RU94011568A - FUEL SUPPLY SYSTEM FOR BURNING CAMERA - Google Patents

FUEL SUPPLY SYSTEM FOR BURNING CAMERA

Info

Publication number
RU94011568A
RU94011568A RU94011568/06A RU94011568A RU94011568A RU 94011568 A RU94011568 A RU 94011568A RU 94011568/06 A RU94011568/06 A RU 94011568/06A RU 94011568 A RU94011568 A RU 94011568A RU 94011568 A RU94011568 A RU 94011568A
Authority
RU
Russia
Prior art keywords
channel
stream
supply system
fuel supply
flow
Prior art date
Application number
RU94011568/06A
Other languages
Russian (ru)
Other versions
RU2118756C1 (en
Inventor
Чиоу Иау-Пин
Эроглу Аднан
Original Assignee
АББ Менеджмент АГ
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
Priority claimed from CH01088/93A external-priority patent/CH687832A5/en
Application filed by АББ Менеджмент АГ filed Critical АББ Менеджмент АГ
Publication of RU94011568A publication Critical patent/RU94011568A/en
Application granted granted Critical
Publication of RU2118756C1 publication Critical patent/RU2118756C1/en

Links

Claims (1)

В системе подачи топлива с сжиганием предварительно подготовленной смеси впрыскивается газообразное и/или жидкое топливо в качестве дополнительного потока в газообразный проходящий по каналу основной поток. Дополнительный поток является значительно меньшим по массе потоком, чем основной. Основной поток направляется через вихревые генераторы, многие из которых расположены в ряд по окружности канала, по меньшей мере на одной стенке канала. Дополнительный поток вводится в канал непосредственно с области расположения вихревых генераторов. Вихревой генератор обнаруживает три свободно обтекаемые плоскости, ориентированные в направлении потока, одна из которых является верхней плоскостью, а две другие - боковыми поверхностями. Топливо подается в канал через насадки, которые находятся за вихревыми генераторами или в них.In the fuel supply system with the combustion of a previously prepared mixture, gaseous and / or liquid fuel is injected as an additional stream into the gaseous main stream passing through the channel. The additional stream is a much smaller mass stream than the main stream. The main flow is directed through vortex generators, many of which are located in a row around the circumference of the channel, at least on one wall of the channel. Additional flow is introduced into the channel directly from the area of the location of the vortex generators. The vortex generator detects three freely streamlined planes oriented in the direction of flow, one of which is the upper plane, and the other two the lateral surfaces. Fuel is fed into the channel through nozzles that are behind or in vortex generators.
RU94011568/06A 1993-04-08 1994-04-07 Combustion chamber fuel supply system RU2118756C1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH01088/93A CH687832A5 (en) 1993-04-08 1993-04-08 Fuel supply for combustion.
CH1088193 1993-04-08
CH1088/93 1993-04-08

Publications (2)

Publication Number Publication Date
RU94011568A true RU94011568A (en) 1995-12-20
RU2118756C1 RU2118756C1 (en) 1998-09-10

Family

ID=4202193

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94011568/06A RU2118756C1 (en) 1993-04-08 1994-04-07 Combustion chamber fuel supply system

Country Status (6)

Country Link
US (1) US5658358A (en)
EP (1) EP0619456B1 (en)
JP (1) JP3527278B2 (en)
CH (1) CH687832A5 (en)
DE (1) DE59404243D1 (en)
RU (1) RU2118756C1 (en)

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EP3301368A1 (en) 2016-09-28 2018-04-04 Siemens Aktiengesellschaft Swirler, combustor assembly, and gas turbine with improved fuel/air mixing
RU2685629C2 (en) * 2017-05-24 2019-04-22 Шор Борис Иосифович Liquid activator
US10969107B2 (en) * 2017-09-15 2021-04-06 General Electric Company Turbine engine assembly including a rotating detonation combustor
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