GB460703A - A device for regulating the charging pressure of internal combustion engines for aircraft - Google Patents
A device for regulating the charging pressure of internal combustion engines for aircraftInfo
- Publication number
- GB460703A GB460703A GB28666/36A GB2866636A GB460703A GB 460703 A GB460703 A GB 460703A GB 28666/36 A GB28666/36 A GB 28666/36A GB 2866636 A GB2866636 A GB 2866636A GB 460703 A GB460703 A GB 460703A
- Authority
- GB
- United Kingdom
- Prior art keywords
- conduit
- valve
- regulating
- air
- aircraft
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B33/00—Engines characterised by provision of pumps for charging or scavenging
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M2700/00—Supplying, feeding or preparing air, fuel, fuel air mixtures or auxiliary fluids for a combustion engine; Use of exhaust gas; Compressors for piston engines
- F02M2700/33—Compressors for piston combustion engines
- F02M2700/331—Charging and scavenging compressors
- F02M2700/335—Control therefor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
460,703. Regulating. BRANDENBURGISCHE MOTORENWERKE GES. Oct. 21, 1936, No. 28666. Convention date, Oct. 23, 1935. [Class 7 (vi)] A multistage blower for charging aircraft engines is provided with a rotary valve 7 which may be adjusted counter - clockwise from the position shown in the Figure, in which the inlet of air from the valve 7 to the suction conduit of the fan 1 is cut off and air is supplied through a restricted opening to the conduit 5 leading to the second fan 2, so that as the valve is thus adjusted, the opening leading to the conduit 5 is increased until it is wide open, after which it begins to reduce again, and the inlet to the conduit 4 is gradually opened, until finally the conduit 5 is cut off from the interior of the valve, and the conduit 4 is fully open, in which all the air supplied passes through both fans and the full output is obtained.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE460703X | 1935-10-23 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB460703A true GB460703A (en) | 1937-02-02 |
Family
ID=6539773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB28666/36A Expired GB460703A (en) | 1935-10-23 | 1936-10-21 | A device for regulating the charging pressure of internal combustion engines for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB460703A (en) |
-
1936
- 1936-10-21 GB GB28666/36A patent/GB460703A/en not_active Expired
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