US4789410A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for heat treating and quenching complex metal components using salt baths
Assignee: RTX Corp
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Filing: 1987-03-03
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Granted: 1988-12-06
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Expires: 2007-03-03
Abstract
Abstract Salt bath techniques are used to heat treat and quench a metal component. The component is first heated to the required heat treatment temperature while disposed within a sealed, first salt bath. Then, while still within the first salt bath, the component is quenched into a second salt bath. Heat is rapidly and uniformly transferred from the hot, first salt bath to the cool, second salt bath, and from the component to the first salt bath. The uniform rate of heat transfer minimizes any undesired stresses on the component, and permits components having complex geometries to be heat treated and quenched without distortion or cracking.
Inventors
- 👤 Robert J. Parizek
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 06:00
CPC Classifications
C; C21; C21D; C21D1/00; C21D1/34; C21D1/44; C21D1/46; C21D1/62; C21D1/63
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
126 words
A method for heating and cooling a metal component, comprising the steps of disposing the component in a first salt bath within a first container; heating the first container to a temperature T 1 , wherein the first salt bath and component therein are raised to the temperature T 1 ; and cooling the first container and the first salt bath and component therewithin by immersing the first container in a second salt bath within a second container such that a portion of the component is in direct contact with the second salt bath, wherein the second salt bath is at a temperature T 2 less than T 1 , and wherein the first salt bath and component therein are cooled to temperature T 2 .
Claim 2
Independent Claim
126 words
A method for heating and cooling a metal component, comprising the steps of disposing the component in a first salt bath within a first container; heating the first container to a temperature T 1 , wherein the first salt bath and component therein are raised to the temperature T 1 ; and cooling the first container and the first salt bath and component therewithin by immersing the first container in a second salt bath within a second container such that a portion of the component is in direct contact with the second salt bath, wherein the second salt bath is at a temperature T 2 less than T 1 , and wherein the first salt bath and component therein are cooled to temperature T 2 .
Claim 3
Dependent Claim
13 words
The method of claim 1, wherein the component is a nickel base superalloy.
Claim 4
Dependent Claim
27 words
The method of claim 2, wherein the component has a nominal composition 12-22Cr, 0-18Co, 2.5-6Mo, 0-4W, 0-4Ta, 0.2-6Al, 0.5-5Ti, 0.01-0.2C, 0.01-0.3B, 0-0.9Zr, 0-1.5V, 0-20Fe, 0-6Cb, balance Ni.
Claim 5
Dependent Claim
31 words
The method of claim 1, wherein the component has a nominal composition of, by weight percent, 12cr-10Co-6W-4.5Al-3Ti-3Mo-1.5Ta-0.3C-0.1Zr-0.015B-balance Ni, T 1 is about 1,120° C. and T 2 is about 540° C.
Claim 6
Independent Claim
157 words
A method for heat treating and quenching an integrally bladed rotor for a gas turbine engine, the rotor comprising a hub, a rim, and a plurality of circumferentially spaced apart blades extending radially outwardly from the rim, the method comprising the steps of disposing the rotor in salt within a salt bath container such that a portion of the rotor hub protrudes from the container, and sealing the rotor within the container, wherein the protruding portion of the hub is not in direct contact with the salt in the container; heating the container and the salt and component therewithin to a temperature T 1 ; and cooling the container and the salt and component therewithin to a temperature T 2 which is less than T 1 by quenching the container in a salt bath at temperature T 2 , wherein during said step of quenching, the protruding portion of the hub directly contacts the quanching salt bath.
Claim 7
Independent Claim
157 words
A method for heat treating and quenching an integrally bladed rotor for a gas turbine engine, the rotor comprising a hub, a rim, and a plurality of circumferentially spaced apart blades extending radially outwardly from the rim, the method comprising the steps of disposing the rotor in salt within a salt bath container such that a portion of the rotor hub protrudes from the container, and sealing the rotor within the container, wherein the protruding portion of the hub is not in direct contact with the salt in the container; heating the container and the salt and component therewithin to a temperature T 1 ; and cooling the container and the salt and component therewithin to a temperature T 2 which is less than T 1 by quenching the container in a salt bath at temperature T 2 , wherein during said step of quenching, the protruding portion of the hub directly contacts the quanching salt bath.
Claim 8
Independent Claim
104 words
A method for heating a metal component to a temperature T 1 and then cooling the component to a temperature T 2 less than T 1 , comprising the steps of disposing the component in a first salt bath at a temperature less than T 1 within a first container, heating the salt bath and the component therein to the temperature T 1 ; and cooling the salt bath and the component therein by immersing the first container into a second salt bath at the temperature T 2 , wherein the first salt bath and component therein are cooled to temperature T 2 .
Claim 9
Independent Claim
104 words
A method for heating a metal component to a temperature T 1 and then cooling the component to a temperature T 2 less than T 1 , comprising the steps of disposing the component in a first salt bath at a temperature less than T 1 within a first container, heating the salt bath and the component therein to the temperature T 1 ; and cooling the salt bath and the component therein by immersing the first container into a second salt bath at the temperature T 2 , wherein the first salt bath and component therein are cooled to temperature T 2 .
References Cited (Backward Citations)
EP0072525A1
Cited
US4583720A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-12-06 | 1992-06-06 | 1992-12-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-12-06 | 1996-06-06 | 1996-12-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-12-06 | 2000-06-06 | 2000-12-06 | $7700.00 | Window Closed / Lapsed |