PL443268A1 - Thermodynamic exhaust manifold, especially for piston aircraft engines - Google Patents
Thermodynamic exhaust manifold, especially for piston aircraft enginesInfo
- Publication number
- PL443268A1 PL443268A1 PL443268A PL44326822A PL443268A1 PL 443268 A1 PL443268 A1 PL 443268A1 PL 443268 A PL443268 A PL 443268A PL 44326822 A PL44326822 A PL 44326822A PL 443268 A1 PL443268 A1 PL 443268A1
- Authority
- PL
- Poland
- Prior art keywords
- exhaust manifold
- aircraft engines
- piston aircraft
- thermodynamic
- rotating cylinder
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N5/00—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy
- F01N5/02—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy the devices using heat
- F01N5/025—Exhaust or silencing apparatus combined or associated with devices profiting by exhaust energy the devices using heat the device being thermoelectric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
- F01N13/00—Exhaust or silencing apparatus characterised by constructional features
- F01N13/08—Other arrangements or adaptations of exhaust conduits
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Exhaust Silencers (AREA)
Abstract
Przedmiotem zgłoszenia jest termodynamiczny kolektor wydechowy, zwłaszcza do tłokowych silników lotniczych, który charakteryzuje się tym, że w centralnej części wewnętrznej części profilowanej (1) kolektora wydechowego znajduje się jednostronnie otwarty obrotowy cylinder (2). W obrotowym cylindrze (2) znajduje się co najmniej 6 otworów. Obrotowy cylinder (2) zamocowany jest na wale (3), a wał (3) łożyskowany jest w zespole łożysk (4), który osadzony jest w podporze (5). Podpora (5) zamocowana jest w wewnętrznej części profilowanej (1) kolektora wydechowego od strony wylotu gazów spalinowych (6).The subject of the application is a thermodynamic exhaust manifold, especially for piston aircraft engines, which is characterized in that in the central part of the internal profiled part (1) of the exhaust manifold there is a rotating cylinder (2) open on one side. There are at least 6 holes in the rotating cylinder (2). The rotating cylinder (2) is mounted on the shaft (3), and the shaft (3) is mounted in a set of bearings (4), which is mounted in the support (5). The support (5) is mounted in the internal profiled part (1) of the exhaust manifold from the side of the exhaust gas outlet (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL443268A PL244749B1 (en) | 2022-12-27 | 2022-12-27 | Thermodynamic exhaust manifold, especially for piston aircraft engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL443268A PL244749B1 (en) | 2022-12-27 | 2022-12-27 | Thermodynamic exhaust manifold, especially for piston aircraft engines |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| PL443268A1 true PL443268A1 (en) | 2023-06-19 |
| PL244749B1 PL244749B1 (en) | 2024-02-26 |
Family
ID=86944906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PL443268A PL244749B1 (en) | 2022-12-27 | 2022-12-27 | Thermodynamic exhaust manifold, especially for piston aircraft engines |
Country Status (1)
| Country | Link |
|---|---|
| PL (1) | PL244749B1 (en) |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5835353B2 (en) * | 2012-01-17 | 2015-12-24 | トヨタ自動車株式会社 | Thermoelectric generator |
| JP2013150419A (en) * | 2012-01-18 | 2013-08-01 | Toyota Motor Corp | Thermoelectric generator |
| KR101421958B1 (en) * | 2013-08-06 | 2014-07-22 | 현대자동차주식회사 | Structure for using exhaust heat of vehicle |
| CN110190781B (en) * | 2019-06-28 | 2020-06-12 | 南京溧水高新创业投资管理有限公司 | Small-sized temperature difference power generation device utilizing waste heat of vehicle tail gas |
-
2022
- 2022-12-27 PL PL443268A patent/PL244749B1/en unknown
Also Published As
| Publication number | Publication date |
|---|---|
| PL244749B1 (en) | 2024-02-26 |
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