PL243621B1 - Method of utilization of recoil energy for powering of a turbine in the hydrogen engine with semi-open gas flow - Google Patents

Method of utilization of recoil energy for powering of a turbine in the hydrogen engine with semi-open gas flow

Info

Publication number
PL243621B1
PL243621B1 PL424451A PL42445118A PL243621B1 PL 243621 B1 PL243621 B1 PL 243621B1 PL 424451 A PL424451 A PL 424451A PL 42445118 A PL42445118 A PL 42445118A PL 243621 B1 PL243621 B1 PL 243621B1
Authority
PL
Poland
Prior art keywords
turbine
energy
gas flow
gases
engine
Prior art date
Application number
PL424451A
Other languages
Polish (pl)
Other versions
PL424451A1 (en
Inventor
Zbigniew Jan Lisowski
Original Assignee
Zbigniew Jan Lisowski
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 Zbigniew Jan Lisowski filed Critical Zbigniew Jan Lisowski
Priority to PL424451A priority Critical patent/PL243621B1/en
Publication of PL424451A1 publication Critical patent/PL424451A1/en
Publication of PL243621B1 publication Critical patent/PL243621B1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/66—Combustion or thrust chambers of the rotary type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/56—Combustion chambers having rotary flame tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

Silnik o jednostronnie otwartym przepływie gazów jest maszyną cieplną składającą się z czterech głównych części: obudowy (1), wału napędowego (2), wirnika zawierającego trzy komory spalania lub ich wielokrotność (3), dwustopniowej turbiny gazowej (4). Sposób wykorzystania energii odrzutu pochodzącej z wirnika (3), w którym są umieszczone trzy (lub wielokrotność) komory spalania (9) generujące wypadkową siłę na skutek odrzutu gazów polega na skierowaniu w stronę łopat dwustopniowej turbiny (4) strumienia gorących gazów spalinowych dzięki ustawionym po obwodzie zgodnie z osią wału (2) stałym kierownicom (6) o kształcie garbu. Kierownice (6) są na stałe połączone z obwodowym zagłębieniem głównej komory rozprężnej (5) w obudowie (1). Napływające do komory rozprężnej (5) gorące gazy są sprężane na przewężeniu obudowy i następnie, rozprężając się, wprawiają w zgodny z wirnikiem ruch obrotowy dwustopniową turbinę. W wyniku wspólnej pracy tych elementów na wale (2) wytwarzana jest mechaniczna energia napędowa zdolna do napędzania dowolnego odbiornika. Silnik wykorzystuje jednocześnie dwa rodzaje energii - odrzut bezpośredni gazów i energię termiczną przepływu tych gazów przez turbinę. Nazwa silnika o jednostronnie otwartym przepływie gazów wynika z braku centralnego wlotu powietrza i sprężarki jak znanych silnikach turbinowych. Silnik o jednostronnie otwartym przepływie gazów napędzany jest energią spalania mieszaniny czystego chemicznie wodoru i tlenu ale może być także zasilany innymi lotnymi paliwami płynnymi oraz gazowymi z udziałem powietrza.An engine with one-sided open gas flow is a thermal machine consisting of four main parts: casing (1), drive shaft (2), rotor containing three combustion chambers or their multiple (3), and a two-stage gas turbine (4). The method of using the recoil energy coming from the rotor (3), in which there are three (or multiple) combustion chambers (9) generating the resultant force due to the recoil of gases, consists in directing a stream of hot exhaust gases towards the blades of the two-stage turbine (4) thanks to the positioned circumference in accordance with the axis of the shaft (2) to fixed vanes (6) in the shape of a hump. The blades (6) are permanently connected to the circumferential recess of the main expansion chamber (5) in the housing (1). Hot gases flowing into the expansion chamber (5) are compressed at the narrowing of the casing and then, expanding, set the two-stage turbine in rotational motion in line with the rotor. As a result of the joint operation of these elements on the shaft (2), mechanical driving energy is generated, capable of driving any receiver. The engine uses two types of energy at the same time - direct recoil of gases and thermal energy of the flow of these gases through the turbine. The name of the engine with one-sided open gas flow results from the lack of a central air inlet and compressor like known turbine engines. The engine with a one-sided open gas flow is powered by the energy of combustion of a mixture of chemically pure hydrogen and oxygen, but it can also be powered by other volatile liquid and gaseous fuels with air.

PL424451A 2018-01-31 2018-01-31 Method of utilization of recoil energy for powering of a turbine in the hydrogen engine with semi-open gas flow PL243621B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL424451A PL243621B1 (en) 2018-01-31 2018-01-31 Method of utilization of recoil energy for powering of a turbine in the hydrogen engine with semi-open gas flow

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL424451A PL243621B1 (en) 2018-01-31 2018-01-31 Method of utilization of recoil energy for powering of a turbine in the hydrogen engine with semi-open gas flow

Publications (2)

Publication Number Publication Date
PL424451A1 PL424451A1 (en) 2018-07-30
PL243621B1 true PL243621B1 (en) 2023-09-18

Family

ID=62954768

Family Applications (1)

Application Number Title Priority Date Filing Date
PL424451A PL243621B1 (en) 2018-01-31 2018-01-31 Method of utilization of recoil energy for powering of a turbine in the hydrogen engine with semi-open gas flow

Country Status (1)

Country Link
PL (1) PL243621B1 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2927973A1 (en) * 1979-07-11 1981-01-15 Herbert Ahlgrimm Rotary hydrogen-oxygen engine - has rotor with combustion chambers and sealing segments interrupting gas supply
DE4310508A1 (en) * 1993-03-31 1994-10-06 Boltersdorf Wilfried Power plant (driving system, drive mechanism)
WO1995017590A1 (en) * 1993-12-15 1995-06-29 Andrew Schlote Rotary heat engine
PL384783A1 (en) * 2008-03-26 2008-09-15 Zbigniew Lisowski Rotating three-cycle engine, jet-propelled

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2927973A1 (en) * 1979-07-11 1981-01-15 Herbert Ahlgrimm Rotary hydrogen-oxygen engine - has rotor with combustion chambers and sealing segments interrupting gas supply
DE4310508A1 (en) * 1993-03-31 1994-10-06 Boltersdorf Wilfried Power plant (driving system, drive mechanism)
WO1995017590A1 (en) * 1993-12-15 1995-06-29 Andrew Schlote Rotary heat engine
PL384783A1 (en) * 2008-03-26 2008-09-15 Zbigniew Lisowski Rotating three-cycle engine, jet-propelled

Also Published As

Publication number Publication date
PL424451A1 (en) 2018-07-30

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