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Combustion chamber design for a gas turbine engine having a deflector with a protruding, combustion gas turbine engine comprising the above structure, and gas turbine engines
Combustion chamber design for a gas turbine engine having a deflector with a protruding, combustion gas turbine engine comprising the above structure, and gas turbine engines
1.u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 chamber u0441u0433u043eu0440u0430u043du0438u00a0 u0434u043bu00a0 gas turbine u0434u0432u0438u0433u0430u0442u0435u043bu00a0 containing u0434u043eu043du043du0443u044e part (4) u0441u0433u043eu0440u0430u043du0438u00a0 chamber, which has at least one substantially u043au0440u0443u0433u043bu043e the hole (6), a deflector (10) installed to the rear flow side (4b) on the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0 in u0443u043fu043eu043cu00a0u043du0443u0442u043eu043c inlet (6) with the aid of the u043du0430u043fu0440u0430u0432u043bu00a0 of the shell (12), a system (8) u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0,u0441u0432u00a0u0437u0430u043du043du0443u044e with u0443u043fu043eu043cu00a0u043du0443u0442u044bu043c aperture and containing a circular conical body (28), u0440u0430u0441u0448u0438u0440u00a0u044eu0449u0438u0439u0441u00a0 direction on flow and u043fu0440u043eu0445u043eu0434u00a0u0449u0438u0439 through u0443u043fu043eu043cu00a0u043du0443u0442u043eu0435 hole, and the means for u0434u0435u0446u0435u043du0442u0440u0438u0440u043eu0432u0430u043du0438u00a0 u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 towards the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0, u043eu0442u043bu0438u0447u0430u044eu0449u0430u00a0u0441u00a0, u0434u0435u0444u043bu0435u043au0442 bps (10) contains a ring acting edge (14).u043fu0440u043eu0445u043eu0434u00a0u0449u0443u044e in u0440u0430u0434u0438u0430u043bu044cu043du043eu043c direction inside the conical body (28) of the system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 contains at its rearward end to the flow of ring groove (30), tci u0440u044bu0442u0443u044e towards the outside and u0440u0430u0441u043fu043eu043bu0430u0433u0430u044eu0449u0443u044eu0441u00a0 on one line in the direction u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u0440u0430u0434u0438u0430u043bu044cu043du043eu043c serving a deflector (14), thusto this u0432u044bu0441u0442u0443u043fu0430u044eu0449u0430u00a0 edges had the opportunity u0443u0431u0438u0440u0430u0442u044cu0441u00a0 in u0443u043fu043eu043cu00a0u043du0443u0442u0443u044e groove in the case of u0434u0435u0446u0435u043du0442u0440u0438u0440u043eu0432u0430u043du0438u00a0 system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 towards the base of the camera u0433u043eu0440u0430u043du0438u00a0.;2. u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 on p.1, in which u043au043eu043bu044cu0446u0435u0432u0430u00a0 canal (30) u043au043eu043du0438u0447u0435u0441u043au043eu0433u043e corps formed u0434u0432u0443u043cu00a0 sidewalls (42, 44), u043eu0442u0441u0442u043eu00a0u0449u0438u043cu0438 from each other in the direction of u0441u0432u00a0u0437u0430u043du043du044bu043cu0438 between with and u043eu0441u0435u0432u043eu043c a circular base part (40), and u0440u0430u0441u0441u0442u043eu00a0u043du0438u0435 between u0443u043fu043eu043cu00a0u043du0443u0442u044bu043cu0438 sidewalls (42,the grooves (44) thicker than the protruding edges (14) of the deflector (10) u0434u043bu00a0 u043eu0431u0435u0441u043fu0435u0447u0435u043du0438u00a0 u0446u0438u0440u043au0443u043bu00a0u0446u0438u0438 air u0432u0435u043du0442u0438u043bu00a0u0446u0438u0438 in any possible u0434u0435u0446u0435u043du0442u0440u0438u0440u043eu0432u0430u043du0438u0438 system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 towards the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0.;3. u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 on p.1, which means that the possibility of u0434u0435u0446u0435u043du0442u0440u0438u0440u043eu0432u0430u043du0438u00a0 system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 towards the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0, u043fu0440u0435u0434u0441u0442u0430u0432u043bu00a0u044eu0442 a ring (24) u0441u0436u0430u0442u0438u00a0 installed with the front flow side (4a) on the base of the chamber (4) u0441u0433u043eu0440u0430u043du0438u00a0 and secure against u043du0430u043fu0440u0430u0432u043bu00a0u044eu0449u0435u0439 casings (12), with which they had u043bu00a0u044eu0442 ring groove (26).open with the axis (x -- x) u043eu0442u0432u0435u0440u0441u0442u0438u00a0 (6) carried out in the bottom of the cell u0441u0433u043eu0440u0430u043du0438u00a0 and conical body (28) of the system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 additionally contains to u043bu044cu0446u0435u0432u043eu0439 flange (32) is able to slide in the direction in u0440u0430u0434u0438u0430u043bu044cu043du043eu043c u043au0430u043du0430u0432u043au0435 (26) formed u0443u043fu043eu043cu00a0u043du0443u0442u044bu043c ring u0441u0436u0430u0442u0438u00a0 and u0443u043fu043eu043cu00a0u043du0443u0442u043eu0439 u043du0430u043fu0440u0430u0432u043bu00a0u044eu0449u0435u0439 casings oh.;4. u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 on 3, in which the flange (32) u043au043eu043du0438u0447u0435u0441u043au043eu0433u043e shell (28) in the direction of the flow with the help of u043fu0440u043eu0434u043eu043bu0436u0430u0435u0442u0441u00a0 essentially cylindrical part (34), u043au043eu0442u043eu0440u0430u00a0 u0441u043eu0435u0434u0438u043du00a0 u0435u0442u0441u00a0 with groove (30) with the aid of a ring (36).;5. u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 on paragraph 4, in which the axis (36) u043au043eu043du0438u0447u0435u0441u043au043eu0433u043e shell (28) contains many holes (52) u0432u0435u043du0442u0438u043bu00a0u0446u0438u0438, u043eu0442u043au0440u044bu0432u0430u044eu0449u0438u0445u0441u00a0 front on the flow side (4a) the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0 and u0432u044bu0445u043eu0434u00a0u0449u0438u0445 back on stream part (4b) of the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0, against the protruding edges (14) of the deflector (10).;6. u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 on article 3, which u0440u0430u0434u0438u0430u043bu044cu043du0430u00a0 height protruding edges (14) of the deflector (10) is at least equal to the height of u0444u043bu0430u043du0446u0430 (32) u043au043eu043du0438u0447u0435u0441u043au043eu0433u043e shell (28) u0434u043bu00a0 on u0435u0441u043fu0435u0447u0435u043du0438u00a0 protection system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 in any possible u0434u0435u0446u0435u043du0442u0440u0438u0440u043eu0432u0430u043du0438u0438 system u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 towards the base of the chamber u0441u0433u043eu0440u0430u043du0438u00a0.;7. u043au043eu043du0441u0442u0440u0443u043au0446u0438u00a0 on 1, in which the system (8) u0432u043fu0440u044bu0441u043au0438u0432u0430u043du0438u00a0 additionally contains at least one u0437u0430u0432u0438u0445u0440u0438u0442u0435u043bu044c (20) of the air contained in the front end for the flow of u043au043eu043du0438u0447u0435u0441u043au043eu0433u043e shell (28), and a ring (18) u0446u0435u043du0442u0440u0438u0440u043eu0432u0430u043du0438u00a0 enshrined at the front end for the flow of air u0437u0430u0432u0438u0445u0440u0438u0442u0435u043bu00a0 and covering the fuel injector (16).;8. the camera u0441u0433u043eu0440u0430u043du0438u00a0 gas turbine u0434u0432u0438u0433u0430u0442u0435u043bu00a0, u0441u043eu0434u0435u0440u0436u0430u0449u0430u00a0 design in accordance with paragraph 1.;9. turboshaft, which contains design, in accordance with paragraph 1.
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