Tool for extracting a metal piece
AssigneeSafran Aircraft Engines Mexico S.A. De C.V.
InventorsJesus Camarena, Jesus Murillo, Allan Puente, Gumaro Rodriguez, Margarita Limon
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Abstract
An extracting tool for extracting a metal piece located in an aerodynamic stream of a turbomachine, such as a flow splitter nose, includes a rod; a first stop located at a distal end of the rod and provided with a claw for bearing against a first edge of the metal piece; a gripping member translationally mounted to the rod and including a first projecting portion arranged to receive a second, opposite edge of the metal piece; a tightening mechanism configured to keep the gripping member bearing against the metal piece and the first stop.
Claims12
An extracting tool for extracting a metal piece located in an aerodynamic stream of a turbomachine, comprising:
- a rod;
- a first stop located at a distal end of the rod and provided with a claw for bearing against a first edge of the metal piece;
- a gripping member translationally mounted to the rod and comprising a central part and a first projecting portion which projects from the central part, the first projection portion radially projects from the claw of the first stop relative to a longitudinal axis of the rod and is arranged to receive a second, opposite edge of the metal piece;
- a tightening mechanism configured to keep the gripping member bearing against the metal piece and the first stop.
Dependencies are inferred from the claim text.