GB367747A - - Google Patents

Info

Publication number
GB367747A
GB367747A GB367747DA GB367747A GB 367747 A GB367747 A GB 367747A GB 367747D A GB367747D A GB 367747DA GB 367747 A GB367747 A GB 367747A
Authority
GB
United Kingdom
Prior art keywords
speed
homann
sectional area
flow
nipple
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.)
Active
Application number
Other languages
English (en)
Publication of GB367747A publication Critical patent/GB367747A/en
Active legal-status Critical Current

Links

Landscapes

  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Gas Burners (AREA)
GB367747D Active GB367747A (enrdf_load_stackoverflow)

Publications (1)

Publication Number Publication Date
GB367747A true GB367747A (enrdf_load_stackoverflow)

Family

ID=1744701

Family Applications (1)

Application Number Title Priority Date Filing Date
GB367747D Active GB367747A (enrdf_load_stackoverflow)

Country Status (1)

Country Link
GB (1) GB367747A (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3516771A (en) * 1968-08-01 1970-06-23 Hewlett Packard Co Burner for spectroscopic use
US4865820A (en) * 1987-08-14 1989-09-12 Davy Mckee Corporation Gas mixer and distributor for reactor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3516771A (en) * 1968-08-01 1970-06-23 Hewlett Packard Co Burner for spectroscopic use
US4865820A (en) * 1987-08-14 1989-09-12 Davy Mckee Corporation Gas mixer and distributor for reactor

Similar Documents

Publication Publication Date Title
US7568345B2 (en) Effervescence injector for an aero-mechanical system for injecting air/fuel mixture into a turbomachine combustion chamber
CA2093712C (en) Apparatus and methods for reducing fuel/air concentration oscillations in gas turbine combustors
CN112088277B (zh) 提高燃气涡轮中的燃烧稳定性的系统和方法
JP2939155B2 (ja) 燃焼のための噴霧角度の小さい液体燃料噴霧器
US6027330A (en) Low NOx fuel gas burner
US20120047902A1 (en) Fuel delivery system for a turbine engine
US6880339B2 (en) Combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
US20120227407A1 (en) Burner for a turbine
GB367747A (enrdf_load_stackoverflow)
RU201164U1 (ru) Горелочное устройство для комбинированного сжигания топлива
GB2143938A (en) Fuel burner for a gas turbine engine
US4217088A (en) Burner for very low pressure gases
RU99113U1 (ru) Двухконтурная центробежно-пневматическая форсунка
GB2073400A (en) Fuel injector
GB1154963A (en) Method for Burning Fuel and Fuel Burner for such method
CN116951470A (zh) 燃气涡轮发动机及用于其的混合器组件、燃烧室、雾化燃料的方法
US2530269A (en) Atomizer for oil burners
GB687667A (en) Improvements in or relating to combustion systems
SU340838A1 (ru) Инжекдионная газовая горелка
WO1993022601A1 (en) Premix liquid and gaseous combustion nozzle for use with a gas turbine engine
CN108469039B (zh) 一种具有低排放的壁面射流椭圆形燃烧室
GB703431A (en) Improvements in or relating to atomising type fluid fuel burners
SU1288447A1 (ru) Инжекционна горелка и способ ее работы
GB189824007A (en) Improvements in or relating to Incandescence Gas Burners.
GB283568A (enrdf_load_stackoverflow)