Platform for a turbomachinery blade
Номер патента: CA1042348A
Опубликовано: 14-11-1978
Автор(ы): Charles T. Salemme, David J. Harris, Richard Ravenhall
Принадлежит: General Electric Co
Опубликовано: 14-11-1978
Автор(ы): Charles T. Salemme, David J. Harris, Richard Ravenhall
Принадлежит: General Electric Co
Реферат: PLATFORM FOR A TURBOMACHINERY BLADE Abstract A turbomachinery blade platform comprising a pair of complementary platform halves, each having an outer flow path defining shroud adapted to extend generally laterally of the blade. An inner flange on each platform half, also extending generally laterally of the blade, is retained in a cooperating slot formed within the support structure retaining the blade. A structural member extending between the shroud and the flange is contoured to conform to an overlapping wedging surface disposed about the blade airfoil surface. The platform is thus provided with redundant retention by both the blade and by the blade support structure.
Rotor assembly with structural platforms for gas turbine engines
Номер патента: EP4223980A2. Автор: Jason Husband,James Glaspey. Владелец: Raytheon Technologies Corp. Дата публикации: 2023-08-09.