DE767546C
(de)
*
|
1938-09-12 |
1952-11-04 |
Bmw Flugmotorenbau G M B H |
Innengekuehlte Turbinenschaufel
|
US2563269A
(en)
*
|
1943-05-22 |
1951-08-07 |
Lockheed Aircraft Corp |
Gas turbine
|
DE969599C
(de)
*
|
1943-05-27 |
1958-06-19 |
Holzwarth Gasturbinen G M B H |
Gekuehlter Duesenkoerper fuer Kreiselmaschinen, insbesondere Abgasturbinen
|
FR963824A
(ja)
*
|
1943-11-19 |
1950-07-21 |
|
|
US2489683A
(en)
*
|
1943-11-19 |
1949-11-29 |
Edward A Stalker |
Turbine
|
BE462182A
(ja)
*
|
1944-12-22 |
1900-01-01 |
|
|
US2463340A
(en)
*
|
1945-02-22 |
1949-03-01 |
Wiberg Oscar Anton |
Axial flow turbine blade structure
|
US2506581A
(en)
*
|
1945-06-30 |
1950-05-09 |
Jr Albon C Cowles |
Means for cooling gas turbine blades
|
US2585871A
(en)
*
|
1945-10-22 |
1952-02-12 |
Edward A Stalker |
Turbine blade construction with provision for cooling
|
US2613910A
(en)
*
|
1947-01-24 |
1952-10-14 |
Edward A Stalker |
Slotted turbine blade
|
US2641439A
(en)
*
|
1947-10-01 |
1953-06-09 |
Chrysler Corp |
Cooled turbine or compressor blade
|
US2750147A
(en)
*
|
1947-10-28 |
1956-06-12 |
Power Jets Res & Dev Ltd |
Blading for turbines and like machines
|
US2613911A
(en)
*
|
1947-11-06 |
1952-10-14 |
Stalker Dev Company |
Fluid turning blade
|
US2641440A
(en)
*
|
1947-11-18 |
1953-06-09 |
Chrysler Corp |
Turbine blade with cooling means and carrier therefor
|
IT454293A
(ja)
*
|
1948-04-22 |
|
|
|
US2687278A
(en)
*
|
1948-05-26 |
1954-08-24 |
Chrysler Corp |
Article with passages
|
US2700530A
(en)
*
|
1948-08-27 |
1955-01-25 |
Chrysler Corp |
High temperature elastic fluid apparatus
|
US2625366A
(en)
*
|
1948-11-18 |
1953-01-13 |
Packard Motor Car Co |
Turbine rotor construction
|
US2858100A
(en)
*
|
1952-02-01 |
1958-10-28 |
Stalker Dev Company |
Blade structure for turbines and the like
|
US2807434A
(en)
*
|
1952-04-22 |
1957-09-24 |
Gen Motors Corp |
Turbine rotor assembly
|
US2873944A
(en)
*
|
1952-09-10 |
1959-02-17 |
Gen Motors Corp |
Turbine blade cooling
|
US2780435A
(en)
*
|
1953-01-12 |
1957-02-05 |
Jackson Thomas Woodrow |
Turbine blade cooling structure
|
DE1000733C2
(de)
*
|
1953-10-21 |
1957-06-19 |
Wilhelm Ludowici Dr Ing |
Wagenfoermiger Brennofen fuer Tonwaren
|
DE1024754B
(de)
*
|
1956-02-11 |
1958-02-20 |
Maschf Augsburg Nuernberg Ag |
Gekuehlte Laufschaufel fuer heiss betriebene Turbinen oder Verdichter
|
FR1177035A
(fr)
*
|
1957-05-28 |
1959-04-20 |
Snecma |
Procédé et dispositif de refroidissement d'organes de machines
|
US3112557A
(en)
*
|
1958-02-10 |
1963-12-03 |
Rolls Royce |
Turbine and compressor blades
|
US3435654A
(en)
*
|
1962-12-24 |
1969-04-01 |
Hermann Papst |
Boundary layer control
|
US4026659A
(en)
*
|
1975-10-16 |
1977-05-31 |
Avco Corporation |
Cooled composite vanes for turbine nozzles
|
US4770608A
(en)
*
|
1985-12-23 |
1988-09-13 |
United Technologies Corporation |
Film cooled vanes and turbines
|
US4738588A
(en)
*
|
1985-12-23 |
1988-04-19 |
Field Robert E |
Film cooling passages with step diffuser
|
US4672727A
(en)
*
|
1985-12-23 |
1987-06-16 |
United Technologies Corporation |
Method of fabricating film cooling slot in a hollow airfoil
|
US4705455A
(en)
*
|
1985-12-23 |
1987-11-10 |
United Technologies Corporation |
Convergent-divergent film coolant passage
|
US4664597A
(en)
*
|
1985-12-23 |
1987-05-12 |
United Technologies Corporation |
Coolant passages with full coverage film cooling slot
|
US4726735A
(en)
*
|
1985-12-23 |
1988-02-23 |
United Technologies Corporation |
Film cooling slot with metered flow
|
US4669957A
(en)
*
|
1985-12-23 |
1987-06-02 |
United Technologies Corporation |
Film coolant passage with swirl diffuser
|
US4653983A
(en)
*
|
1985-12-23 |
1987-03-31 |
United Technologies Corporation |
Cross-flow film cooling passages
|
US4676719A
(en)
*
|
1985-12-23 |
1987-06-30 |
United Technologies Corporation |
Film coolant passages for cast hollow airfoils
|
US4684323A
(en)
*
|
1985-12-23 |
1987-08-04 |
United Technologies Corporation |
Film cooling passages with curved corners
|
GB2202907A
(en)
*
|
1987-03-26 |
1988-10-05 |
Secr Defence |
Cooled aerofoil components
|
US4859147A
(en)
*
|
1988-01-25 |
1989-08-22 |
United Technologies Corporation |
Cooled gas turbine blade
|
US5097660A
(en)
*
|
1988-12-28 |
1992-03-24 |
Sundstrand Corporation |
Coanda effect turbine nozzle vane cooling
|
GB9821639D0
(en)
|
1998-10-06 |
1998-11-25 |
Rolls Royce Plc |
Coolant passages for gas turbine components
|
US6589600B1
(en)
*
|
1999-06-30 |
2003-07-08 |
General Electric Company |
Turbine engine component having enhanced heat transfer characteristics and method for forming same
|
US7357351B2
(en)
*
|
2002-07-18 |
2008-04-15 |
Eric T. Schmidt |
Linear shock wave absorber
|
US7798765B2
(en)
*
|
2007-04-12 |
2010-09-21 |
United Technologies Corporation |
Out-flow margin protection for a gas turbine engine
|
US8246297B2
(en)
|
2008-07-21 |
2012-08-21 |
Pratt & Whitney Canada Corp. |
Shroud segment cooling configuration
|
US11286783B2
(en)
*
|
2020-04-27 |
2022-03-29 |
Raytheon Technologies Corporation |
Airfoil with CMC liner and multi-piece monolithic ceramic shell
|