NL6802034A - - Google Patents
Info
- Publication number
- NL6802034A NL6802034A NL6802034A NL6802034A NL6802034A NL 6802034 A NL6802034 A NL 6802034A NL 6802034 A NL6802034 A NL 6802034A NL 6802034 A NL6802034 A NL 6802034A NL 6802034 A NL6802034 A NL 6802034A
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
-
- 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
- F05D2240/00—Components
- F05D2240/60—Shafts
- F05D2240/63—Glands for admission or removal of fluids from shafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH50768A CH487337A (de) | 1968-01-10 | 1968-01-10 | Anordnung für den Durchtritt von Gas durch den Mantel eines hohlen Rotors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| NL6802034A true NL6802034A (US20060241273A1-20061026-C00009.png) | 1969-07-14 |
Family
ID=4188582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NL6802034A NL6802034A (US20060241273A1-20061026-C00009.png) | 1968-01-10 | 1968-02-13 |
Country Status (6)
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3614257A (en) * | 1969-07-19 | 1971-10-19 | Rolls Royce | Gas turbine engine |
| US3632221A (en) * | 1970-08-03 | 1972-01-04 | Gen Electric | Gas turbine engine cooling system incorporating a vortex shaft valve |
| US4008977A (en) * | 1975-09-19 | 1977-02-22 | United Technologies Corporation | Compressor bleed system |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3990812A (en) * | 1975-03-03 | 1976-11-09 | United Technologies Corporation | Radial inflow blade cooling system |
| DE2633291C3 (de) * | 1976-07-23 | 1981-05-14 | Kraftwerk Union AG, 4330 Mülheim | Gasturbinenanlage mit Kühlung durch zwei unabhängige Kühlluftströme |
| US4184797A (en) * | 1977-10-17 | 1980-01-22 | General Electric Company | Liquid-cooled turbine rotor |
| US4309147A (en) * | 1979-05-21 | 1982-01-05 | General Electric Company | Foreign particle separator |
| US4306834A (en) * | 1979-06-25 | 1981-12-22 | Westinghouse Electric Corp. | Balance piston and seal for gas turbine engine |
| DE3014279A1 (de) * | 1980-04-15 | 1981-10-22 | M.A.N. Maschinenfabrik Augsburg-Nürnberg AG, 4200 Oberhausen | Einrichtung zur kuehlung des inneren einer gasturbine |
| GB2075123B (en) * | 1980-05-01 | 1983-11-16 | Gen Electric | Turbine cooling air deswirler |
| FR2491549B1 (fr) * | 1980-10-08 | 1985-07-05 | Snecma | Dispositif de refroidissement d'une turbine a gaz, par prelevement d'air au niveau du compresseur |
| US4648241A (en) * | 1983-11-03 | 1987-03-10 | United Technologies Corporation | Active clearance control |
| US4674955A (en) * | 1984-12-21 | 1987-06-23 | The Garrett Corporation | Radial inboard preswirl system |
| DE3603350A1 (de) * | 1986-02-04 | 1987-08-06 | Walter Prof Dipl Ph Sibbertsen | Verfahren zur kuehlung thermisch belasteter bauelemente von stroemungsmaschinen, vorrichtung zur durchfuehrung des verfahrens sowie ausbildung thermisch belasteter schaufeln |
| FR2614654B1 (fr) * | 1987-04-29 | 1992-02-21 | Snecma | Disque de compresseur axial de turbomachine a prelevement d'air centripete |
| GB2253442B (en) * | 1991-03-02 | 1994-08-24 | Rolls Royce Plc | An axial flow turbine assembly |
| DE19617539B4 (de) * | 1996-05-02 | 2006-02-09 | Alstom | Rotor für eine thermische Turbomaschine |
| US5738488A (en) * | 1996-11-12 | 1998-04-14 | General Electric Co. | Gland for transferring cooling medium to the rotor of a gas turbine |
| US6053701A (en) * | 1997-01-23 | 2000-04-25 | Mitsubishi Heavy Industries, Ltd. | Gas turbine rotor for steam cooling |
| US6837676B2 (en) * | 2002-09-11 | 2005-01-04 | Mitsubishi Heavy Industries, Ltd. | Gas turbine |
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1968
- 1968-01-10 CH CH50768A patent/CH487337A/de not_active IP Right Cessation
- 1968-02-06 DE DE19681601664 patent/DE1601664B2/de active Pending
- 1968-02-13 NL NL6802034A patent/NL6802034A/xx unknown
- 1968-12-24 FR FR1597088D patent/FR1597088A/fr not_active Expired
-
1969
- 1969-01-10 GB GB157169A patent/GB1194663A/en not_active Expired
- 1969-01-10 BE BE726726D patent/BE726726A/xx unknown
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3614257A (en) * | 1969-07-19 | 1971-10-19 | Rolls Royce | Gas turbine engine |
| US3632221A (en) * | 1970-08-03 | 1972-01-04 | Gen Electric | Gas turbine engine cooling system incorporating a vortex shaft valve |
| US4008977A (en) * | 1975-09-19 | 1977-02-22 | United Technologies Corporation | Compressor bleed system |
Also Published As
| Publication number | Publication date |
|---|---|
| DE1601664B2 (de) | 1971-12-02 |
| BE726726A (US20060241273A1-20061026-C00009.png) | 1969-07-10 |
| GB1194663A (en) | 1970-06-10 |
| FR1597088A (US20060241273A1-20061026-C00009.png) | 1970-06-22 |
| DE1601664A1 (de) | 1970-08-06 |
| CH487337A (de) | 1970-03-15 |
