PL437916A1 - Aircraft propulsion system - Google Patents

Aircraft propulsion system

Info

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
Application number
PL437916A
Other languages
Polish (pl)
Inventor
Paweł Wawrzyński
Original Assignee
Paweł Wawrzyński
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 Paweł Wawrzyński filed Critical Paweł Wawrzyński
Priority to PL437916A priority Critical patent/PL437916A1/en
Publication of PL437916A1 publication Critical patent/PL437916A1/en

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.

PL437916A 2021-05-19 2021-05-19 Aircraft propulsion system PL437916A1 (en)

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)

Similar Documents

Publication Publication Date Title
RU2168445C2 (en) Device for suction of boundary layer and for monitoring of shock boundary layer for aircraft
RU2672197C2 (en) Aircraft propulsion assembly with fire extinguishing system
RU2487054C2 (en) Aircraft zone vent system
CN101952171B (en) Aircraft propulsion assembly comprising hot air bleed systems
US2632295A (en) Inlet ram for power plants
CN101365870A (en) Infrared suppression system
US10260371B2 (en) Method and assembly for providing an anti-icing airflow
BRPI0816559A2 (en) system and method for air conditioning of at least a partial area of an aircraft
BR0318553B1 (en) fluid cooling system of an aircraft and its aircraft
RU2008107594A (en) ENGINE INSTALLATION FOR AIRCRAFT AND AIRCRAFT CONTAINING AT LEAST ONE SUCH ENGINE INSTALLATION
CN111071460A (en) Nacelle for an aircraft engine
RU2116935C1 (en) Aircraft suction generator system for maintenance of boundary-layer laminarity
SG11201810661WA (en) Railway vehicle air-conditioning duct
PL437916A1 (en) Aircraft propulsion system
US4778130A (en) Ultra hypersonic aircraft
PL439030A1 (en) Aircraft propulsion system
US2841956A (en) Combination variable area converging-diverging nozzle and thrust destroyer
EA201100058A1 (en) ZENITA CONTROLLED ROCKET
Balakin et al. Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
US3486435A (en) Aircraft pressurization system
US2422694A (en) Wall-mounted ram-type aircraft heater
US2548794A (en) Aircraft engine cooling system
US2476643A (en) By-pass system for cooling fans
BR112019026384B8 (en) Propulsion ejector system of a vehicle and vehicle
RU2727103C2 (en) Electric jet propulsion plant