FR1040697A - Perfectionnements aux rotors et notamment à ceux de compresseurs, turbines et moteurs à réaction - Google Patents
Perfectionnements aux rotors et notamment à ceux de compresseurs, turbines et moteurs à réactionInfo
- Publication number
- FR1040697A FR1040697A FR1040697DA FR1040697A FR 1040697 A FR1040697 A FR 1040697A FR 1040697D A FR1040697D A FR 1040697DA FR 1040697 A FR1040697 A FR 1040697A
- Authority
- FR
- France
- Prior art keywords
- compressors
- rotors
- turbines
- those
- jet engines
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/021—Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
-
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1040697T | 1951-04-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1040697A true FR1040697A (fr) | 1953-10-16 |
Family
ID=9589090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1040697D Expired FR1040697A (fr) | 1951-04-14 | 1951-04-14 | Perfectionnements aux rotors et notamment à ceux de compresseurs, turbines et moteurs à réaction |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR1040697A (fr) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3758232A (en) * | 1969-01-27 | 1973-09-11 | Secr Defence | Blade assembly for gas turbine engines |
US4011295A (en) * | 1974-10-07 | 1977-03-08 | The Garrett Corporation | Ceramic rotor for gas turbine engine |
US4826645A (en) * | 1984-07-07 | 1989-05-02 | Rolls-Royce Limited | Method of making an integral bladed member |
US4867644A (en) * | 1987-05-15 | 1989-09-19 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US4919594A (en) * | 1987-05-15 | 1990-04-24 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
FR2874232A1 (fr) * | 1998-07-28 | 2006-02-17 | Rolls Royce Plc Plc | Rotor metallique renforce de fibres. |
US7811062B1 (en) | 1997-06-03 | 2010-10-12 | Rolls-Royce Plc | Fiber reinforced metal rotor |
-
1951
- 1951-04-14 FR FR1040697D patent/FR1040697A/fr not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3758232A (en) * | 1969-01-27 | 1973-09-11 | Secr Defence | Blade assembly for gas turbine engines |
US4011295A (en) * | 1974-10-07 | 1977-03-08 | The Garrett Corporation | Ceramic rotor for gas turbine engine |
US4076456A (en) * | 1974-10-07 | 1978-02-28 | The Garrett Corporation | Ceramic rotor for gas turbine engine |
US4826645A (en) * | 1984-07-07 | 1989-05-02 | Rolls-Royce Limited | Method of making an integral bladed member |
US4867644A (en) * | 1987-05-15 | 1989-09-19 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US4919594A (en) * | 1987-05-15 | 1990-04-24 | Allied-Signal Inc. | Composite member, unitary rotor member including same, and method of making |
US7811062B1 (en) | 1997-06-03 | 2010-10-12 | Rolls-Royce Plc | Fiber reinforced metal rotor |
FR2874232A1 (fr) * | 1998-07-28 | 2006-02-17 | Rolls Royce Plc Plc | Rotor metallique renforce de fibres. |
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