WO2016020742A1 - Moteur à air sous pression pour générateurs d'énergie électrique - Google Patents
Moteur à air sous pression pour générateurs d'énergie électrique Download PDFInfo
- Publication number
- WO2016020742A1 WO2016020742A1 PCT/IB2015/001317 IB2015001317W WO2016020742A1 WO 2016020742 A1 WO2016020742 A1 WO 2016020742A1 IB 2015001317 W IB2015001317 W IB 2015001317W WO 2016020742 A1 WO2016020742 A1 WO 2016020742A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- pressurized air
- engine
- rotor
- pressure chamber
- pressure
- Prior art date
Links
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
- F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C1/00—Rotary-piston machines or engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C19/00—Sealing arrangements in rotary-piston machines or engines
- F01C19/02—Radially-movable sealings for working fluids
- F01C19/06—Radially-movable sealings for working fluids of resilient material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C19/00—Sealing arrangements in rotary-piston machines or engines
- F01C19/08—Axially-movable sealings for working fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
Definitions
- the present invention relates to a pressurized air engine, particularly for electric power generators.
- a pressurized air engine is an engine performing a mechanical work by exploiting the pressurized air expansion.
- a pneumatic motor usually transforms pressurized air into a mechanical work through either a linear or a rotary movement.
- Pressurized air is fed from high pressure pressurized air tanks, for example with a pressure of about 300 bars, and the pressurized air expansion drives a piston or a turbine coupled to a shaft.
- the aim of the present invention is to provide such a pressurized air engine which is improved in comparison with prior pneumatic engines.
- a main object of the invention is to provide such a pressurized air engine which may be usefully used in an electric power generating machine.
- Another object is to provide such a pressurized air engine which may also be used for driving motor vehicles.
- Yet another object of the present invention is to provide such a pressurized air engine construction which may be made starting from easily commercially available elements and materials and which, moreover, is very competitive from a mere economic standpoint.
- Yet another object of the present invention is to provide such a pressurized air engine construction which is very reliable and safe in operation.
- a pressurized air engine for electric power generators characterized in that said pressurized air engine comprises two flanges applied to an engine rotor, integral with a drive shaft, said engine rotor including at least a first pressure chamber and at least a second pressure chamber, identical to said first pressure chamber and arranged at a symmetrically opposite position with respect to said first pressure chamber.
- Said pressure chambers being fed by pressurized air.
- Each said pressure or plenum chamber is designed as a hollow cylinder or any other hollow body having an operating surface on which a pressurized air pressure operates, thereby providing a lever effect causing said engine rotor to be rotated.
- Figure 1 is a partially cross-sectioned side view of the pressurized air engine according to the present invention, being applied to an electric power generator;
- Figure 2 is a front view of the pressurized air engine drive shaft
- Figure 3 is a side view of the pressurized air engine drive shaft;
- Figure 4 is a drive shaft cross-sectional view, substantially taken through the section plane IV-IV of Figure 3;
- FIG. 5 is yet another side view of the drive shaft. DESCRIPTION OF THE PREFERRED EMBODIMENTS
- the pressurized air engine is air supplied from a pressurized air tank 2, which is coupled to the engine 1 through a ball valve 3.
- the pressurized air tank 2 comprises a connecting element 4 for a compressor, not shown in the drawings, for loading said tank with pressurized air at pressure from 10 to 100 bars, preferably 90 bars.
- the pressurized air engine 1 comprises two flanges 5 being applied to an engine rotor 6 integral with a drive shaft 7 with a related cylinder 14.
- Said engine rotor 6 comprises a first pressure or plenum chamber 8 and a second pressure or plenum chamber 88, identical to the first pressure chamber 8 and being arranged at a symmetrically opposite position to said first chamber.
- each said pressure chamber 8, 88 is made as a hollow cylinder or any other hollow body having an operating surface A on which a pressure F operates, thereby providing a lever effect causing the engine rotor 6 to turn.
- the engine rotor 6 may comprise a plurality of pressure or plenum chamber pairs 8, 88, for example 4 or 6 pressure chambers.
- Said engine rotor 6 is tightly provided with two flanges 5 and related cylinder and being to that end provided with suitable gaskets.
- the engine rotor 6 comprises moreover a switch off valve 9 coupled to a flange 5 and being designed for removing pressure from the engine while holding the valve 3 closed.
- the engine rotor 6 comprises moreover a plurality of axially expanding bands, indicated by the reference number 10, and related radial bands 11 , arranged at a 45 degree arrangement with respect to the axial bands 10, and being urged by cylindrical springs 12.
- the drive shaft 7 is in turn coupled to a dynamo 13 for generating electric power, as shown by way of an example in Figure 1.
- the pressurized air engine according to the present invention operates as follows.
- the pressurized air sealed tank 2 is air loaded, preferably at a pressure of 90 bars.
- the only pressure force being generated is the force F pushing on the head or top surface A of the chamber.
- said engine drive shaft is coupled to the dynamo 13 for generating electric power.
- the pressurized air engine has a sealed or tight construction, achieved by dedicated gaskets to provide a constant pressure in said chambers 8, 88.
- the pressurized air engine 1 according to the present invention may be advantageously assembled on a motor vehicle.
- the present invention has provided a pressurized air engine having a high efficiency and which may be used for generating electric power and/or for motor vehicle applications.
- the materials used as well as the contingent size and shapes can be any, depending on requirements.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
Selon l'invention, un moteur à air sous pression, en particulier pour des générateurs d'énergie électrique, comprend un rotor de moteur ayant deux brides intégrées à un arbre d'entraînement, ledit rotor comprenant en outre au moins une première chambre de pression et au moins une seconde chambre de pression pour équilibrer ledit rotor, ladite deuxième chambre de pression étant identique à ladite première chambre de pression et étant disposée symétriquement à l'opposé de la première chambre de pression, lesdites première et deuxième chambres étant alimentées en air sous pression, chaque chambre de pression étant conçue sous la forme d'un cylindre creux ou de tout autre type de corps creux, avec une surface fonctionnelle sur laquelle agit une pression générée par de l'air sous pression, ledit air sous pression entrant directement dans la première chambre et ensuite dans la deuxième chambre, ce qui permet d'obtenir un effet de levier amenant ledit rotor de moteur à tourner.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP15767237.9A EP3177809A1 (fr) | 2014-08-06 | 2015-08-04 | Moteur à air sous pression pour générateurs d'énergie électrique |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITMI2014A001458 | 2014-08-06 | ||
ITMI20141458 | 2014-08-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2016020742A1 true WO2016020742A1 (fr) | 2016-02-11 |
Family
ID=51753318
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IB2015/001317 WO2016020742A1 (fr) | 2014-08-06 | 2015-08-04 | Moteur à air sous pression pour générateurs d'énergie électrique |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP3177809A1 (fr) |
WO (1) | WO2016020742A1 (fr) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE891165C (de) * | 1950-03-09 | 1953-09-24 | Alois Horner | Turbine fuer gas- und dampffoermige Treibmittel |
US3609058A (en) * | 1969-09-08 | 1971-09-28 | Balazs K Tarsoly | Turbine motor having balanced gas lubricated rotor |
WO2007129846A1 (fr) * | 2006-05-09 | 2007-11-15 | Joon Tai Park | Moteur à turbine à air comprimé |
WO2008014586A1 (fr) * | 2006-08-03 | 2008-02-07 | Arthur Isbrecht | Moteur à combustion interne rotatif avec rotor circulaire |
WO2011104606A2 (fr) * | 2010-02-24 | 2011-09-01 | Air Power Technologies Group Limited | Moteur thermique à haut rendement entraîné par air comprimé ou autres gaz compressibles |
WO2013050852A2 (fr) * | 2011-10-07 | 2013-04-11 | Mariani Augusto | Moteur à combustion interne rotatif à haute efficacité |
-
2015
- 2015-08-04 WO PCT/IB2015/001317 patent/WO2016020742A1/fr active Application Filing
- 2015-08-04 EP EP15767237.9A patent/EP3177809A1/fr not_active Withdrawn
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE891165C (de) * | 1950-03-09 | 1953-09-24 | Alois Horner | Turbine fuer gas- und dampffoermige Treibmittel |
US3609058A (en) * | 1969-09-08 | 1971-09-28 | Balazs K Tarsoly | Turbine motor having balanced gas lubricated rotor |
WO2007129846A1 (fr) * | 2006-05-09 | 2007-11-15 | Joon Tai Park | Moteur à turbine à air comprimé |
WO2008014586A1 (fr) * | 2006-08-03 | 2008-02-07 | Arthur Isbrecht | Moteur à combustion interne rotatif avec rotor circulaire |
WO2011104606A2 (fr) * | 2010-02-24 | 2011-09-01 | Air Power Technologies Group Limited | Moteur thermique à haut rendement entraîné par air comprimé ou autres gaz compressibles |
WO2013050852A2 (fr) * | 2011-10-07 | 2013-04-11 | Mariani Augusto | Moteur à combustion interne rotatif à haute efficacité |
Also Published As
Publication number | Publication date |
---|---|
EP3177809A1 (fr) | 2017-06-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2017103126A (ru) | Гибридизация компрессоров турбореактивного двигателя | |
WO2011003163A8 (fr) | Compresseur linéaire | |
WO2012069122A3 (fr) | Dispositif de récupération de la chaleur résiduelle | |
RU2013149798A (ru) | Система уплотнения вала | |
MXPA05007417A (es) | Motor de compresion variable. | |
CN105715308A (zh) | 用于防涡轮增压器爆裂的压缩机组件 | |
WO2011009453A3 (fr) | Moteur à pistons axiaux, procédé pour faire fonctionner un moteur à pistons axiaux et procédé de réalisation d'un échangeur thermique d'un moteur à pistons axiaux | |
JP2017505412A (ja) | 軸受係止組立体及びその組み立て方法 | |
RU2017109234A (ru) | Система вспомогательных агрегатов у двигателя внутреннего сгорания | |
WO2013050852A2 (fr) | Moteur à combustion interne rotatif à haute efficacité | |
RS20180681A2 (sr) | Gasno-turbinsko postrojenje sa pneumatskim motorom sa unutrašnjim sagorevanjem pri konstantnom pritisku | |
WO2016020742A1 (fr) | Moteur à air sous pression pour générateurs d'énergie électrique | |
BRPI1009259A2 (pt) | motor de ar comprimido, uso do mesmo e veículo motorizado | |
US8910613B2 (en) | Internal combustion engine | |
US20170350250A1 (en) | Free rotary fluid machine | |
CN104047711A (zh) | 齿轮式转子发动机 | |
WO2015051860A3 (fr) | Chaîne de propulsion d'un véhicule automobile hybride | |
RU2593858C1 (ru) | Комбинированный роторно-поршневой двигатель внутреннего сгорания | |
US20180156319A1 (en) | Planetary friction gear mechanism, method for operating a planetary friction gear mechanism, and fluid energy machine | |
US20070137609A1 (en) | True rotary internal combustion engine | |
US20090084101A1 (en) | Apparatuses for Converting Pressure Differences of Gaseous or Liquid Media Into Rotary Motion | |
KR20170073799A (ko) | 엔진용 터닝기어 | |
WO2018184078A3 (fr) | Moteur à combustion interne rotatif hybride triphasé tesla | |
RU2011146869A (ru) | Насосный узел для подачи топлива, предпочтительно дизельного топлива, в двигатель внутреннего сгорания | |
CN204942544U (zh) | 全剖分式碳环密封装置 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 15767237 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
REEP | Request for entry into the european phase |
Ref document number: 2015767237 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2015767237 Country of ref document: EP |