GB337599A - Improvements in process and apparatus for operating explosion turbines - Google Patents

Improvements in process and apparatus for operating explosion turbines

Info

Publication number
GB337599A
GB337599A GB3311629A GB3311629A GB337599A GB 337599 A GB337599 A GB 337599A GB 3311629 A GB3311629 A GB 3311629A GB 3311629 A GB3311629 A GB 3311629A GB 337599 A GB337599 A GB 337599A
Authority
GB
United Kingdom
Prior art keywords
fuel
chamber
operating
explosion turbines
turbines
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
GB3311629A
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 GB3311629A priority Critical patent/GB337599A/en
Publication of GB337599A publication Critical patent/GB337599A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R7/00—Intermittent or explosive combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

337,599. Holzwarth, H. Oct. 31, 1929. Working-fluid supply.-In a gas turbine having an explosion chamber as described in Specification 312,167 the wall 16 at the charging end of the chamber 3 is formed conical so that a contracting- expanding nozzle 14, 21, 17 is formed, the contraction 21 being in the region where the fuel is injected into the air stream. The aid and fuel valves are actuated automatically. The arrangement gives better atomization and scavenging. Specifica,tions 900/11 and 295,635 also are referred to.
GB3311629A 1929-10-31 1929-10-31 Improvements in process and apparatus for operating explosion turbines Expired GB337599A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3311629A GB337599A (en) 1929-10-31 1929-10-31 Improvements in process and apparatus for operating explosion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3311629A GB337599A (en) 1929-10-31 1929-10-31 Improvements in process and apparatus for operating explosion turbines

Publications (1)

Publication Number Publication Date
GB337599A true GB337599A (en) 1930-11-06

Family

ID=10348763

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3311629A Expired GB337599A (en) 1929-10-31 1929-10-31 Improvements in process and apparatus for operating explosion turbines

Country Status (1)

Country Link
GB (1) GB337599A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021243832A1 (en) * 2020-06-03 2021-12-09 西安热工研究院有限公司 Pulse detonation combustion chamber having detonation gas energy distribution smooth structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021243832A1 (en) * 2020-06-03 2021-12-09 西安热工研究院有限公司 Pulse detonation combustion chamber having detonation gas energy distribution smooth structure

Similar Documents

Publication Publication Date Title
GB721126A (en) Improvements in or relating to gas burners
GB639617A (en) Improvements in and relating to combustion chambers
GB588847A (en) Improvements in combustion chambers for internal combustion turbines
GB616695A (en) Improvements in and relating to gas turbine power plants
GB650462A (en) Improvements in or relating to combustion apparatus
GB622513A (en) Improvements in or relating to combustion apparatus
GB579424A (en) Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
GB331555A (en) Method and apparatus for the combustion of pulverised fuel, more particularly pulverised coal
GB587083A (en) Improvements in combustion chambers for internal combustion turbines
GB271706A (en) Improvements in motive fluid generators for use particularly in torpedoes
GB337599A (en) Improvements in process and apparatus for operating explosion turbines
GB565952A (en) Improvements in means for generating a mixture of steam and combustion products under pressure
GB699166A (en) Improvements in or relating to gas turbine plants
GB686425A (en) Improvements in or relating to gas turbine power plants
GB374378A (en) Improvements in and relating to constant volume gas turbines
GB701320A (en) Improvements in or relating to combustion equipment of gas-turbine engines
GB374648A (en) Improvements in and relating to methods of operating cylindrical elongated explosionchambers, in particular for internal combustion turbines
GB805786A (en) Improvements in gas turbine plants associated with gas producers
GB294978A (en) Method of working explosion turbines with coal dust
GB358514A (en) Improvements in or relating to internal combustion turbines
GB215603A (en) Improvements in gas turbines
GB186083A (en) Improved method of and apparatus for the economic transformation of the energy of steam by turbines
GB579511A (en) Improvements in or relating to jet-propulsion apparatus for aircraft
GB715197A (en) Jet propulsion engines
GB510740A (en) Method and apparatus for charging elongated explosion chambers