GB460794A - Internal combustion turbine - Google Patents

Internal combustion turbine

Info

Publication number
GB460794A
GB460794A GB27769/35A GB2776935A GB460794A GB 460794 A GB460794 A GB 460794A GB 27769/35 A GB27769/35 A GB 27769/35A GB 2776935 A GB2776935 A GB 2776935A GB 460794 A GB460794 A GB 460794A
Authority
GB
United Kingdom
Prior art keywords
turbine
gas
nozzle
temperature
combustion
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
GB27769/35A
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.)
AUGUST VAN DEN HONERT
Original Assignee
AUGUST VAN DEN HONERT
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 AUGUST VAN DEN HONERT filed Critical AUGUST VAN DEN HONERT
Publication of GB460794A publication Critical patent/GB460794A/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/34—Gas-turbine plants characterised by the use of combustion products as the working fluid with recycling of part of the working fluid, i.e. semi-closed cycles with combustion products in the closed part of the cycle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action

Abstract

460,794. Gas turbines. HONERT, A. VAN DEN. Oct. 8, 1935, No. 27769. Convention date, Oct. 9, 1934. [Class 110 (iii)] In an internal-combustion turbine, the relative positions of the nozzle and fuel jets are such that the amount of fuel burnt when the mixture reaches the nozzle throat is enough to raise the temperature of the mixture well above ignition temperature. In the divergent portion of the nozzle combustion continues, but any further increase in temperature is counteracted by a decrease due to the expansion of the gases. The jet from this nozzle can be used either alone to drive a gas turbine or it may be led to an injector where it induces a large mass of gas which passes with it through the.turbine. The inlet end of the jet apparatus g connects with the outlet end of the turbine t through a cooler k whilst the outlet end is connected to the turbine inlet. As combustion gases are continuously being added to the circuit an outlet for exhaust gas is provided where the pressure is atmospheric or above. In a modification, the jet apparatus can be used to create a flow of gas at atmospheric pressure or as a compresser of the gas which expands in the turbine blades.
GB27769/35A 1934-10-09 1935-10-08 Internal combustion turbine Expired GB460794A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NL460794X 1934-10-09

Publications (1)

Publication Number Publication Date
GB460794A true GB460794A (en) 1937-02-04

Family

ID=19786385

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27769/35A Expired GB460794A (en) 1934-10-09 1935-10-08 Internal combustion turbine

Country Status (3)

Country Link
DE (1) DE648907C (en)
GB (1) GB460794A (en)
NL (1) NL39438C (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3996738A (en) * 1975-04-11 1976-12-14 Siegfried Justus Gas turbine circuit system
CH683018A5 (en) * 1990-06-19 1993-12-31 Asea Brown Boveri Process for increasing the compressor-related pressure gradient of a gas turbine of a power plant.
US5271216A (en) * 1990-06-19 1993-12-21 Asea Brown Boveri Ltd. Method for increasing the compressor-related pressure drop of the gas turbine of a power plant

Also Published As

Publication number Publication date
NL39438C (en)
DE648907C (en) 1937-08-14

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