DE1098151B - Process for the manufacture of an impeller for turbomachinery composed of steel parts - Google Patents
Process for the manufacture of an impeller for turbomachinery composed of steel partsInfo
- Publication number
- DE1098151B DE1098151B DED28623A DED0028623A DE1098151B DE 1098151 B DE1098151 B DE 1098151B DE D28623 A DED28623 A DE D28623A DE D0028623 A DED0028623 A DE D0028623A DE 1098151 B DE1098151 B DE 1098151B
- Authority
- DE
- Germany
- Prior art keywords
- impeller
- turbomachinery
- manufacture
- steel parts
- welded
- Prior art date
- Legal status (The legal status 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 status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/048—Form or construction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Verfahren zum Herstellen eines aus Stahlteilen zusammengesetzten Laufrades für Turbomaschinen Die Erfindung betrifft ein Verfahren zum Herstellen eines aus Stahlteilen zusammengesetzten Laufrades für Turbomaschinen mit vorwiegend radialer Strömung, bei dem .die radialen, bis zur Nabe reichenden Schaufeln zwischen einer Rad- und einer Deckscheibe eingeschweißt sind.Method for manufacturing an impeller composed of steel parts for turbo machines The invention relates to a method for producing a Steel parts assembled impeller for turbomachinery with predominantly radial Flow, in which .the radial blades reaching up to the hub between a Wheel and a cover disk are welded.
Bisher war es üblich, die Laufradschaufeln besagter Turbomaschinen zuerst an der Radscheibe und anschließend an der Deckscheibe anzuschweißen, wobei, behindert durch einen engen Schaufelkanal, nur an dessen inneren und äußeren Teil ein Anschweißen möglich war. Es zeigte sich jedoch hierbei, daß auf diese Weise hergestellte Laufräder den heutzutage an sie gestellten hohen Beanspruchungen nicht gewachsen waren.Up to now it was common to use the impeller blades of said turbo machines to be welded first to the wheel disc and then to the cover disc, whereby, obstructed by a narrow blade channel, only on its inner and outer part welding was possible. It was found, however, that in this way manufactured impellers do not meet the high demands placed on them today had grown.
Um diesen Schwierigkeiten zu begegnen, wird erfindungsgemäß vorgeschlagen, sämtliche Schaufeln auf ihrer ganzen Länge zuerst an der Deckscheibe und in einem darauffolgenden Arbeitsgang an der Radscheibe anzuschweißen.In order to counter these difficulties, it is proposed according to the invention that all blades along their entire length first on the cover disk and in one the following work step to be welded to the wheel disc.
Bei der Anwendung dieses Verfahrens ist es nunmehr möglich, auch die am höchsten beanspruchte Stelle des Laufrades, nämlich die Verbindung der Schaufeln mit der Deckscheibe an der Übergangsstelle des axialen in den radialen Teil des Strömungskanals, einwandfrei herzustellen, so daß ein derartig zusammengeschweißtes Laufrad den neuzeitlichen Festigkeitsansprüchen in jeder Weise genügt. Im weiteren ist durch den Erfindungsvorschlag der Weg geebnet zum Bau größter Einheiten von geschweißten Laufrädern für Turbomaschinen.When using this method, it is now possible to also use the the most stressed point on the impeller, namely the connection between the blades with the cover plate at the transition point from the axial to the radial part of the Flow channel to produce properly, so that such a welded together Impeller satisfies modern strength requirements in every way. In the further the inventive proposal paved the way for the construction of the largest units of welded impellers for turbo machines.
Claims (1)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED28623A DE1098151B (en) | 1958-07-28 | 1958-07-28 | Process for the manufacture of an impeller for turbomachinery composed of steel parts |
CH7539459A CH368262A (en) | 1958-07-28 | 1959-07-06 | Process for the manufacture of a steel impeller for turbo machines and an impeller manufactured according to this process |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DED28623A DE1098151B (en) | 1958-07-28 | 1958-07-28 | Process for the manufacture of an impeller for turbomachinery composed of steel parts |
Publications (1)
Publication Number | Publication Date |
---|---|
DE1098151B true DE1098151B (en) | 1961-01-26 |
Family
ID=7039753
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DED28623A Pending DE1098151B (en) | 1958-07-28 | 1958-07-28 | Process for the manufacture of an impeller for turbomachinery composed of steel parts |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH368262A (en) |
DE (1) | DE1098151B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0283825A1 (en) * | 1987-03-23 | 1988-09-28 | Philipp Hilge GmbH | Turbo machine rotor |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE906975C (en) * | 1950-05-03 | 1954-03-18 | Licentia Gmbh | Impeller for radial turbo compressors |
-
1958
- 1958-07-28 DE DED28623A patent/DE1098151B/en active Pending
-
1959
- 1959-07-06 CH CH7539459A patent/CH368262A/en unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE906975C (en) * | 1950-05-03 | 1954-03-18 | Licentia Gmbh | Impeller for radial turbo compressors |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0283825A1 (en) * | 1987-03-23 | 1988-09-28 | Philipp Hilge GmbH | Turbo machine rotor |
Also Published As
Publication number | Publication date |
---|---|
CH368262A (en) | 1963-03-31 |
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