FIELD: engines and pumps.
SUBSTANCE: housing of a jet-turbine engine has the possibility of installing into it of a variety of blades and includes attachment devices of the end of each blade, which are located on the housing side opposite to blades. Attachment devices include a ring-shaped element passing around the housing, and the housing includes holes through which ends of blades pass for their interaction with attachment devices. The housing is made of long fibres connected with thermoplastic resin. The ring-shaped element is obtained by pultrusion and soaked with thermoplastic resin welded with thermoplastic resin of the housing; besides, the whole assembly is connected by means of hot pressing. The other invention of the group relates to a jet-turbine engine containing the above housing and many blades, each of which has an end connected to the housing.
EFFECT: group of inventions allows simplifying production and assembly of a jet-turbine engine housing.
5 cl, 4 dwg
| Title |
Year |
Author |
Number |
| VANE OF TURBOJET ENGINE, IN PARTICULAR, VANE OF OUTLET STRAIGHTENER, AND TURBOJET ENGINE WITH SUCH VANES |
2011 |
- Masson Rishar
- Denleavi Patrik
- Dezhuajo Bertran
|
RU2544102C2 |
| STRUCTURAL OR NON-STRUCTURAL CONNECTING SUPPORT OF COMPRESSOR CRANKCASE OF JET TURBINE ENGINE; INTERMEDIATE CRANKCASE OF JET TURBINE ENGINE, AND JET TURBINE ENGINE |
2008 |
- Zhjulliar Zhak
- Molinari Oliv'E
- Morel' Patrik
- Riu Zhorzh
|
RU2472042C2 |
| BLADE OF COMPOSITE MATERIAL, COMPRESSOR OF GAS TURBINE ENGINE COMPRISING SUCH BLADE AND TURBOJET ENGINE |
2008 |
- Le Khong Son
- Lombar Zhan-P'Er Fransua
|
RU2498083C2 |
| DRUM FORMING ROTOR OF TURBOMACHINE AND COMPRESSOR AND TURBOJET ENGINE WITH SUCH DRUM |
2003 |
|
RU2314437C2 |
| COMPRESSOR HOUSING RESISTING TITANIUM FIRE, HIGH-PRESSURE COMPRESSOR WITH SUCH HOUSING AND AIRCRAFT ENGINE EQUIPPED WITH SUCH COMPRESSOR |
2009 |
- Ferre, Loran
- Mon, Klod, Marsel'
|
RU2524782C2 |
| STATOR OF AIRCRAFT GAS TURBINE ENGINE AND AIRCRAFT GAS TURBINE ENGINE |
2015 |
- Charbonnier, Simon, Pierre, Claude
- Perrier, Matthieu, Yoann
|
RU2706098C2 |
| AIRCRAFT NACELLE THRUST REVERSER GRID |
2018 |
- Oliveux Geraldine
- Desjoyeaux Bertrand
- Thomas Cedric
|
RU2766970C2 |
| AIRCRAFT TURBOJET ENGINE ATTACHMENT STRUT |
2006 |
- D'Oshon Lionel'
- Setu Zhan-Mishel'
- Lafon Loran
- Shart'E David
|
RU2399558C2 |
| FRAME, COMPRESSOR, TURBO AND GASTURBINE ENGINE INCLUDED INTO FRAME |
2003 |
- Le B'E Filipp
- Lebre Jan
- Mon Marsel'
|
RU2324076C2 |
| GAS-TURBINE ENGINE CONTAINING FAN AND COMPRESSOR |
2016 |
- Gribanovskij Vladimir Aleksandrovich
|
RU2625078C1 |
