ES8501848A1 - Wind propulsion system of combined action (Machine-translation by Google Translate, not legally binding) - Google Patents
Wind propulsion system of combined action (Machine-translation by Google Translate, not legally binding)Info
- Publication number
- ES8501848A1 ES8501848A1 ES528977A ES528977A ES8501848A1 ES 8501848 A1 ES8501848 A1 ES 8501848A1 ES 528977 A ES528977 A ES 528977A ES 528977 A ES528977 A ES 528977A ES 8501848 A1 ES8501848 A1 ES 8501848A1
- Authority
- ES
- Spain
- Prior art keywords
- translation
- machine
- legally binding
- google translate
- combined action
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired
Links
- VJYFKVYYMZPMAB-UHFFFAOYSA-N ethoprophos Chemical compound CCCSP(=O)(OCC)SCCC VJYFKVYYMZPMAB-UHFFFAOYSA-N 0.000 abstract 2
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Jet Pumps And Other Pumps (AREA)
Abstract
COMBINED ACTION WIND PROPULSION SYSTEM, CONSISTING IN PRODUCING AN AIR FLOW THROUGH FANS (2A) AT THE ENTRANCE OF A MAIN DUCT (1) SOLIDARITY OF THE MOBILE PLATFORM (10), INCREASING SUCH A FLOW BY 4 TUBOS SECONDARY DUCT (3), LOCATED IN ZONES (5) OF MINIMUM SECTION AND MAXIMUM SUCTION, AND DIRECT IT TO ONE OR SEVERAL PROPULSION CYLINDERS (2) DRIVEN BY ENGINES, WHICH, WHEN TURNING, INTERCEPT THE AIR FLOW, PRODUCING A DEPRESSION PROPELLING FORCE (D) TO MOVE THE MOBILE PLATFORM. (Machine-translation by Google Translate, not legally binding)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES528977A ES528977A0 (en) | 1984-01-19 | 1984-01-19 | COMBINED ACTION WIND PROPULSION SYSTEM |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| ES528977A ES528977A0 (en) | 1984-01-19 | 1984-01-19 | COMBINED ACTION WIND PROPULSION SYSTEM |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| ES8501848A1 true ES8501848A1 (en) | 1984-12-16 |
| ES528977A0 ES528977A0 (en) | 1984-12-16 |
Family
ID=8486745
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES528977A Granted ES528977A0 (en) | 1984-01-19 | 1984-01-19 | COMBINED ACTION WIND PROPULSION SYSTEM |
Country Status (1)
| Country | Link |
|---|---|
| ES (1) | ES528977A0 (en) |
-
1984
- 1984-01-19 ES ES528977A patent/ES528977A0/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| ES528977A0 (en) | 1984-12-16 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| SE8203975D0 (en) | KOMPOUNDDRIVAGGREGAT | |
| ES8102643A1 (en) | Systems for utilizing the energy of a moving air current | |
| IT8519739A0 (en) | COUNTER-ROTATING TURBO FAN ENGINE WITH HIGH DERIVATION RATIO. | |
| IT1135606B (en) | AUXILIARY VENTILATION SYSTEM FOR GAS TURBO ENGINES | |
| DE69008429D1 (en) | Turbo jet and rocket combination engine. | |
| SE8803415L (en) | gas turbine engine | |
| IT1185598B (en) | BLADES RETAINING SYSTEM, ESPECIALLY OF GAS TURBO ENGINE COMPRESSOR BLADES | |
| DE69300239D1 (en) | Gas turbine combined with air separation system. | |
| JPS5738645A (en) | Propulsion reinforcing turbo fan engine | |
| IT8323356A0 (en) | COUPLED. SUPPORT SYSTEM FOR TURBO SHAFT GAS TURBINE ENGINES | |
| GB2095335B (en) | Gas turbine engine air intake system | |
| IT7923984A0 (en) | COOLING AIR DELIVERY SYSTEM TO ADJUST THE THERMAL EXPANSION OF THE BAND/ROTOR IN GAS TURBO ENGINES. | |
| IT8324164A0 (en) | IMPROVEMENTS MADE TO THE AIR INTAKES OF AGAS TURBINE ENGINES MOUNTED ON AIRCRAFT. | |
| IT8521319A0 (en) | GAS TURBO ENGINE CONTROL SYSTEM. | |
| GB2018362A (en) | Gas turbine engine cooling | |
| DE69006868D1 (en) | Gas turbine air jet engine. | |
| JPS5377319A (en) | Axial-flow fan | |
| IT8719132A0 (en) | FUEL INJECTION SYSTEM FOR AN AIR COMPRESSION ENGINE, WITH ELECTRONIC REGULATION. | |
| IT8423838A0 (en) | COMPACT FRESH GAS INLET SYSTEM, FOR ENGINES WITH COMBINED SUPERCHARGING. | |
| FR2671138B1 (en) | CONDITIONING AND IGNITION SYSTEM OF THE ROCKET ENGINE. | |
| IT8519738A0 (en) | COOLING AIR CONTROL SYSTEM FOR AGAS TURBO ENGINE. | |
| GB2014663A (en) | Gas Turbine Ducted Fan Engine | |
| JPS5341097A (en) | Air conditioning exhaust system | |
| IT8324154A0 (en) | FINAL IDLE RPM REGULATOR FOR INTERNAL MICRO-INJECTION ENGINES. | |
| IT8119747A0 (en) | HIGH EFFICIENCY MOTOR FOR APPLICATIONS IN LAND, SEA AND AIR ENGINES, AS WELL AS FOR LIGHTING, HEATING, REFRIGERATION AND SIMILAR USE. |