BRAZING COMPONENTS AND TECHNIQUES
20170368646 ยท 2017-12-28
Inventors
Cpc classification
B23K1/18
PERFORMING OPERATIONS; TRANSPORTING
B23K1/0008
PERFORMING OPERATIONS; TRANSPORTING
F05D2220/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R2900/00017
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2230/237
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R2900/00019
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C7/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F23R3/283
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B23K37/00
PERFORMING OPERATIONS; TRANSPORTING
B23K1/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method of joining includes applying braze to a braze reservoir in a first component. A second component is engaged to the first component, wherein a joint location is defined between the first and second components. A wicking structure provides flow communication from the braze reservoir to the joint location. The method also includes joining the first and second components together at the joint location by applying heat to the braze to flow the braze from the reservoir through the wicking structure to the joint location to form a braze joint at the joint location.
Claims
1. A method of joining comprising: applying braze to a braze reservoir in a first component; engaging a second component to the first component, wherein a joint location is defined between the first and second components, wherein a wicking structure provides flow communication from the braze reservoir to the joint location; heating the braze; flowing the braze from the reservoir through the wicking structure to the joint location; and joining the first and second components together.
2. A method as recited in claim 1, wherein engaging the second component to the first component includes engaging the second component to the first component with the wicking structure between the first and second components.
3. A method as recited in claim 1, wherein engaging the second component to the first component includes engaging the second component to the first component with the first and second components are radially nested, wherein the wicking structure is radially between the first and second components, and wherein the joint location and the braze reservoir are axially spaced apart.
4. A method as recited in claim 1, wherein the first component includes a radial vane, wherein the wicking structure extends radially through the radial vane, and wherein joining the first and second components includes flowing the braze radially outward to the joint location, wherein the joint location is at an end of the radial vane.
5. A method as recited in claim 1, wherein there is a gap between the first and second components on either side of the braze reservoir after the first and second components are engaged, wherein the wicking structure and the joint location are on one side of the braze reservoir, and wherein joining includes flowing the braze into the wicking structure to the joint location leaving the gap on the side of the braze reservoir opposite the wicking structure substantially devoid of braze.
6. A method as recited in claim 1, wherein there is a gap between the first and second components adjacent the wicking structure when the first and second components are engaged, wherein joining includes flowing the braze into the wicking structure to the joint location leaving the gap substantially devoid of braze.
7. A nozzle comprising: a first nozzle component; a second nozzle component joined to the first nozzle component at a joint location; and a wicking structure extending from a braze reservoir to the joint location, wherein the braze reservoir is defined in the first nozzle component.
8. A nozzle as recited in claim 7, wherein the wicking structure and a braze joint are between the first and second nozzle components.
9. A nozzle as recited in claim 7, wherein the first and second nozzle components are radially nested, wherein the wicking structure is radially between the first and second nozzle components, and wherein the joint location and the braze reservoir are axially spaced apart.
10. A nozzle as recited in claim 7, wherein the first nozzle component includes a radial vane, wherein the wicking structure extends radially through the radial vane, and wherein the joint location is at an end of the radial vane.
11. A nozzle as recited in claim 7, wherein there is a gap between the first and second nozzle components on either side of the braze reservoir, wherein the wicking structure and the joint location are on one side of the braze reservoir, and wherein the gap on the side of the braze reservoir opposite the wicking structure is substantially devoid of braze.
12. A nozzle as recited in claim 7, wherein there is a gap between the first and second nozzle components adjacent the wicking structure, wherein the gap is substantially devoid of braze.
13. A nozzle as recited in claim 7, wherein the wicking structure is integral with the first nozzle component.
14. A nozzle as recited in claim 13, wherein the wicking structure includes a repeating pattern.
15. A nozzle as recited in claim 7, wherein the wicking structure includes a semi-sintered material.
16. A nozzle as recited in claim 7, wherein the wicking structure includes a woven material.
17. A method of making a braze joint comprising: applying braze to a braze reservoir in a first component; engaging a second component to the first component, wherein a joint location is defined between the first and second components, wherein a wicking structure provides flow communication from the braze reservoir to the joint location; heating the braze; flowing the braze from the reservoir through the wicking structure to the joint location; and joining the first and second components together.
18. A method as recited in claim 17, further comprising additively manufacturing the wicking structure.
19. A method as recited in claim 18, wherein the wicking structure is additively manufactured as part of at least one of the first or second components.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, preferred embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
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DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0022] Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of a portion of a nozzle in accordance with the disclosure is shown in
[0023] This disclosure describes techniques in brazing using the exemplary context of joining nozzle components, such as used in gas turbine engines. However, those skilled in the art will readily appreciate that brazing techniques as disclosed herein can be used to join any suitable components without departing from the scope of this disclosure.
[0024] A nozzle 100 includes a first nozzle component 102 and a second nozzle component 104 (shown in
[0025] Referring now to
[0026] With reference now to
[0027] With reference to
[0028] With reference now to
[0029] The methods and systems of the present disclosure, as described above and shown in the drawings, provide for brazing with superior properties including improved control over the flow of braze during the brazing process compared to traditional techniques. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.