EP2900930A4 - Überkühlter ganzheitlich beschaufelter rotor aus mehreren legierungen - Google Patents
Überkühlter ganzheitlich beschaufelter rotor aus mehreren legierungenInfo
- Publication number
- EP2900930A4 EP2900930A4 EP13841587.2A EP13841587A EP2900930A4 EP 2900930 A4 EP2900930 A4 EP 2900930A4 EP 13841587 A EP13841587 A EP 13841587A EP 2900930 A4 EP2900930 A4 EP 2900930A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- uber
- bladed rotor
- integrally bladed
- cooled multi
- alloy integrally
- 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.)
- Withdrawn
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
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- 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
- F01D5/34—Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
-
- 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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/40—Heat treatment
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/630,120 US20140140859A1 (en) | 2012-09-28 | 2012-09-28 | Uber-cooled multi-alloy integrally bladed rotor |
PCT/US2013/061427 WO2014052320A1 (en) | 2012-09-28 | 2013-09-24 | Uber-cooled multi-alloy integrally bladed rotor |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2900930A1 EP2900930A1 (de) | 2015-08-05 |
EP2900930A4 true EP2900930A4 (de) | 2016-05-18 |
Family
ID=50388908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13841587.2A Withdrawn EP2900930A4 (de) | 2012-09-28 | 2013-09-24 | Überkühlter ganzheitlich beschaufelter rotor aus mehreren legierungen |
Country Status (3)
Country | Link |
---|---|
US (1) | US20140140859A1 (de) |
EP (1) | EP2900930A4 (de) |
WO (1) | WO2014052320A1 (de) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20150003997A1 (en) * | 2013-07-01 | 2015-01-01 | United Technologies Corporation | Method of forming hybrid metal ceramic components |
US10344597B2 (en) * | 2015-08-17 | 2019-07-09 | United Technologies Corporation | Cupped contour for gas turbine engine blade assembly |
US10239157B2 (en) | 2016-04-06 | 2019-03-26 | General Electric Company | Additive machine utilizing rotational build surface |
US9988721B2 (en) * | 2016-06-28 | 2018-06-05 | Delavan, Inc. | Additive manufacturing processing with oxidation |
GB2553146A (en) * | 2016-08-26 | 2018-02-28 | Rolls Royce Plc | A friction welding process |
GB201701236D0 (en) * | 2017-01-25 | 2017-03-08 | Rolls Royce Plc | Bladed disc and method of manufacturing the same |
GB2560001B (en) * | 2017-02-24 | 2019-07-17 | Rolls Royce Plc | A weld stub arrangement and a method of using the arrangement to make an article |
US20180371924A1 (en) * | 2017-06-27 | 2018-12-27 | Florida Turbine Technologies, Inc. | Additively Manufactured Blisk with Optimized Microstructure for Small Turbine Engines |
US10954804B2 (en) * | 2017-07-05 | 2021-03-23 | Raytheon Technologies Corporation | Rotary machines including a hybrid rotor with hollow and solid rotor blade sets |
US10935037B2 (en) | 2018-01-05 | 2021-03-02 | Raytheon Technologies Corporation | Tool for simultaneous local stress relief of each of a multiple of linear friction welds of a rotor forging |
US10633731B2 (en) * | 2018-01-05 | 2020-04-28 | United Technologies Corporation | Method for producing enhanced fatigue and tensile properties in integrally bladed rotor forgings |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4784573A (en) * | 1987-08-17 | 1988-11-15 | United Technologies Corporation | Turbine blade attachment |
US4864706A (en) * | 1987-08-12 | 1989-09-12 | United Technologies Corporation | Fabrication of dual alloy integrally bladed rotors |
US5113583A (en) * | 1990-09-14 | 1992-05-19 | United Technologies Corporation | Integrally bladed rotor fabrication |
US6283714B1 (en) * | 1999-08-11 | 2001-09-04 | General Electric Company | Protection of internal and external surfaces of gas turbine airfoils |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4529452A (en) * | 1984-07-30 | 1985-07-16 | United Technologies Corporation | Process for fabricating multi-alloy components |
US20090239061A1 (en) * | 2006-11-08 | 2009-09-24 | General Electric Corporation | Ceramic corrosion resistant coating for oxidation resistance |
US8383028B2 (en) * | 2008-11-13 | 2013-02-26 | The Boeing Company | Method of manufacturing co-molded inserts |
US8251660B1 (en) * | 2009-10-26 | 2012-08-28 | Florida Turbine Technologies, Inc. | Turbine airfoil with near wall vortex cooling |
GB201010929D0 (en) * | 2010-06-30 | 2010-08-11 | Rolls Royce Plc | A turbine rotor assembly |
US9410436B2 (en) * | 2010-12-08 | 2016-08-09 | Pratt & Whitney Canada Corp. | Blade disk arrangement for blade frequency tuning |
-
2012
- 2012-09-28 US US13/630,120 patent/US20140140859A1/en not_active Abandoned
-
2013
- 2013-09-24 WO PCT/US2013/061427 patent/WO2014052320A1/en active Application Filing
- 2013-09-24 EP EP13841587.2A patent/EP2900930A4/de not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4864706A (en) * | 1987-08-12 | 1989-09-12 | United Technologies Corporation | Fabrication of dual alloy integrally bladed rotors |
US4784573A (en) * | 1987-08-17 | 1988-11-15 | United Technologies Corporation | Turbine blade attachment |
US5113583A (en) * | 1990-09-14 | 1992-05-19 | United Technologies Corporation | Integrally bladed rotor fabrication |
US6283714B1 (en) * | 1999-08-11 | 2001-09-04 | General Electric Company | Protection of internal and external surfaces of gas turbine airfoils |
Non-Patent Citations (1)
Title |
---|
See also references of WO2014052320A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO2014052320A1 (en) | 2014-04-03 |
EP2900930A1 (de) | 2015-08-05 |
US20140140859A1 (en) | 2014-05-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20150428 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAX | Request for extension of the european patent (deleted) | ||
RA4 | Supplementary search report drawn up and despatched (corrected) |
Effective date: 20160420 |
|
RIC1 | Information provided on ipc code assigned before grant |
Ipc: F02C 7/00 20060101ALI20160414BHEP Ipc: F01D 5/18 20060101ALI20160414BHEP Ipc: F01D 5/28 20060101ALI20160414BHEP Ipc: F01D 5/34 20060101ALI20160414BHEP Ipc: F01D 5/30 20060101AFI20160414BHEP |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: UNITED TECHNOLOGIES CORPORATION |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20161122 |