FR1136390A - Perfectionnements apportés aux rotors à ailettes pour machines à flux axial - Google Patents
Perfectionnements apportés aux rotors à ailettes pour machines à flux axialInfo
- Publication number
- FR1136390A FR1136390A FR1136390DA FR1136390A FR 1136390 A FR1136390 A FR 1136390A FR 1136390D A FR1136390D A FR 1136390DA FR 1136390 A FR1136390 A FR 1136390A
- Authority
- FR
- France
- Prior art keywords
- axial flow
- flow machines
- vane rotors
- rotors
- vane
- 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.)
- Expired
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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3053—Fixing blades to rotors; Blade roots ; Blade spacers by means of pins
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1482553A GB745073A (en) | 1953-05-27 | 1953-05-27 | Improvements in or relating to rotors for axial-flow compressors and like machines |
GB391459A GB815507A (en) | 1953-05-27 | 1954-10-01 | Improvements in or relating to bladed rotors for axial-flow fluid machines |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1136390A true FR1136390A (fr) | 1957-05-13 |
Family
ID=32395787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1136390D Expired FR1136390A (fr) | 1953-05-27 | 1955-09-19 | Perfectionnements apportés aux rotors à ailettes pour machines à flux axial |
Country Status (4)
Country | Link |
---|---|
US (1) | US2925997A (fr) |
BE (1) | BE541578A (fr) |
FR (1) | FR1136390A (fr) |
GB (1) | GB815506A (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2906496A (en) * | 1957-05-28 | 1959-09-29 | Ransom S Thompson | Retaining means for pin used for rotor blade attachment |
US3039739A (en) * | 1958-11-28 | 1962-06-19 | Gen Motors Corp | Pinned blade connecting means |
US3042369A (en) * | 1959-02-11 | 1962-07-03 | Gen Motors Corp | Pinned blade sealing means |
FR2637321A1 (fr) * | 1988-10-05 | 1990-04-06 | Snecma | Rotor de turbomachine muni d'un dispositif de fixation des aubes |
FR2660363A1 (fr) * | 1990-04-03 | 1991-10-04 | Gen Electric | Structure de fixation d'extremite interne d'aube de turbine. |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3043562A (en) * | 1961-04-10 | 1962-07-10 | Gen Electric | Combination sealing and restraining member for long-shank turbo-machine buckets |
BE635976A (fr) * | 1962-08-10 | |||
CH516731A (de) * | 1969-12-12 | 1971-12-15 | Bbc Sulzer Turbomaschinen | Schaufelkranz für Turbomaschinen |
US4119389A (en) * | 1977-01-17 | 1978-10-10 | General Motors Corporation | Radially removable turbine vanes |
FR2419389A1 (fr) * | 1978-03-08 | 1979-10-05 | Snecma | Perfectionnements aux flasques de rotors de turbomachines |
US4344740A (en) * | 1979-09-28 | 1982-08-17 | United Technologies Corporation | Rotor assembly |
US10767558B2 (en) * | 2018-03-07 | 2020-09-08 | Rolls-Royce North American Technologies Inc. | Adaptive-curvature inertial particle separators |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2537739A (en) * | 1946-10-26 | 1951-01-09 | Wright Aeronautical Corp | Fan blade mounting |
FR960069A (fr) * | 1947-04-02 | 1950-04-12 | ||
GB679714A (en) * | 1949-04-21 | 1952-09-24 | Rolls Royce | Improvements in or relating to axial-flow compressors and turbines |
GB667979A (en) * | 1949-07-28 | 1952-03-12 | Rolls Royce | Improvements in or relating to axial flow compressors and turbines |
-
0
- BE BE541578D patent/BE541578A/xx unknown
-
1954
- 1954-10-01 GB GB28411/54A patent/GB815506A/en not_active Expired
-
1955
- 1955-09-12 US US533782A patent/US2925997A/en not_active Expired - Lifetime
- 1955-09-19 FR FR1136390D patent/FR1136390A/fr not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2906496A (en) * | 1957-05-28 | 1959-09-29 | Ransom S Thompson | Retaining means for pin used for rotor blade attachment |
US3039739A (en) * | 1958-11-28 | 1962-06-19 | Gen Motors Corp | Pinned blade connecting means |
US3042369A (en) * | 1959-02-11 | 1962-07-03 | Gen Motors Corp | Pinned blade sealing means |
FR2637321A1 (fr) * | 1988-10-05 | 1990-04-06 | Snecma | Rotor de turbomachine muni d'un dispositif de fixation des aubes |
EP0363280A1 (fr) * | 1988-10-05 | 1990-04-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Rotor de turbomachine muni d'un dispositif de fixation des aubes |
US5007800A (en) * | 1988-10-05 | 1991-04-16 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." | Rotor blade fixing for turbomachine rotors |
FR2660363A1 (fr) * | 1990-04-03 | 1991-10-04 | Gen Electric | Structure de fixation d'extremite interne d'aube de turbine. |
Also Published As
Publication number | Publication date |
---|---|
US2925997A (en) | 1960-02-23 |
BE541578A (fr) | |
GB815506A (en) | 1959-06-24 |
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