Device and method employing a turbine for contributing...

F - Mech Eng,Light,Heat,Weapons – 01 – D

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Details

F01D 1/24 (2006.01) B64C 11/00 (2006.01) B64C 11/14 (2006.01) B64C 27/32 (2006.01) B64C 27/82 (2006.01) F01D 5/12 (2006.01) F01D 5/34 (2006.01) F02C 6/20 (2006.01) F02K 3/06 (2006.01)

Patent

CA 2336021

Turbine (14) is added to the spinner (12) of a propeller (10) to provide a contribution to propulsive thrust of the propeller (10). The turbine (14) comprises a group of turbine modules (14a) which are mounted on the periphery of the spinner (12) between root portions of the propeller blades (10b). Each module (14a) includes a curved row of angulated turbine vanes (16) held between a curved base plate (18) and a curved outer plate (20).

On ajoute une turbine (14) à la casserole (12) d'une hélice (10) pour contribuer à la poussée propulsive de l'hélice (10). La turbine (14) comprend un groupe de modules (14a) de turbine qui sont montés sur la périphérie de l'hélice (12), entre les parties emplantures des aubes (10b) de l'hélice. Chaque module (14a) comporte une rangée courbe d'aubes de turbine angulaires (16) maintenues entre une plaque de base courbe (18) et une plaque extérieure courbe (20).

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