GB461846A - Improvements in or relating to the purification of the liquids used in aircraft provided with propellers - Google Patents
Improvements in or relating to the purification of the liquids used in aircraft provided with propellersInfo
- Publication number
- GB461846A GB461846A GB8775/36A GB877536A GB461846A GB 461846 A GB461846 A GB 461846A GB 8775/36 A GB8775/36 A GB 8775/36A GB 877536 A GB877536 A GB 877536A GB 461846 A GB461846 A GB 461846A
- Authority
- GB
- United Kingdom
- Prior art keywords
- liquid
- bores
- propeller
- march
- impurities
- 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
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M1/00—Pressure lubrication
- F01M1/10—Lubricating systems characterised by the provision therein of lubricant venting or purifying means, e.g. of filters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Centrifugal Separators (AREA)
Abstract
461,846. Centrifugal separators. VULLIERME, M. March 24, 1936, No. 8775. Convention date, March 25, 1935. [Class 23] [Also in Groups XXVI and XXXIII] A liquid used in an aircraft motor, for cooling or lubricating, is passed through passages in the propeller, for the centrifugal separation of impurities from it. The liquid passes through a pipe 1 in the propeller shaft, and then through one or more bores 4 through the length of the propeller. The return flow passes through tubes 5 inside the bores 4, to the tube 2<a> in the propeller shaft. The impurities are deposited in a space 9 normally closed by a frusto-conical plug 8 kept in position by a screw. The return tubes 5 have a number of spring blade valves 14 normally closing openings 10 in the pipes. If the supply pressure of the liquid is excessive the springs deflect and allow liquid to pass from the bores 4 to the interior of the pipes 5 without travelling to the space 9.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE461846X | 1935-03-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB461846A true GB461846A (en) | 1937-02-25 |
Family
ID=6539908
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8775/36A Expired GB461846A (en) | 1935-03-25 | 1936-03-24 | Improvements in or relating to the purification of the liquids used in aircraft provided with propellers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB461846A (en) |
-
1936
- 1936-03-24 GB GB8775/36A patent/GB461846A/en not_active Expired
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