GB509285A - A device for starting internal combustion engines especially diesel aero-engines - Google Patents
A device for starting internal combustion engines especially diesel aero-enginesInfo
- Publication number
- GB509285A GB509285A GB30166/38A GB3016638A GB509285A GB 509285 A GB509285 A GB 509285A GB 30166/38 A GB30166/38 A GB 30166/38A GB 3016638 A GB3016638 A GB 3016638A GB 509285 A GB509285 A GB 509285A
- Authority
- GB
- United Kingdom
- Prior art keywords
- engine
- turbine
- engines
- starting
- aero
- 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
- F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
- F02N7/00—Starting apparatus having fluid-driven auxiliary engines or apparatus
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
509,285. Turning - gear; starting. MASCHINENFABRlK AUGSBURG-NURNBERG AKT.-GES. Oct. 18, 1938, No. 30166. Convention date, Oct. 21, 1937. [Class 7 (v)] An engine starter, particularly for diesel aero-engines, comprises a combustion turbine 1 adapted during normal running to drive a supercharger 8 or other engine auxiliary and being normally driven by exhaust gases from the engine; for starting purposes, the turbine is driven by gases from a combustion chamber 11 and is placed in driving connection with the engine through the medium of gearing 2, 3 or a fly-wheel or an air compressor for supplying air under pressure to the engine to cause its initial rotation. As shown, a valve 10 enables the turbine 1 to be put in communication either with the chamber 11 or the engine exhaust pipe. The gear 3 is provided with a disengageable clutch and may be formed as a fly-wheel. During the starting period, the cooling water, lubricating oil or fuel for the engine may be heated in a jacket 13 on the turbine 1 and also in a jacket on the chamber 11.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE509285X | 1937-10-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB509285A true GB509285A (en) | 1939-07-13 |
Family
ID=6547168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30166/38A Expired GB509285A (en) | 1937-10-21 | 1938-10-18 | A device for starting internal combustion engines especially diesel aero-engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB509285A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE747919C (en) * | 1940-04-09 | 1944-10-20 | Axial flow machine | |
US3427802A (en) * | 1966-08-31 | 1969-02-18 | Dresser Ind | Gas starting arrangement for two-cycle turbocharged engine |
US4470488A (en) * | 1983-04-06 | 1984-09-11 | Alphe Broussard | Carrying case for health program |
-
1938
- 1938-10-18 GB GB30166/38A patent/GB509285A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE747919C (en) * | 1940-04-09 | 1944-10-20 | Axial flow machine | |
US3427802A (en) * | 1966-08-31 | 1969-02-18 | Dresser Ind | Gas starting arrangement for two-cycle turbocharged engine |
US4470488A (en) * | 1983-04-06 | 1984-09-11 | Alphe Broussard | Carrying case for health program |
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