PL437916A1 - Aircraft propulsion system - Google Patents
Aircraft propulsion systemInfo
- Publication number
- PL437916A1 PL437916A1 PL437916A PL43791621A PL437916A1 PL 437916 A1 PL437916 A1 PL 437916A1 PL 437916 A PL437916 A PL 437916A PL 43791621 A PL43791621 A PL 43791621A PL 437916 A1 PL437916 A1 PL 437916A1
- Authority
- PL
- Poland
- Prior art keywords
- aircraft
- channel
- electromagnetic radiation
- duct
- receiver
- Prior art date
Links
Landscapes
- Excavating Of Shafts Or Tunnels (AREA)
Abstract
Wynalazek dotyczy układu do napędzania statku powietrznego, w szczególności do wynoszenia ładunków na orbitę okołoziemską, w którym statek powietrzny zawiera zamocowaną do swojego kadłuba jednostkę napędową (1) zawierającą obudowę ze ścianką boczną (2) i wewnętrznym przelotowym kanałem (3). Wlot (4) kanału (3) ma mniejszą powierzchnię niż powierzchnia wylotu (5) kanału (3) tak, że kanał (3) jest zbieżny w kierunku swojego wlotu (4). Wewnątrz kanału (3) usytuowany jest odbiornik (8) promieniowania elektromagnetycznego (7) do ogrzewania powietrza przepływającego przez kanał (3). Układ zawiera ponadto źródło (6) promieniowania elektromagnetycznego (7) skonfigurowane do kierowania wiązek promieniowania elektromagnetycznego (7) do odbiornika (8), które to źródło (6) usytuowane jest poza statkiem powietrznym.The invention relates to a system for propelling an aircraft, in particular for launching payloads into Earth orbit, in which the aircraft comprises a propulsion unit (1) attached to its fuselage, comprising a housing with a side wall (2) and an internal through passage (3). The inlet (4) of the channel (3) has a smaller area than the area of the outlet (5) of the channel (3), so that the channel (3) tapers towards its inlet (4). Inside the duct (3) there is a receiver (8) for electromagnetic radiation (7) for heating the air flowing through the duct (3). The system further comprises a source (6) of electromagnetic radiation (7) configured to direct the beams of electromagnetic radiation (7) to a receiver (8), which source (6) is located outside the aircraft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL437916A PL437916A1 (en) | 2021-05-19 | 2021-05-19 | Aircraft propulsion system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL437916A PL437916A1 (en) | 2021-05-19 | 2021-05-19 | Aircraft propulsion system |
Publications (1)
Publication Number | Publication Date |
---|---|
PL437916A1 true PL437916A1 (en) | 2022-11-21 |
Family
ID=84191864
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL437916A PL437916A1 (en) | 2021-05-19 | 2021-05-19 | Aircraft propulsion system |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL437916A1 (en) |
-
2021
- 2021-05-19 PL PL437916A patent/PL437916A1/en unknown
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