Lateral deflection interblade platform for a turbojet blade...

Details Lateral deflection interblade platform for a turbojet blade... Lateral deflection interblade platform for a turbojet blade...

F - Mech Eng,Light,Heat,Weapons

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F01D 5/30 (2006.01) F01D 5/02 (2006.01) F01D 5/22 (2006.01) F01D 9/02 (2006.01) F01D 11/00 (2006.01) F01D 21/04 (2006.01)

Patent

CA 2475148

An inter-vane platform (3), for a vane support disk (1) of a turbine engine fan, comprises a central part (5) of one piece with the support disk (1) between two adjacent vanes (2), and two lateral parts (8,9), forming extensions to two lateral edges (6,7) of the central part (5), and each designed in such a way as to deflect under the impact of the vane (2) opposite which it is located.

Une plate-forme inter-aubes (3), pour un disque de support d'aubes (1) d'une soufflante de turboréacteur, comprend une partie centrale (5) solidarisée au disque de support (1) entre deux aubes adjacentes (2), et deux parties latérales (8,9) prolongeant deux bords latéraux (6,7) de la partie centrale (5) et chacune agencée de manière à fléchir sous l'impact de l'aube (2) en regard de laquelle elle est placée.

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