IT1176673B - QUARRY SHOVEL FOR TURBOMACHINE - Google Patents
QUARRY SHOVEL FOR TURBOMACHINEInfo
- Publication number
- IT1176673B IT1176673B IT22562/84A IT2256284A IT1176673B IT 1176673 B IT1176673 B IT 1176673B IT 22562/84 A IT22562/84 A IT 22562/84A IT 2256284 A IT2256284 A IT 2256284A IT 1176673 B IT1176673 B IT 1176673B
- Authority
- IT
- Italy
- Prior art keywords
- quarry
- turbomachine
- shovel
- quarry shovel
- Prior art date
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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
-
- 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
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- 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)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US53519883A | 1983-09-23 | 1983-09-23 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| IT8422562A0 IT8422562A0 (en) | 1984-09-07 |
| IT8422562A1 IT8422562A1 (en) | 1986-03-07 |
| IT1176673B true IT1176673B (en) | 1987-08-18 |
Family
ID=24133260
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT22562/84A IT1176673B (en) | 1983-09-23 | 1984-09-07 | QUARRY SHOVEL FOR TURBOMACHINE |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JPS60138300A (en) |
| DE (1) | DE3434001A1 (en) |
| FR (1) | FR2552500A1 (en) |
| GB (1) | GB2147055A (en) |
| IT (1) | IT1176673B (en) |
Families Citing this family (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4041104C1 (en) * | 1990-12-21 | 1992-06-04 | Mtu Muenchen Gmbh | |
| US5129787A (en) * | 1991-02-13 | 1992-07-14 | United Technologies Corporation | Lightweight propulsor blade with internal spars and rigid base members |
| US5375978A (en) * | 1992-05-01 | 1994-12-27 | General Electric Company | Foreign object damage resistant composite blade and manufacture |
| FR2694900B1 (en) * | 1992-08-19 | 1994-10-21 | Hispano Suiza Sa | Method of manufacturing assemblies composed of two glued parts and comprising a forming step. |
| US6048174A (en) * | 1997-09-10 | 2000-04-11 | United Technologies Corporation | Impact resistant hollow airfoils |
| RU2145004C1 (en) * | 1998-09-16 | 2000-01-27 | Леженников Вячеслав Ефремович | Composite blade of axial-flow fan |
| JP4390026B2 (en) * | 1999-07-27 | 2009-12-24 | 株式会社Ihi | Composite wing |
| GB2365078B (en) | 2000-07-27 | 2004-04-21 | Rolls Royce Plc | A gas turbine engine blade |
| DE10307610A1 (en) | 2003-02-22 | 2004-09-02 | Rolls-Royce Deutschland Ltd & Co Kg | Compressor blade for an aircraft engine |
| GB0315975D0 (en) | 2003-07-09 | 2003-08-13 | Rolls Royce Plc | Guide vane |
| GB0717009D0 (en) * | 2007-09-01 | 2007-10-10 | Rolls Royce Plc | A component structure |
| GB0822909D0 (en) | 2008-12-17 | 2009-01-21 | Rolls Royce Plc | Airfoil |
| CN103089317B (en) * | 2011-10-31 | 2015-06-10 | 中航商用航空发动机有限责任公司 | Hollow fan blade and manufacturing method thereof |
| US9410437B2 (en) * | 2012-08-14 | 2016-08-09 | General Electric Company | Airfoil components containing ceramic-based materials and processes therefor |
| GB201500605D0 (en) * | 2015-01-15 | 2015-02-25 | Rolls Royce Plc | Fan blade |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3095180A (en) * | 1959-03-05 | 1963-06-25 | Stalker Corp | Blades for compressors, turbines and the like |
| GB1097456A (en) * | 1965-06-03 | 1968-01-03 | Rolls Royce | Composite material and a method of manufacturing the material |
| US3572971A (en) * | 1969-09-29 | 1971-03-30 | Gen Electric | Lightweight turbo-machinery blading |
| US3600103A (en) * | 1969-10-06 | 1971-08-17 | United Aircraft Corp | Composite blade |
| US3623204A (en) * | 1970-02-02 | 1971-11-30 | Gen Motors Corp | Method of fabricating hollow gas turbine blades |
| US3695778A (en) * | 1970-09-18 | 1972-10-03 | Trw Inc | Turbine blade |
| FR2157730A1 (en) * | 1971-10-29 | 1973-06-08 | Trw Inc | Composite air foils - produced from layers of tapes side-by-side encased in sheath and bonded |
| US3942231A (en) * | 1973-10-31 | 1976-03-09 | Trw Inc. | Contour formed metal matrix blade plies |
| US3927817A (en) * | 1974-10-03 | 1975-12-23 | Rockwell International Corp | Method for making metallic sandwich structures |
| US3981616A (en) * | 1974-10-22 | 1976-09-21 | The United States Of America As Represented By The Secretary Of The Air Force | Hollow composite compressor blade |
| GB2063747A (en) * | 1979-11-23 | 1981-06-10 | Gen Motors Corp | Method for manufacturing a clad turbine airfoil assembly |
| US4301584A (en) * | 1980-01-31 | 1981-11-24 | United Technologies Corporation | Method of forming fiber and metal matrix composite |
-
1984
- 1984-09-07 IT IT22562/84A patent/IT1176673B/en active
- 1984-09-15 DE DE19843434001 patent/DE3434001A1/en not_active Withdrawn
- 1984-09-19 GB GB08423715A patent/GB2147055A/en not_active Withdrawn
- 1984-09-20 FR FR8414450A patent/FR2552500A1/en not_active Withdrawn
- 1984-09-21 JP JP59196993A patent/JPS60138300A/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| JPS60138300A (en) | 1985-07-22 |
| IT8422562A1 (en) | 1986-03-07 |
| DE3434001A1 (en) | 1985-04-04 |
| IT8422562A0 (en) | 1984-09-07 |
| GB8423715D0 (en) | 1984-10-24 |
| FR2552500A1 (en) | 1985-03-29 |
| GB2147055A (en) | 1985-05-01 |
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