PL415225A1 - Aircraft combustion engine with the intra-vane fuel combustion and method for controlling the combustion engine with the intra-vane fuel combustion - Google Patents
Aircraft combustion engine with the intra-vane fuel combustion and method for controlling the combustion engine with the intra-vane fuel combustionInfo
- Publication number
- PL415225A1 PL415225A1 PL415225A PL41522515A PL415225A1 PL 415225 A1 PL415225 A1 PL 415225A1 PL 415225 A PL415225 A PL 415225A PL 41522515 A PL41522515 A PL 41522515A PL 415225 A1 PL415225 A1 PL 415225A1
- Authority
- PL
- Poland
- Prior art keywords
- blades
- combustion
- intra
- combustion engine
- vane fuel
- Prior art date
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Lotniczy silnik spalinowy z wewnątrz łopatkowym spalaniem paliwa, wyposażony w łopaty wentylatora, lub śmigła lub wiropłata, charakteryzuje się tym, że wewnątrz wirujących łopat wentylatora (1) lub śmigła lub łopaty wiropłata usytuowane są kanały (5), połączone z dyszami (9). Powietrze doprowadzone jest do wykonanych wewnątrz wirujących łopat wentylatora (1) lub śmigła lub łopaty wiropłata kanałów (5), które doprowadzają powietrze do znajdujących się w końcowych częściach łopat komór spalania (6), gdzie spalone zostaje paliwo dostarczone z układu zasilania (11), a spaliny o wysokiej energii kanałami spalinowymi (10) przemieszczają się do dysz (9), w których wytwarzana jest siła ciągu, a której składowe powodują obrót wentylatora lub śmigła, oraz częściowo może być wytwarzany ciąg odrzutowy wzdłuż osi silnika.An internal combustion engine with internal vane fuel combustion, equipped with fan blades, or propellers or rotorcraft, is characterized by the fact that inside the rotating fan blades (1) or the rotor blades or rotor blades there are channels (5) connected to the nozzles (9). The air is supplied to the fan blades (5) made inside the rotating blades (1) or the propeller or blades that supply air to the combustion chambers (6) located in the end parts of the blades, where the fuel supplied from the power supply system (11) is burned, and high-energy exhaust gases through flue gas (10) travel to nozzles (9), in which thrust is generated, the components of which cause the fan or propeller to rotate, and partly jet thrust along the engine axis.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL415225A PL415225A1 (en) | 2015-12-10 | 2015-12-10 | Aircraft combustion engine with the intra-vane fuel combustion and method for controlling the combustion engine with the intra-vane fuel combustion |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL415225A PL415225A1 (en) | 2015-12-10 | 2015-12-10 | Aircraft combustion engine with the intra-vane fuel combustion and method for controlling the combustion engine with the intra-vane fuel combustion |
Publications (1)
Publication Number | Publication Date |
---|---|
PL415225A1 true PL415225A1 (en) | 2017-06-19 |
Family
ID=59061568
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL415225A PL415225A1 (en) | 2015-12-10 | 2015-12-10 | Aircraft combustion engine with the intra-vane fuel combustion and method for controlling the combustion engine with the intra-vane fuel combustion |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL415225A1 (en) |
-
2015
- 2015-12-10 PL PL415225A patent/PL415225A1/en unknown
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