GB347964A - Improvements in and relating to vibration damping devices particularly for turbines, propellers and the like - Google Patents
Improvements in and relating to vibration damping devices particularly for turbines, propellers and the likeInfo
- Publication number
- GB347964A GB347964A GB20332/30A GB2033230A GB347964A GB 347964 A GB347964 A GB 347964A GB 20332/30 A GB20332/30 A GB 20332/30A GB 2033230 A GB2033230 A GB 2033230A GB 347964 A GB347964 A GB 347964A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- rod
- propellers
- turbines
- relating
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/008—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft characterised by vibration absorbing or balancing means
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
347,964. Turbine blades. BRITISH THOMSON-HOUSTON CO., Ltd., Crown House, Aldwych, London.-(Assignees of Kimball, A. L. ; 1546, Wendell Avenue, Schenectady, New York, U.S.A.) July 4, 1930, No. 20332. Convention date, July 5, 1929. [Class 110 (iii).] A device for damping lateral vibrations of turbine blades comprises a rod 8, which has a natural frequency of vibration higher than that of the turbine blade 5, and which is rigidly fixed by the part 9 to the base of the blade. The rod extends into a hole 6 bored in the blade and is surrounded by a fluid. The rod 8 may be tapered and may have the end in the form of a cup 11. Fig. 4 shows the rod fixed by a base 23 in a hole 6 bored out of a propeller blade 12.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US347964XA | 1929-07-05 | 1929-07-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB347964A true GB347964A (en) | 1931-05-07 |
Family
ID=21878656
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20332/30A Expired GB347964A (en) | 1929-07-05 | 1930-07-04 | Improvements in and relating to vibration damping devices particularly for turbines, propellers and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB347964A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2440815A1 (en) * | 1978-07-12 | 1980-06-06 | Fagersta Ab | HOLLOW METAL OBJECT, DAMPED AGAINST NOISE |
US5415524A (en) * | 1993-06-01 | 1995-05-16 | Gamble; Christopher L. | Fluid propulsion device |
US5558497A (en) * | 1995-07-31 | 1996-09-24 | United Technologies Corporation | Airfoil vibration damping device |
GB2305220A (en) * | 1981-07-02 | 1997-04-02 | Secr Defence | Ships propeller dampers |
US5820343A (en) * | 1995-07-31 | 1998-10-13 | United Technologies Corporation | Airfoil vibration damping device |
US6283707B1 (en) | 1999-03-19 | 2001-09-04 | Rolls-Royce Plc | Aerofoil blade damper |
EP1602801A1 (en) * | 2004-05-27 | 2005-12-07 | United Technologies Corporation | Rotor blade with a stick damper |
US20130039765A1 (en) * | 2011-08-12 | 2013-02-14 | Hamilton Sundstrand Corporation | Aircraft propellers |
-
1930
- 1930-07-04 GB GB20332/30A patent/GB347964A/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2440815A1 (en) * | 1978-07-12 | 1980-06-06 | Fagersta Ab | HOLLOW METAL OBJECT, DAMPED AGAINST NOISE |
GB2305220A (en) * | 1981-07-02 | 1997-04-02 | Secr Defence | Ships propeller dampers |
GB2305220B (en) * | 1981-07-02 | 1998-01-07 | Secr Defence | Propeller dampers |
US5415524A (en) * | 1993-06-01 | 1995-05-16 | Gamble; Christopher L. | Fluid propulsion device |
US5558497A (en) * | 1995-07-31 | 1996-09-24 | United Technologies Corporation | Airfoil vibration damping device |
US5820343A (en) * | 1995-07-31 | 1998-10-13 | United Technologies Corporation | Airfoil vibration damping device |
US6283707B1 (en) | 1999-03-19 | 2001-09-04 | Rolls-Royce Plc | Aerofoil blade damper |
EP1602801A1 (en) * | 2004-05-27 | 2005-12-07 | United Technologies Corporation | Rotor blade with a stick damper |
US7217093B2 (en) | 2004-05-27 | 2007-05-15 | United Technologies Corporation | Rotor blade with a stick damper |
US20130039765A1 (en) * | 2011-08-12 | 2013-02-14 | Hamilton Sundstrand Corporation | Aircraft propellers |
US8882464B2 (en) * | 2011-08-12 | 2014-11-11 | Hamilton Sundstrand Corporation | Aircraft propellers |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB534193A (en) | Improvements in and relating to elastic fluid turbine buckets | |
GB347964A (en) | Improvements in and relating to vibration damping devices particularly for turbines, propellers and the like | |
GB346480A (en) | Improvements in the mounting of blades in steam or gas turbines | |
GB400957A (en) | Improvements in and relating to rotating bodies subject to pulsating torque | |
GB909004A (en) | Improvements in or relating to propeller blades | |
GB535980A (en) | Improvements in and relating to turbine blades | |
GB523038A (en) | Hollow blade for exhaust gas turbine rotors | |
GB561897A (en) | Improvements in or relating to vibration damping means for turbine blades | |
GB732622A (en) | Oscillation dampers for the blades of steam and gas turbines, axial flow compressors and similar machines | |
GB359349A (en) | Method of producing a hollow blade for steam and gas turbines | |
GB235171A (en) | Improvements in or relating to packing means in steam, gas or other turbines | |
GB574770A (en) | Improvements relating to the blades of turbines and other machines | |
GB355028A (en) | Rotor blade for explosion turbines | |
GB476222A (en) | Guiding means for turbo-machines | |
SU44376A1 (en) | The method of excitation of mechanical vibrations of turbine blades | |
GB721049A (en) | Improvements in turbine and dynamic compressor blades | |
GB572058A (en) | Improvements in and relating to bladed bodies | |
GB271102A (en) | Improvements in and relating to elastic fluid turbines | |
GB479020A (en) | Improvements in and relating to vibration damping devices | |
GB384976A (en) | Improvements in centrifugal governors | |
GB319211A (en) | Improvements in and relating to methods of and means for balancing rotors | |
SU55545A1 (en) | The method of mounting the blades in the groove of the steam turbine rotor | |
GB231898A (en) | ||
GB534382A (en) | Improvements in and relating to elastic fluid turbine casings | |
GB340706A (en) | Blade ring for radial flow gas or steam turbines and method for producing such blade rings |