FIELD: engines and pumps.
SUBSTANCE: gas turbine engine structural carcass, for example, intermediate or outlet carcass, is composed by elements including inner and outer coaxial shell rings and radial supports connecting the shell rings. Every said shell ring is composed by multiple cylinder sections, their ends including radial flanges bolted to radial flanges of radial supports. Another invention of proposed set covers gas turbine engine with above described structural carcass.
EFFECT: simplified production and repair.
12 cl, 5 dwg
| Title |
Year |
Author |
Number |
| INTERMEDIATE CASE OF JET TURBINE ENGINE, AND JET TURBINE ENGINE |
2008 |
- Djushatell' T'Erri
- Verso Filipp
|
RU2484262C2 |
| STATOR OF AIRCRAFT GAS TURBINE ENGINE AND AIRCRAFT GAS TURBINE ENGINE |
2015 |
- Charbonnier, Simon, Pierre, Claude
- Perrier, Matthieu, Yoann
|
RU2706098C2 |
| GAS TURBINE ENGINE FAN CHANNEL |
2007 |
- Beten Brjuno Al'Ber
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|
RU2452865C2 |
| GAS TURBINE ENGINE DISTRIBUTOR, GAS TURBINE ENGINE TURBINE AND GAS TURBINE ENGINE |
2009 |
- Fasha T'Erri
- Zhirar Patrik Zhozef Mari
- Supizon Zhan-Ljuk
|
RU2506431C2 |
| BLANK AND SINGLE-PIECE BLADE UNIT FOR INTERMEDIATE CASING OF GAS TURBINE ENGINE |
2013 |
- Zhima Mate
- Kupe Dominik Mari Kristian
- Marshal Yan
- Papen Terri Zhorzh Pol
|
RU2645510C2 |
| PREFORM AND ONE-PIECE BLADE FOR GAS TURBINE ENGINE |
2013 |
- Zhima Mate
- Kupe Dominik Mari Kristian
|
RU2653823C2 |
| INTERTURBINE CASE WITH COOLING CIRCUIT AND GAS TURBINE ENGINE THEREWITH |
2008 |
- Gimbar Zhan-Mishel'
- Pabion Filipp
- Prestel' Sebast'En
- Supizon Zhan-Ljuk
|
RU2450129C2 |
| GAS TURBINE ENGINE |
2015 |
|
RU2613101C1 |
| GUIDE UNIT FOR AIR FLOW AT INLET OF COMBUSTION CHAMBER OF GAS TURBINE ENGINE |
2007 |
|
RU2435104C2 |
| IMPROVED FIRE-FIGHTING DEVICE INTENDED TO BE INSTALLED BETWEEN THE END OF THE AIRCRAFT GAS TURBINE ENGINE BACK PROP AND THE GAS TURBINE ENGINE HOOD LIMITING THE INTERMEDIATE FLOW COMPARTMENT |
2019 |
- Jacon, Bruno, Alexandre, Didier
- Simonotti, Herve
|
RU2795414C2 |
