Method for producing a cylindrical component
09821368 ยท 2017-11-21
Assignee
Inventors
Cpc classification
B21K1/26
PERFORMING OPERATIONS; TRANSPORTING
F01D25/24
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B21J5/06
PERFORMING OPERATIONS; TRANSPORTING
Y10T29/4932
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B21D5/01
PERFORMING OPERATIONS; TRANSPORTING
International classification
B21K1/26
PERFORMING OPERATIONS; TRANSPORTING
B21J5/06
PERFORMING OPERATIONS; TRANSPORTING
B21D22/26
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to a method for producing a cylindrical component, particularly of turbomachines. In the process, a heated blank is provided. The blank is then formed to create a flat blank (2). The flat blank (2) is next bent and/or rolled to form a cylindrical half-shell (40).
Claims
1. A method for producing a cylindrical component for turbomachines, comprising the steps of: (a) providing a heated blank; (b) press forming the heated blank to form a flat blank; (c) bending or rolling the flat blank into a cylindrical half-shell; (d) forming at least two half-cylindrical-shells with steps (a) through (c); and (e) configuring and arranging the at least two half-cylindrical-shells formed in step (d) into a housing.
2. The method according to claim 1, wherein the flat blank is substantially rectangular in shape.
3. The method according to claim 1, wherein the flat blank has a machining allowance on at least one of its contours.
4. The method according to claim 3, wherein the machining allowance is between 0 and 10 mm.
5. The method according to claim 1, wherein at least one rib and/or one eyelet is formed in at least one surface of the blank.
6. The method according to claim 1, wherein at least one contact surface of each of the half-cylindrical-shells is machined to a final dimension.
7. The method according to claim 1, wherein the step of press forming is accomplished by drop forging.
8. The method according to claim 1, wherein the at least two half-cylindrical-shells have identical outer contours after the step of press forming is complete.
9. The method according to claim 8, further comprising the step of: (f) providing the housing as a cylindrical component in a turbomachine.
10. The method according to claim 8, further comprising the step of: providing the housing as a cylindrical component in a turbomachine.
11. A method for producing a cylindrical component for turbomachines, comprising the steps of: providing a heated blank; press forming the heated blank to form a flat blank; bending or rolling the flat blank into a half-cylindrical-shell; forming at least two half-cylindrcal-shells; and configuring and arranging the at least two half-cylindrical-shells into a housing, the at least two cylindrical half-shells having identical outer contours after the step of press forming is complete.
Description
BRIEF DESCRIPTION OF THE DRAWING FIGURES
(1) In the following, preferred exemplary embodiments of the invention will be described in detail on the basis of the schematic drawing. Shown therein are:
(2)
(3)
DESCRIPTION OF THE INVENTION
(4) Shown in
(5) The front first contact surface 13 borders the bottom lengthwise edge 6 on the outer face 12. The rear second contact surface 15, which is not depicted, borders the top lengthwise edge 4 on the outer face 12. The third contact surface 17 borders the first cross edge 8 on the outer face 12. The fourth contact surface 19, which is not depicted, borders the second cross edge 10 on the outer face 12.
(6) A plurality of cross ribs 18 to 30 lie between the flange projections 14 and 16 and, in this case, are parallel to the cross edges 8 and 10. The position of the ribs is typically defined by the strength requirements. In this case, all cross ribs 18 to 30 have the same thickness d.sub.R. Molded between the cross ribs 22 and 24 are two upset eyelets 32 and 34, which can be bored out in a latter processing step. It is also conceivable that, instead of the upset eyelets 32 and 34, eyelets can be produced directly by press forming. This would save a later machining step (for example, boring) that produces material debris.
(7) The cross ribs 26 to 30 can be joined to one another via a lengthwise rib 36, if this is required for reasons of structural mechanics, for example.
(8) The outer face 12, together with all corresponding contours, such as ribs and/or upset eyelets or eyelets, may be produced advantageously without any machining allowance during drop forging, so that any later machining of this outer face 12 is dispensed with.
(9) The blank 2 is than bent or rolled, so that the essentially cylindrical half-shell 40 depicted in