PL424280A1 - Revolving-block heat engine - Google Patents
Revolving-block heat engineInfo
- Publication number
- PL424280A1 PL424280A1 PL424280A PL42428018A PL424280A1 PL 424280 A1 PL424280 A1 PL 424280A1 PL 424280 A PL424280 A PL 424280A PL 42428018 A PL42428018 A PL 42428018A PL 424280 A1 PL424280 A1 PL 424280A1
- Authority
- PL
- Poland
- Prior art keywords
- rotor
- main rotor
- additional
- combustion chambers
- outlet side
- Prior art date
Links
- 230000006835 compression Effects 0.000 abstract 3
- 238000007906 compression Methods 0.000 abstract 3
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 239000007789 gas Substances 0.000 abstract 1
- 230000035939 shock Effects 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
- F01D1/28—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially radially
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Supercharger (AREA)
Abstract
Silnik ma korpus, w którym jest osadzony wirnik główny (1) o przepływie osiowym, zawierający na swoim obwodzie układ przepływowy złożony z wewnętrznych kanałów sprężających po stronie wlotowej, komór spalania i dysz wylotowych po stronie wylotowej, w którym wewnętrzne kanały sprężające tworzą kompresor falowy wytwarzający fale uderzeniowe sprężające powietrze doprowadzane do komór spalania, oraz osadzony współosiowo w korpusie dodatkowy wirnik o przepływie osiowym z częścią turbinową (3) napędzaną spalinami opuszczającymi wirnik główny (1). Dodatkowy wirnik stanowi wirnik swobodny, o kierunku obrotu przeciwnym do kierunku obrotu wirnika głównego (1), przy czym część turbinowa (3), usytuowana po stronie wylotowej wirnika głównego (1), jest połączona sztywno z częścią sprężającą (2) usytuowaną po stronie wlotowej wirnika głównego (1). W innym wykonaniu silnik ma osadzony współosiowo w korpusie dodatkowy wirnik o przepływie promieniowym.The engine has a body in which the main rotor (1) with axial flow is mounted, containing on its periphery a flow system composed of internal compression channels on the inlet side, combustion chambers and exhaust nozzles on the outlet side, in which the internal compression channels form a wave compressor producing shock waves compressing the air supplied to the combustion chambers, and an additional axial flow rotor coaxially mounted in the body with the turbine part (3) driven by exhaust gases leaving the main rotor (1). The additional rotor is a free rotor, with a direction of rotation opposite to the direction of rotation of the main rotor (1), whereby the turbine part (3), located on the outlet side of the main rotor (1), is rigidly connected to the compression part (2) located on the inlet side main rotor (1). In another embodiment, the motor has an additional radial flow impeller mounted coaxially in the body.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL424280A PL243763B1 (en) | 2018-01-16 | 2018-01-16 | Revolving-block heat engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL424280A PL243763B1 (en) | 2018-01-16 | 2018-01-16 | Revolving-block heat engine |
Publications (2)
Publication Number | Publication Date |
---|---|
PL424280A1 true PL424280A1 (en) | 2019-07-29 |
PL243763B1 PL243763B1 (en) | 2023-10-09 |
Family
ID=67384361
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL424280A PL243763B1 (en) | 2018-01-16 | 2018-01-16 | Revolving-block heat engine |
Country Status (1)
Country | Link |
---|---|
PL (1) | PL243763B1 (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1435687A (en) * | 1971-11-26 | 1976-05-12 | Chair R S De | Gas generators |
US20060283170A1 (en) * | 2005-06-15 | 2006-12-21 | Clauson Luke W | Radial flow turbine |
WO2012171094A1 (en) * | 2011-06-16 | 2012-12-20 | Socpra Sciences Et Génie, S.E.C. | Combustion systems and combustion system components for rotary ramjet engines |
US8839599B1 (en) * | 2013-10-07 | 2014-09-23 | Juan Pedro Mesa, Jr. | Axial combustion engine |
WO2015181519A1 (en) * | 2014-05-28 | 2015-12-03 | Gabrielle Engine Limited | Combustion engine |
CN106930786A (en) * | 2017-04-27 | 2017-07-07 | 西安交通大学 | A kind of multistage radial-flow type counter rotating turbine structure |
-
2018
- 2018-01-16 PL PL424280A patent/PL243763B1/en unknown
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1435687A (en) * | 1971-11-26 | 1976-05-12 | Chair R S De | Gas generators |
US20060283170A1 (en) * | 2005-06-15 | 2006-12-21 | Clauson Luke W | Radial flow turbine |
WO2012171094A1 (en) * | 2011-06-16 | 2012-12-20 | Socpra Sciences Et Génie, S.E.C. | Combustion systems and combustion system components for rotary ramjet engines |
US8839599B1 (en) * | 2013-10-07 | 2014-09-23 | Juan Pedro Mesa, Jr. | Axial combustion engine |
WO2015181519A1 (en) * | 2014-05-28 | 2015-12-03 | Gabrielle Engine Limited | Combustion engine |
CN106930786A (en) * | 2017-04-27 | 2017-07-07 | 西安交通大学 | A kind of multistage radial-flow type counter rotating turbine structure |
Also Published As
Publication number | Publication date |
---|---|
PL243763B1 (en) | 2023-10-09 |
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