RU2010100673A - GAS TURBINE INSTALLATION - Google Patents
GAS TURBINE INSTALLATION Download PDFInfo
- Publication number
- RU2010100673A RU2010100673A RU2010100673/06A RU2010100673A RU2010100673A RU 2010100673 A RU2010100673 A RU 2010100673A RU 2010100673/06 A RU2010100673/06 A RU 2010100673/06A RU 2010100673 A RU2010100673 A RU 2010100673A RU 2010100673 A RU2010100673 A RU 2010100673A
- Authority
- RU
- Russia
- Prior art keywords
- housing
- adjacent
- shaft
- turbine
- combustion chambers
- Prior art date
Links
- 238000009434 installation Methods 0.000 title claims abstract 3
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000002485 combustion reaction Methods 0.000 claims abstract 4
- 239000000446 fuel Substances 0.000 claims abstract 2
- 230000007246 mechanism Effects 0.000 claims abstract 2
- 239000000203 mixture Substances 0.000 claims abstract 2
Landscapes
- Supercharger (AREA)
Abstract
Газотурбинная установка, состоящая из корпуса, центробежного компрессора, вала, камер сгораний и корпуса турбины, вала, сборника газовых продуктов с выхлопными патрубками и др. механизмы, отличающаяся тем, что она выполнена корпусом с воздухозаборником, приготавливающим топливную смесь, прилегающим к центробежному компрессору с увеличенным диаметром диска по отношению его лопаток, заключенными в кожух с примыкающими к нему по внешней окружности, симметрично расположенные окна входа камер сгораний, как минимум две с окнами выхода, прилегающими в др. половине корпуса к лопаткам турбины, так и за ними по всей окружности, прилегает кольцевой сборник газовых продуктов с выхлопными патрубками. Gas turbine installation, consisting of a housing, a centrifugal compressor, a shaft, combustion chambers and a turbine housing, a shaft, a collection of gas products with exhaust pipes, and other mechanisms, characterized in that it is made of a housing with an air intake preparing the fuel mixture adjacent to a centrifugal compressor with the increased diameter of the disk relative to its blades, enclosed in a casing with adjacent to it along the outer circumference, symmetrically located windows of the entrance of the combustion chambers, at least two with exit windows, at ayuschimi in others. half casing to the turbine blades and for them over the entire circumference, adjacent annular gas collection products tailpipes.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2010100673/06A RU2010100673A (en) | 2010-01-11 | 2010-01-11 | GAS TURBINE INSTALLATION |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2010100673/06A RU2010100673A (en) | 2010-01-11 | 2010-01-11 | GAS TURBINE INSTALLATION |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2010100673A true RU2010100673A (en) | 2011-07-20 |
Family
ID=44752135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2010100673/06A RU2010100673A (en) | 2010-01-11 | 2010-01-11 | GAS TURBINE INSTALLATION |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2010100673A (en) |
-
2010
- 2010-01-11 RU RU2010100673/06A patent/RU2010100673A/en unknown
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