GB552745A - Improvements in, or relating to the balancing of blades of airscrews and the like - Google Patents
Improvements in, or relating to the balancing of blades of airscrews and the likeInfo
- Publication number
- GB552745A GB552745A GB1338941A GB1338941A GB552745A GB 552745 A GB552745 A GB 552745A GB 1338941 A GB1338941 A GB 1338941A GB 1338941 A GB1338941 A GB 1338941A GB 552745 A GB552745 A GB 552745A
- Authority
- GB
- United Kingdom
- Prior art keywords
- weights
- blade
- balance
- adjustment
- airscrews
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Earth Drilling (AREA)
- Transmission Devices (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
552,745. Balancing airscrews. DANIELS, A. O., GERMAN, H. V., and HORDERN-RICHMOND AIRCRAFT, Ltd. Oct. 17, 1941, No. 13389. [Class 114] Static vertical balance of an airscrew blade is obtained by the adjustment about the axis of the blade root of two equal balance weights. In one form, Figs. 3 and 4, two quadrant weights 22, 23 are angularly adjustable about the root of the blade 10 and clamped by a nut 13 threaded upon an axial tube 11 containing weights 24 for the adjustment of the horizontal balance. Serrations on the adjacent faces of the weights 22, 23 and a base plate 18 lock the weights against movement. If desired a third weight may be employed to partially balance the blade, the two weights 22, 23 being used for a final fine adjustment. Instead of the weights being in the same plane they may be in adjacent planes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1338941A GB552745A (en) | 1941-10-17 | 1941-10-17 | Improvements in, or relating to the balancing of blades of airscrews and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1338941A GB552745A (en) | 1941-10-17 | 1941-10-17 | Improvements in, or relating to the balancing of blades of airscrews and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB552745A true GB552745A (en) | 1943-04-22 |
Family
ID=10022070
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1338941A Expired GB552745A (en) | 1941-10-17 | 1941-10-17 | Improvements in, or relating to the balancing of blades of airscrews and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB552745A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5273398A (en) * | 1992-12-01 | 1993-12-28 | United Technologies Corporation | Rotor blade balance weight assembly |
-
1941
- 1941-10-17 GB GB1338941A patent/GB552745A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5273398A (en) * | 1992-12-01 | 1993-12-28 | United Technologies Corporation | Rotor blade balance weight assembly |
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