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INVENTION
Russian Federation Patent RU2075632
GASDYNAMIC INSTALLATION
Name of the inventor: Viktor Perov
The name of the patentee: Viktor Perov
Address for correspondence:
Starting date of the patent: 1995.03.29
Usage: used in the wind industry. The inventive gasdynamic arrangement comprises a turbine, the axis of the bearing, the housing with inlet and outlet nozzle, a power turbine, a compressor chamber, an annular burner and ignition system, wherein the turbine compressor chamber, an annular burner and power turbine are line-open type, on the same axis bearings without the housing to define said dynamic compression turbine oncoming flow of fuel and supplying it to an annular burner and an ignition system with a consequent impact on the speed of the jet turbine blades.
DESCRIPTION OF THE INVENTION
The invention relates to power engineering, namely to the design of the installation.
Known gas-dynamic installation operating in windmill mode, comprising a turbine, the bearing axis of the housing with an inlet and an outlet nozzle (as with the USSR N 1285185, cl F 03 D 1/04, published 1987 -.... A prototype).
The aim of the invention is to increase the efficiency, the use of natural, biological, and others. Gas, reducing environmental pollution, in the absence of fuel able to work in windmill mode.
The invention consists in an open line-of basic units on the same axis with the incident flow of combustion dynamic spray process.
To achieve this purpose the gas-dynamic installation design (Fig. 1) is a turbine 1 with blades 2 and intakes 3, a compression chamber 4, an annular burner 5 elektrozazhigatelyami 6 and a pipeline supplying fuel through the hollow shaft 7, on which the power turbine 8 blades 9 and bearing 10.
When starting the fuel is fed under pressure through the hollow axis 7 and into the annular burner pipes 5 at a time is switched through the ignition system and elektrozazhigateli 6 ignites the fuel-air mixture. Hot flow exerts pressure on inclined blades mounted to the jet 9 power turbine 8 and the entire power plant begins to unwind. In the process of promotion of the air flow is captured by the blades of the turbine 1 and 2 through the air inlets 3 is supplied to the compressor chamber 4, where the degree of compression with an increase in speed increases and reaches the burner ring 5, while increasing fuel supply to improve the power.
When the forward movement of the installation due to the oncoming flow of the degree of compression and the blade 2 of the turbine 1 increases significantly transform into working windmill mode, allowing further increase capacity.
CLAIM
Gas-dynamic plant comprising a turbine, the bearing axis of the housing with inlet and outlet nozzles, characterized in that it further comprises a power turbine, a compressor chamber, an annular burner and ignition system, wherein the turbine compressor chamber, an annular burner and power turbine are line-open type on the same axis with bearings without housing to define said dynamic compression turbine oncoming flow of fuel and supplying it to an annular burner and an ignition system with a consequent impact on the speed of the jet turbine blades.
print version
Publication date 02.04.2007gg
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