UA18702A - method of manufacturing the investment casting from titanium alloys - Google Patents

method of manufacturing the investment casting from titanium alloys

Info

Publication number
UA18702A
UA18702A UA4838617A UA4838617A UA18702A UA 18702 A UA18702 A UA 18702A UA 4838617 A UA4838617 A UA 4838617A UA 4838617 A UA4838617 A UA 4838617A UA 18702 A UA18702 A UA 18702A
Authority
UA
Ukraine
Prior art keywords
gas
mould
determined
static compaction
titanium alloys
Prior art date
Application number
UA4838617A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Ігор Дмитрович Биков
Игорь Дмитриевич Быков
Валерій Григорович Клочихін
Валерий Григорьевич Клочихин
Ігор Альфредович Розбігаєв
Игорь Альфредович Разбегаев
Олег Ігоревич Биков
Олег Игоревич Быков
Іван Якович Кондратов
Иван Яковлевич Кондратов
Original Assignee
Запорізьке Виробниче Об'Єднання "Моторобудівник"
Запорожское производственное объединение "Моторостроитель"
Український Науково-Дослідний Інститут Спеціальних Сталей, Сплавів Та Ферросплавів
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Запорізьке Виробниче Об'Єднання "Моторобудівник", Запорожское производственное объединение "Моторостроитель", Український Науково-Дослідний Інститут Спеціальних Сталей, Сплавів Та Ферросплавів filed Critical Запорізьке Виробниче Об'Єднання "Моторобудівник"
Priority to UA4838617A priority Critical patent/UA18702A/en
Publication of UA18702A publication Critical patent/UA18702A/en

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Abstract

A method of manufacturing investment casting from titanium alloys includes production of a mould, filling, gas-static compaction of castings. At first, alloy is poured into the mould, without filling a cavity of head, and prior to gas-static compaction sizes of shrinkage pores are determined, for example by X-ray method, and location of depressions after gas-static compaction is corrected. After this, at subsequent production of the moulds above the places of shrinkage pores compensating cavities are performed, which size is determined from dependences: h = 2a, S = 6b, I = 6c, where: h, S, I - height, width and length of the compensating cavities respectively; and a, b, c height, width and length of the shrinkage pores respectively, determined after filling metal into the mould without heads. The gas-static compaction of castings is performed together with the compensators.
UA4838617A 1990-06-12 1990-06-12 method of manufacturing the investment casting from titanium alloys UA18702A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UA4838617A UA18702A (en) 1990-06-12 1990-06-12 method of manufacturing the investment casting from titanium alloys

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UA4838617A UA18702A (en) 1990-06-12 1990-06-12 method of manufacturing the investment casting from titanium alloys

Publications (1)

Publication Number Publication Date
UA18702A true UA18702A (en) 1997-12-25

Family

ID=74538873

Family Applications (1)

Application Number Title Priority Date Filing Date
UA4838617A UA18702A (en) 1990-06-12 1990-06-12 method of manufacturing the investment casting from titanium alloys

Country Status (1)

Country Link
UA (1) UA18702A (en)

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