GB745073A - Improvements in or relating to rotors for axial-flow compressors and like machines - Google Patents
Improvements in or relating to rotors for axial-flow compressors and like machinesInfo
- Publication number
- GB745073A GB745073A GB1482553A GB1482553A GB745073A GB 745073 A GB745073 A GB 745073A GB 1482553 A GB1482553 A GB 1482553A GB 1482553 A GB1482553 A GB 1482553A GB 745073 A GB745073 A GB 745073A
- Authority
- GB
- United Kingdom
- Prior art keywords
- axial
- engages
- pivot
- annular
- plate member
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
745,073. Axial-flow compressors. ROLLSROYCE, Ltd. May 17, 1954 [May 27, 1953], No. 14825/53. Class 110(3) In a rotor for an axial-flow compressor in which the rotor blades are pivotally mounted on the periphery of a disc or drum, a pivot pin for a blade is restrained against displacement axially of itself by a plate member which engages a circumferentially-extending groove on the pivot pin, means being provided to locate the plate member against displacement relative to the disc or drum. A multi-stage axial-flow compressor rotor comprises a number of discs 10, mounted on a common shaft and spaced apart by for instance, flanges 21. The rotor blades 12 are pivoted 'at their roots 14 between annular flanges 11a, 11b by means of pivot pins 15. Plate - members 16 have semi-circular notches 18 which engage annular grooves 17 on the pivot pins 15; each member 16 co-operates with, say, five or, as shown, three pivot 'pins 15. Each plate member 16 engages 'at its outer periphery in a channel 22 and is restrained against circumferential displacement by the engagement of bent lugs 23 with notches formed in an annular rib 25, and against radial displacement by a springy tongue 24 of less thickness than the remainder of the member 16 and having a rib 27 which engages in an annular channel 26.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE541578D BE541578A (en) | 1953-05-27 | ||
GB1482553A GB745073A (en) | 1953-05-27 | 1953-05-27 | Improvements in or relating to rotors for axial-flow compressors and like machines |
GB28411/54A GB815506A (en) | 1953-05-27 | 1954-10-01 | Improvements in or relating to bladed rotors for axial-flow fluid machines |
GB391459A GB815507A (en) | 1953-05-27 | 1954-10-01 | Improvements in or relating to bladed rotors for axial-flow fluid machines |
US533782A US2925997A (en) | 1953-05-27 | 1955-09-12 | Rotors for axial-flow fluid machines with pivoted blades and blade pivot retaining means |
FR1136390D FR1136390A (en) | 1953-05-27 | 1955-09-19 | Improvements in vane rotors for axial flow machines |
Applications Claiming Priority (1)
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 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB745073A true GB745073A (en) | 1956-02-22 |
Family
ID=10048142
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1482553A Expired GB745073A (en) | 1953-05-27 | 1953-05-27 | Improvements in or relating to rotors for axial-flow compressors and like machines |
GB391459A Expired GB815507A (en) | 1953-05-27 | 1954-10-01 | Improvements in or relating to bladed rotors for axial-flow fluid machines |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB391459A Expired GB815507A (en) | 1953-05-27 | 1954-10-01 | Improvements in or relating to bladed rotors for axial-flow fluid machines |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB745073A (en) |
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 (en) * | 1988-10-05 | 1990-04-06 | Snecma | TURBOMACHINE ROTOR PROVIDED WITH A BLADE FIXING DEVICE |
US5435693A (en) * | 1994-02-18 | 1995-07-25 | Solar Turbines Incorporated | Pin and roller attachment system for ceramic blades |
US5993160A (en) * | 1997-12-11 | 1999-11-30 | Pratt & Whitney Canada Inc. | Cover plate for gas turbine rotor |
WO2010023205A1 (en) * | 2008-08-26 | 2010-03-04 | Snecma | Fixed vane assembly for a turbine engine with a reduced weight, and a turbine engine including at least one such fixed vane assembly |
-
1953
- 1953-05-27 GB GB1482553A patent/GB745073A/en not_active Expired
-
1954
- 1954-10-01 GB GB391459A patent/GB815507A/en not_active Expired
Cited By (14)
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 (en) * | 1988-10-05 | 1990-04-06 | Snecma | TURBOMACHINE ROTOR PROVIDED WITH A BLADE FIXING DEVICE |
EP0363280A1 (en) * | 1988-10-05 | 1990-04-11 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" | Turbo machinery rotor with means for blade fixation |
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 |
US5435693A (en) * | 1994-02-18 | 1995-07-25 | Solar Turbines Incorporated | Pin and roller attachment system for ceramic blades |
US5993160A (en) * | 1997-12-11 | 1999-11-30 | Pratt & Whitney Canada Inc. | Cover plate for gas turbine rotor |
WO2010023205A1 (en) * | 2008-08-26 | 2010-03-04 | Snecma | Fixed vane assembly for a turbine engine with a reduced weight, and a turbine engine including at least one such fixed vane assembly |
FR2935428A1 (en) * | 2008-08-26 | 2010-03-05 | Snecma | FIXED BLADE OF TURBOMACHINE WITH REDUCED MASS AND TURBOMACHINE COMPRISING AT LEAST ONE SUCH FIXED AUBAGE |
CN102132011A (en) * | 2008-08-26 | 2011-07-20 | 斯奈克玛 | Fixed vane assembly for turbine engine with reduced weight, and a turbine engine including at least one such fixed vane assembly |
JP2012500937A (en) * | 2008-08-26 | 2012-01-12 | スネクマ | Reduced weight turbine engine stationary blade assembly and turbine engine including at least one such stationary blade assembly |
US8757966B2 (en) | 2008-08-26 | 2014-06-24 | Snecma | Stationary vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such stationary vane assembly |
CN102132011B (en) * | 2008-08-26 | 2014-11-05 | 斯奈克玛 | Fixed vane assembly for turbine engine with reduced weight, and a turbine engine including at least one such fixed vane assembly |
Also Published As
Publication number | Publication date |
---|---|
GB815507A (en) | 1959-06-24 |
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