GB588655A - Improvements in or relating to exhaust-cooling devices for internal combustion engines - Google Patents
Improvements in or relating to exhaust-cooling devices for internal combustion enginesInfo
- Publication number
- GB588655A GB588655A GB32150/39A GB3215039A GB588655A GB 588655 A GB588655 A GB 588655A GB 32150/39 A GB32150/39 A GB 32150/39A GB 3215039 A GB3215039 A GB 3215039A GB 588655 A GB588655 A GB 588655A
- Authority
- GB
- United Kingdom
- Prior art keywords
- exhaust
- sheets
- internal combustion
- combustion engines
- curved
- 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
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P1/00—Air cooling
- F01P1/06—Arrangements for cooling other engine or machine parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2060/00—Cooling circuits using auxiliaries
- F01P2060/10—Fuel manifold
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P2060/00—Cooling circuits using auxiliaries
- F01P2060/16—Outlet manifold
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Abstract
588,655. Cooling exhaust gases. SOC. ANON DES APPAREILS G. A. L. Dec. 13, 1939, No. 32150. Convention date, March 30. [Class 7 (ii)] An exhaust cooling device for internal combustion engines of aircraft or vehicles comprises thin hollow blades or sheets 3, Figs. 1 and 2, with a freely open outlet edge 8, the sheets being curved to bring the exhaust stream into alignment with the air current at the outlet point whatever be the direction of the exhaust pipes 6 forming part of the manifold 5. The passages in the sheets are sub-divided by pressing together the walls of the sheet along lines 4, Fig. 2. The sheets may be either parallel or disposed radially to an axis adjacent-the flange 7. In the case of a twelve cylinder engine of V-form one exhaust cooling device is connected to the adjacent outlets of each pair of cylinders. In the application to a radial engine, Fig. 5 arranged behind the cowling 13 of an aeroplane having a fuselage 14, the sheets are curved so as to direct the exhaust in the direction f4 of the resultant of the external and internal air currents f1<1> and f3.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR588655X | 1939-03-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB588655A true GB588655A (en) | 1947-05-30 |
Family
ID=8962216
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32150/39A Expired GB588655A (en) | 1939-03-30 | 1939-12-13 | Improvements in or relating to exhaust-cooling devices for internal combustion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB588655A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2944392A (en) * | 1956-03-29 | 1960-07-12 | United Aircraft Corp | Hollow vane exhaust silencer effecting thrust generation |
US3930627A (en) * | 1973-10-03 | 1976-01-06 | Summa Corporation | Radiation shielding and gas diffusion apparatus |
-
1939
- 1939-12-13 GB GB32150/39A patent/GB588655A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2944392A (en) * | 1956-03-29 | 1960-07-12 | United Aircraft Corp | Hollow vane exhaust silencer effecting thrust generation |
US3930627A (en) * | 1973-10-03 | 1976-01-06 | Summa Corporation | Radiation shielding and gas diffusion apparatus |
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