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 (da)

Publications (1)

Publication Number Publication Date
GB367747A true GB367747A (da)

Family

ID=1744701

Family Applications (1)

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

Country Status (1)

Country Link
GB (1) GB367747A (da)

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
US5211004A (en) Apparatus for reducing fuel/air concentration oscillations in gas turbine combustors
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
EP2177835A2 (en) Fuel delivery system for a turbine engine
US4062182A (en) Combustion chamber for gas turbine engines
CN113324262B (zh) 一种用于低排放燃气轮机的同轴分级气体燃料燃烧室头部
US20120047902A1 (en) Fuel delivery system for a turbine engine
TW200411113A (en) Improved combination of a premixing chamber and a combustion chamber, with low emission of pollutants, for gas turbines running on liquid and/or gas fuel
GB367747A (da)
RU201164U1 (ru) Горелочное устройство для комбинированного сжигания топлива
CN112088277B (zh) 提高燃气涡轮中的燃烧稳定性的系统和方法
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
GB1498135A (en) Gas turbine engine
US2530269A (en) Atomizer for oil burners
GB687667A (en) Improvements in or relating to combustion systems
CN108469039B (zh) 一种具有低排放的壁面射流椭圆形燃烧室
SU340838A1 (ru) Инжекдионная газовая горелка
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.
SU769200A1 (ru) Стеклодувна горелка