GB531864A - Improvements in and relating to the utilisation of the exhaust gases of internal combustion aircraft engines - Google Patents
Improvements in and relating to the utilisation of the exhaust gases of internal combustion aircraft enginesInfo
- Publication number
- GB531864A GB531864A GB22662/39A GB2266239A GB531864A GB 531864 A GB531864 A GB 531864A GB 22662/39 A GB22662/39 A GB 22662/39A GB 2266239 A GB2266239 A GB 2266239A GB 531864 A GB531864 A GB 531864A
- Authority
- GB
- United Kingdom
- Prior art keywords
- exhaust
- fairing
- exhaust gases
- gases
- utilisation
- 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
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
Abstract
531,864. Utilizing aircraft exhaust gases. JUNKERS FLUGZEUG-UND-MOTORENWERKE AKT.-GES. Aug. 4, 1939, No. 22662. Convention date, Sept. 2, 1938. [Class 4] In the utilization of exhaust gases of internalcombustion engines for propulsion purposes, the exhaust pipes 3 of the cylinders are grouped into sheaves or bunches and are so arranged that their exhaust nozzles 3b lie in a plane approximately transverse to the direction of outflow of the gases. The exhaust pipes may be covered with a fairing 4 provided with a fresh air inlet 5 and extended at 7 behind the nozzles to conceal the flames issuing therefrom. In some cases, a partition 14 is arranged between the fairing and the engine for directing heated air into a conduit 8 for heating purposes, the exhaust flames being quenched by air entering through inlets 9 in a fairing 10.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE531864X | 1938-09-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB531864A true GB531864A (en) | 1941-01-13 |
Family
ID=6555171
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB22662/39A Expired GB531864A (en) | 1938-09-02 | 1939-08-04 | Improvements in and relating to the utilisation of the exhaust gases of internal combustion aircraft engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB531864A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3216181A (en) * | 1962-07-13 | 1965-11-09 | Ivan H Carpenter | Exhaust system |
-
1939
- 1939-08-04 GB GB22662/39A patent/GB531864A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3216181A (en) * | 1962-07-13 | 1965-11-09 | Ivan H Carpenter | Exhaust system |
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