摘要 |
In an aircraft propeller system, a ring 29, 29 surrounds and is fastened to a rotor, such as a turbine or planetary gear transmission, and supports an array of propeller blades. A back-up system for preventing the ring from unwinding from the rotor under the influence of centrifugal load if the ring should fail 53 is provided. In one approach of the invention, a metal foil 50 is wound around the ring to provide a secondary, back-up ring. In another embodiment, "catchers" or hooks (70, Fig 14) are provided which engage flanges (73) provided on the ring. Other embodiments are disclosed. <IMAGE>
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申请人 |
GENERAL ELECTRIC CO., SCHENECTADY, N.Y., US |
发明人 |
HEMSWORTH, MARTIN CARL;HUSAIN, SIFARAT SETH, CINCINNATI, OHIO, US;WAKEMAN, LAWRENCEBURG, INDIANA, US;KROGER, GERARD PAUL, CINCINNATI, OHIO, US |