PL423114A1 - Hybrid propulsion system of an aircraft - Google Patents
Hybrid propulsion system of an aircraftInfo
- Publication number
- PL423114A1 PL423114A1 PL423114A PL42311417A PL423114A1 PL 423114 A1 PL423114 A1 PL 423114A1 PL 423114 A PL423114 A PL 423114A PL 42311417 A PL42311417 A PL 42311417A PL 423114 A1 PL423114 A1 PL 423114A1
- Authority
- PL
- Poland
- Prior art keywords
- aircraft
- propulsion system
- hybrid propulsion
- driving
- rectifiers
- Prior art date
Links
- 230000001105 regulatory effect Effects 0.000 abstract 1
Landscapes
- Control Of Multiple Motors (AREA)
- Control Of Eletrric Generators (AREA)
Abstract
Układ napędowy statku powietrznego składa się z dwóch niezależnych zespołów napędowych złożonych z co najmniej jednego silnika turbinowego (8) napędzającego bezpośrednio bez pośrednictwa przekładni i z co najmniej jednego generatora prądu zmiennego (7), który poprzez prostowniki (6) przekazuje przewodami zasilającymi (13) wytworzony prąd elektryczny do falowników (4) sterowanych przez urządzenie kontrolno-regulujące (3), połączone z dwoma silnikami prądu przemiennego (1 i 2) napędzającymi śmigła (9, 10), pracujące w układzie przeciwbieżnym o stałym skoku.The aircraft propulsion system consists of two independent propulsion units composed of at least one turbine engine (8) driving directly without gearing and with at least one alternating current generator (7), which through rectifiers (6) transmits generated cables (13) electric current to inverters (4) controlled by a control and regulating device (3), connected to two AC motors (1 and 2) driving propellers (9, 10), working in a counter-rotating system with constant pitch.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL423114A PL233584B1 (en) | 2017-10-09 | 2017-10-09 | Hybrid propulsion system of an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL423114A PL233584B1 (en) | 2017-10-09 | 2017-10-09 | Hybrid propulsion system of an aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
PL423114A1 true PL423114A1 (en) | 2019-04-23 |
PL233584B1 PL233584B1 (en) | 2019-11-29 |
Family
ID=66167884
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL423114A PL233584B1 (en) | 2017-10-09 | 2017-10-09 | Hybrid propulsion system of an aircraft |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL233584B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
PL438034A1 (en) | 2021-05-28 | 2022-12-05 | Politechnika Rzeszowska im. Ignacego Łukasiewicza | Aviation turboalternator |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2423509A (en) * | 2005-02-25 | 2006-08-30 | Boeing Co | Vertical and short take-off and landing aircraft |
RU2534676C1 (en) * | 2013-05-27 | 2014-12-10 | Дмитрий Сергеевич Дуров | Cryogenic turbo-electric stol aircraft |
-
2017
- 2017-10-09 PL PL423114A patent/PL233584B1/en unknown
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2423509A (en) * | 2005-02-25 | 2006-08-30 | Boeing Co | Vertical and short take-off and landing aircraft |
RU2534676C1 (en) * | 2013-05-27 | 2014-12-10 | Дмитрий Сергеевич Дуров | Cryogenic turbo-electric stol aircraft |
Also Published As
Publication number | Publication date |
---|---|
PL233584B1 (en) | 2019-11-29 |
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