NL7012615A - - Google Patents
Info
- Publication number
- NL7012615A NL7012615A NL7012615A NL7012615A NL7012615A NL 7012615 A NL7012615 A NL 7012615A NL 7012615 A NL7012615 A NL 7012615A NL 7012615 A NL7012615 A NL 7012615A NL 7012615 A NL7012615 A NL 7012615A
- Authority
- NL
- Netherlands
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
-
- 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)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Laminated Bodies (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US86197569A | 1969-09-29 | 1969-09-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL7012615A true NL7012615A (https=) | 1971-03-31 |
Family
ID=25337270
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL7012615A NL7012615A (https=) | 1969-09-29 | 1970-08-26 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US3572971A (https=) |
| BE (1) | BE753304R (https=) |
| CH (1) | CH512006A (https=) |
| DE (1) | DE2047361A1 (https=) |
| FR (1) | FR2060555A6 (https=) |
| GB (1) | GB1270348A (https=) |
| NL (1) | NL7012615A (https=) |
Families Citing this family (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1375541A (https=) * | 1970-07-29 | 1974-11-27 | ||
| US3699623A (en) * | 1970-10-20 | 1972-10-24 | United Aircraft Corp | Method for fabricating corrosion resistant composites |
| US3827118A (en) * | 1970-11-27 | 1974-08-06 | Garrett Corp | Airfoil and method of forming the same |
| US3679324A (en) * | 1970-12-04 | 1972-07-25 | United Aircraft Corp | Filament reinforced gas turbine blade |
| US3717419A (en) * | 1971-07-09 | 1973-02-20 | Susquehanna Corp | Turbine blade |
| US4108572A (en) * | 1976-12-23 | 1978-08-22 | United Technologies Corporation | Composite rotor blade |
| US4111606A (en) * | 1976-12-27 | 1978-09-05 | United Technologies Corporation | Composite rotor blade |
| IT1176673B (it) * | 1983-09-23 | 1987-08-18 | Gen Electric | Pala cava per turbomacchina |
| US4815940A (en) * | 1986-08-04 | 1989-03-28 | United Technologies Corporation | Fatigue strengthened composite article |
| FR2625528B1 (fr) * | 1987-12-31 | 1993-06-04 | Plastiremo | Aube monobloc composite fibre-resine pour turbomachine et procede pour sa fabrication |
| US5137426A (en) * | 1990-08-06 | 1992-08-11 | General Electric Company | Blade shroud deformable protective coating |
| US5449273A (en) * | 1994-03-21 | 1995-09-12 | United Technologies Corporation | Composite airfoil leading edge protection |
| US5486096A (en) * | 1994-06-30 | 1996-01-23 | United Technologies Corporation | Erosion resistant surface protection |
| GB2293631B (en) * | 1994-09-30 | 1998-09-09 | Gen Electric | Composite fan blade trailing edge reinforcement |
| JP4060981B2 (ja) * | 1998-04-08 | 2008-03-12 | 本田技研工業株式会社 | ガスタービンの静翼構造体及びそのユニット |
| US6190133B1 (en) * | 1998-08-14 | 2001-02-20 | Allison Engine Company | High stiffness airoil and method of manufacture |
| EP1828545A2 (en) * | 2004-12-01 | 2007-09-05 | United Technologies Corporation | Annular turbine ring rotor |
| DK176541B1 (da) * | 2005-09-30 | 2008-07-28 | Lm Glasfiber As | Laminat eller en sandwich-konstruktion med formbart kernemateriale |
| DE102006061915A1 (de) * | 2006-12-21 | 2008-07-03 | Rolls-Royce Deutschland Ltd & Co Kg | Hybrid-Fanschaufel und Verfahren zu deren Herstellung |
| US7753653B2 (en) * | 2007-01-12 | 2010-07-13 | General Electric Company | Composite inlet guide vane |
| DE102008052380B4 (de) * | 2008-10-20 | 2012-09-20 | Siemens Aktiengesellschaft | Turbinenschaufelblatt und Turbinenschaufel für eine Turbine sowie Verfahren zur direkten Bestimmung des Erosionsfortschritts eines Turbinenschaufelblattes |
| US8186961B2 (en) | 2009-01-23 | 2012-05-29 | Pratt & Whitney Canada Corp. | Blade preloading system |
| US8387504B2 (en) | 2011-01-06 | 2013-03-05 | General Electric Company | Fiber-reinforced Al-Li compressor airfoil and method of fabricating |
| FR2983519B1 (fr) * | 2011-12-01 | 2015-07-24 | Snecma Propulsion Solide | Aube de turbine a pale creuse en materiau composite, turbine ou compresseur ayant un distributeur ou redresseur forme de telles aubes et turbomachine les comprenant |
| EP2904250A4 (en) * | 2012-10-01 | 2015-10-21 | United Technologies Corp | HIGH POWER TRANSMISSION POWER DENSITY OF A DOUBLE-FLOW GEAR TURBOFACTOR |
| US20150041059A1 (en) * | 2013-03-18 | 2015-02-12 | Rohr, Inc. | Inner fixed structure with attached corner fitting |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB722341A (en) * | 1952-03-19 | 1955-01-26 | Rolls Royce | Improvements relating to turbine blades |
| US2920868A (en) * | 1955-10-05 | 1960-01-12 | Westinghouse Electric Corp | Dampened blade structure |
| US3132841A (en) * | 1958-05-12 | 1964-05-12 | Gen Motors Corp | Compressor blade and manufacture thereof |
| US2929755A (en) * | 1958-07-24 | 1960-03-22 | Orenda Engines Ltd | Plastic blades for gas turbine engines |
| US3032317A (en) * | 1958-10-24 | 1962-05-01 | Robert G Frank | Jet turbine bucket wheel |
| GB901075A (en) * | 1960-05-12 | 1962-07-11 | Rolls Royce | Improvements relating to compressor blades |
-
1969
- 1969-09-29 US US861975A patent/US3572971A/en not_active Expired - Lifetime
-
1970
- 1970-07-02 GB GB32207/70A patent/GB1270348A/en not_active Expired
- 1970-07-07 CH CH1028170A patent/CH512006A/de not_active IP Right Cessation
- 1970-07-10 BE BE753304D patent/BE753304R/xx active
- 1970-07-20 FR FR7026702A patent/FR2060555A6/fr not_active Expired
- 1970-08-26 NL NL7012615A patent/NL7012615A/xx unknown
- 1970-09-25 DE DE19702047361 patent/DE2047361A1/de active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| BE753304R (fr) | 1970-12-16 |
| GB1270348A (en) | 1972-04-12 |
| FR2060555A6 (https=) | 1971-06-18 |
| US3572971A (en) | 1971-03-30 |
| CH512006A (de) | 1971-08-31 |
| DE2047361A1 (de) | 1971-04-08 |