee
BERNARD SIDDONS
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 BERNARD SIDDONS filed Critical BERNARD SIDDONS
Priority to GB1941534A priority Critical patent/GB440493A/en
Publication of GB440493A publication Critical patent/GB440493A/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
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • F01C21/0809—Construction of vanes or vane holders
    • F01C21/0818—Vane tracking; control therefor
    • F01C21/0827—Vane tracking; control therefor by mechanical means
    • F01C21/0836—Vane tracking; control therefor by mechanical means comprising guiding means, e.g. cams, rollers
    • 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
    • F01C1/34—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 relative reciprocation between the co-operating members
    • F01C1/344—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 relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F01C1/3441—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 relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
    • F01C1/3442—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 relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
    • 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
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • F01C21/0809—Construction of vanes or vane holders
    • F01C21/0881—Construction of vanes or vane holders the vanes consisting of two or more parts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Abstract

440,493. Gas turbines; rotary compressors. FISHER, F. D., and SIDDONS, B., 49, High Street, Beighton, near Sheffield. July 2, 1934, No. 19415. [Classes 110 (ii) and 110 (iii)] Combustible mixture for use in a gas turbine R<2> is compressed in a rotary compressor A of the outwardly-sliding vane type, the charge being ignited in the compressor at the time of minimum volume and released to the turbine through uncovered ports in substantially unexpanded form. Ignition may be by spark-plug or, after the engine has started, by flame passing through a gap in the casing from a chamber which has just been fired to the following compression chamber. The turbine rotor R is mounted on a fixed sleeve, and is geared to the power shaft C. upon which the rotor of the compressor A is mounted, by double-reduction gearing S, T, U, W, which also drives the oil pump and magneto. The vanes of the compressor are channel shaped and are fitted with packing plates A<1> which are pressed axially by wedges A<2>. Clock springs H act on the vanes and wedges.
GB1941534A 1934-07-02 1934-07-02 Improvements in and relating to internal-combustion turbines and compressor units Expired GB440493A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1941534A GB440493A (en) 1934-07-02 1934-07-02 Improvements in and relating to internal-combustion turbines and compressor units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1941534A GB440493A (en) 1934-07-02 1934-07-02 Improvements in and relating to internal-combustion turbines and compressor units

Publications (1)

Publication Number Publication Date
GB440493A true GB440493A (en) 1936-01-01

Family

ID=10128965

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1941534A Expired GB440493A (en) 1934-07-02 1934-07-02 Improvements in and relating to internal-combustion turbines and compressor units

Country Status (1)

Country Link
GB (1) GB440493A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2207703A (en) * 1987-07-20 1989-02-08 Wang Liang Chih Rotary fluid flow machine
EP3943710A1 (en) * 2020-07-24 2022-01-26 Dimitris Ziremidis Sliding vane machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2207703A (en) * 1987-07-20 1989-02-08 Wang Liang Chih Rotary fluid flow machine
EP3943710A1 (en) * 2020-07-24 2022-01-26 Dimitris Ziremidis Sliding vane machine

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