GB456126A - Improvements in and relating to airscrews - Google Patents
Improvements in and relating to airscrewsInfo
- Publication number
- GB456126A GB456126A GB1633236A GB1633236A GB456126A GB 456126 A GB456126 A GB 456126A GB 1633236 A GB1633236 A GB 1633236A GB 1633236 A GB1633236 A GB 1633236A GB 456126 A GB456126 A GB 456126A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flange
- secured
- blade
- hub
- airscrew
- 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
- B64C11/02—Hub construction
- B64C11/04—Blade mountings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Road Paving Structures (AREA)
Abstract
456,126. Air-screws. CLIFFORD, E., 8, King's Road, Kingston-on-Thames, and AIRSCREW CO., Ltd., Weybridge, Surrey. June 11, 1936, No. 16332. [Class 114] In air-screws in which each blade root has an annular flange adapted to be secured to the hub, a clamping ring is provided which is secured by bolts parallel to the blade axis. The airscrew blade 1 has flange 2 which is held against the hub 3 by means of a sectional flange 6 secured by bolts 5. The flange is provided with projections or serrations 12 adapted to interlock with pins 10 on a metal bridge piece 11 secured under two adjacent nuts 8. The nuts 8 are tightened to give to the bolts 5 an initial tension slightly greater than the maximum centrifugal force obtained when the air-screw is running. Beneath the flange 2 is disposed a sleeve 13 for positioning the flange with respect to the hub, and this sleeve is formed with an eccentrically disposed outer edge so that by adjusting it the blade may be set when balancing the complete airscrew.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1633236A GB456126A (en) | 1936-06-11 | 1936-06-11 | Improvements in and relating to airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1633236A GB456126A (en) | 1936-06-11 | 1936-06-11 | Improvements in and relating to airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB456126A true GB456126A (en) | 1936-11-03 |
Family
ID=10075375
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1633236A Expired GB456126A (en) | 1936-06-11 | 1936-06-11 | Improvements in and relating to airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB456126A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4790722A (en) * | 1985-12-18 | 1988-12-13 | M A N Gutehoffnungshutte GmbH | Multi-blade rotor for a windmill-type apparatus |
GB2475008A (en) * | 2011-03-05 | 2011-05-04 | Michael Victor Rodrigues | Jet engine blade to disc joint |
-
1936
- 1936-06-11 GB GB1633236A patent/GB456126A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4790722A (en) * | 1985-12-18 | 1988-12-13 | M A N Gutehoffnungshutte GmbH | Multi-blade rotor for a windmill-type apparatus |
GB2475008A (en) * | 2011-03-05 | 2011-05-04 | Michael Victor Rodrigues | Jet engine blade to disc joint |
GB2475008B (en) * | 2011-03-05 | 2011-09-21 | Michael Victor Rodrigues | Turbofan jet engine fail-proof blade to disc joints |
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