PL423114A1 - Hybrid propulsion system of an aircraft - Google Patents

Hybrid propulsion system of an aircraft

Info

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
Application number
PL423114A
Other languages
Polish (pl)
Other versions
PL233584B1 (en
Inventor
Edward MARGAŃSKI
Andrzej IZDEBSKI
Original Assignee
Izdebski Andrzej
Marganski Edward
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Izdebski Andrzej, Marganski Edward filed Critical Izdebski Andrzej
Priority to PL423114A priority Critical patent/PL233584B1/en
Publication of PL423114A1 publication Critical patent/PL423114A1/en
Publication of PL233584B1 publication Critical patent/PL233584B1/en

Links

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.

PL423114A 2017-10-09 2017-10-09 Hybrid propulsion system of an aircraft PL233584B1 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (2)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
RU2016139023A (en) ARCHITECTURE OF THE POWER SYSTEM OF THE MULTI-MOTOR HELICOPTER AND THE RELATED HELICOPTER
AR103532A1 (en) PROCEDURE FOR OPERATING A WIND FARM
BR112017003417A2 (en) electric drive system for mining trailer truck
EP2928068A3 (en) Systems utilizing a controllable voltage AC generator system
EP4249748A3 (en) Method for controlling a wind turbine
BR112018002134A2 (en) electric vehicle charging station, and method for controlling at least one electric vehicle charging station
RU2015117607A (en) STATIC EXCITER SYSTEM FOR GENERATORS
EP2779431A3 (en) Generation of a current reference to control a brushless motor
RU2396695C1 (en) Electromechanical control device
PL423114A1 (en) Hybrid propulsion system of an aircraft
BR112017017375A2 (en) system for supplying at least one electric consumer or direct current energy store
BR112013021481A2 (en) welding system with rotational speed converter for auxiliary power generator and method for operating the welding system
RU2396693C1 (en) Self-contained electric control device
RU2461116C1 (en) Electromechanical device
Zharkov et al. Electric starter mode three-stage synchronous generator with damping cage
RU156788U1 (en) DEVICE FOR BENCH TESTS OF ASYNCHRONOUS TRACTION ENGINES
RU2602063C2 (en) Electromechanical control device
PL424586A3 (en) Hybrid propulsion system of a helicopter
EP2793389A3 (en) Interleaved motor controllers for an electric taxi system
EP2878793A3 (en) Engine control apparatus and engine control method
RU2582648C2 (en) Electromechanical control device
RU2548364C1 (en) Electromechanical device
EP2928069A3 (en) Systems utilizing a controllable voltage AC generator system
GB2596503A8 (en) Power generation system and plant control device
TR201906088T4 (en) Method for solar power plant operation.