摘要:
A method of manufacturing a gas turbine engine component includes providing a core having a brittle feature, supporting the feature with a first meltable material, arranging the core with the first meltable material in a first mold, and surrounding the core and the first meltable material with a second meltable material to provide a component shape. The method also includes coating the second meltable material with a refractory material to produce a second mold, removing the first and second meltable material, and casting a component in the second mold.
摘要:
A method of manufacturing a replacement body (99) for a component (W) is provided. The method includes the steps of: a) additively manufacturing a crucible (100) for casting of the replacement body (99); b) solidifying a metal material within the crucible (100) to form a directionally solidified microstructure within the replacement body (99); and c) removing the crucible (100) to reveal the directionally solidified replacement body (99).
摘要:
Purposes of the present invention are to provide a dry coated sand having a high degree of fluidity at the room temperature, a method of advantageously producing the coated sand, and a method of producing a casting mold having excellent properties, by using the coated sand. The dry coated sand is obtained by mixing an aqueous solution of a water glass used as a binder, with a heated refractory aggregate, whereby water in the aqueous solution is evaporated, and a coating layer of the binder is formed on surfaces of the refractory aggregate. A moisture percentage in the thus obtained dry coated sand is controlled so as to be not more than 0.5% by mass. The intended casting mold is obtained by filling a molding cavity of a forming mold, with the dry coated sand, and passing a steam through the coated sand, to solidify or cure the coated sand.
摘要:
An article includes a first portion having a first grain pattern and a second portion having a second grain pattern different from the first grain pattern. The article is a cast article such as a turbine engine blade.
摘要:
A method and a device for rapidly drying ware shell and a ware shell are provide, and it pertains to the field of precision casting technology. It is designed to solve the problem that the ware shell drying process fails to ensure high quality of a ware shell and rapid drying simultaneously when the ware shell has a complex structure. The method includes following steps: a. putting a ware shell to be dried in a sealed chamber; b. vacuuming the sealed chamber under the premise condition of controlling the ware shell in a constant temperature state, and cooling the gas in the sealed chamber in a predetermined time period to condensate the moisture in the sealed chamber; c. vacuum injecting gas to the sealed vacuum chamber to make the chamber return to normal atmosphere pressure; D. determining whether the ware shell is dry. If result is YES, then end, otherwise back to step b.
摘要:
Dosage apparatus for a machine adapted for manufacturing sand cores, comprising an inlet (1) for receiving bonding agent, a vessel (2) where the received bonding agent is stored, a conveying unit (3) for conveying the bonding agent from one site to another within the apparatus (100), control means for controlling the conveying unit (3) and an evacuation region (5) through which the bonding agent coming from the vessel (2) is evacuated towards its final destination. The conveying unit (3) comprises a variable-frequency drive, and the apparatus (100) comprises a scale (6) that is adapted for detecting the mass of the bonding agent that is supplied and is communicated with the control means, the control means being adapted for controlling the evacuation of the bonding agent from the vessel (2) depending on the detections obtained with the scale (6).
摘要:
The method consists of foundry casting a preform according to shapes having desired dimensions, transferring said foundry preform into a tunnel furnace, then an operation of preheating at a temperature ranging from 400 to 500°, transferring the preheated foundry preform into a forge die of substantially smaller dimensions and shape and carrying out the coining operation at a pressure ranging from 600 to 700 MPa, the method being characterised in that before transferring the preheated foundry preform into the forge die, said forge die and the preform positioning means consisting of pins are subjected to a powder spraying operation over the entire inner surface of the forge die likely to receive the preheated foundry preform, and over the pins.