GB530543A - Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes - Google Patents
Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposesInfo
- Publication number
- GB530543A GB530543A GB18663/39A GB1866339A GB530543A GB 530543 A GB530543 A GB 530543A GB 18663/39 A GB18663/39 A GB 18663/39A GB 1866339 A GB1866339 A GB 1866339A GB 530543 A GB530543 A GB 530543A
- Authority
- GB
- United Kingdom
- Prior art keywords
- utilisation
- relating
- exhaust gas
- pipes
- gas energy
- 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
530,543. Propelling aircraft. JUNKERS FLUGZEUG - UND - MOTORENWERKE AKT.-GES. June 27, 1939. No. 18663. Convention date, July 9, 1938. Addition to 506,699. Drawings to Specification. [Class 4] Aero-engine exhaust pipes constructed and arranged as described in the parent Specification have their free ends connected together by means of one or more coupling bars in order to suppress oscillations. As shown, fishplates are secured to the exhaust pipes by welding or soldering and the fish-plates are connected by bars disposed above and below the pipes. Clearance in the securing means may provide for expansion and the bar below the pipes may be braced to a part not subject to the oscillations.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE530543X | 1938-07-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB530543A true GB530543A (en) | 1940-12-13 |
Family
ID=6554563
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18663/39A Expired GB530543A (en) | 1938-07-09 | 1939-06-27 | Improvements in and relating to the utilisation of the exhaust gas energy of aircraft engines for propulsion purposes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB530543A (en) |
-
1939
- 1939-06-27 GB GB18663/39A patent/GB530543A/en not_active Expired
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