RS20090068A - Rotor blade for framed hydro and aero turbines - Google Patents

Rotor blade for framed hydro and aero turbines

Info

Publication number
RS20090068A
RS20090068A RSP-2009/0068A RSP20090068A RS20090068A RS 20090068 A RS20090068 A RS 20090068A RS P20090068 A RSP20090068 A RS P20090068A RS 20090068 A RS20090068 A RS 20090068A
Authority
RS
Serbia
Prior art keywords
framed
turbines
hydro
aero
fluid
Prior art date
Application number
RSP-2009/0068A
Other languages
Serbian (sr)
Inventor
Nenad PAUNOVIĆ
Original Assignee
Nenad PAUNOVIĆ
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 Nenad PAUNOVIĆ filed Critical Nenad PAUNOVIĆ
Priority to RSP-2009/0068A priority Critical patent/RS20090068A/en
Publication of RS20090068A publication Critical patent/RS20090068A/en

Links

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/20Hydro energy

Landscapes

  • Hydraulic Turbines (AREA)

Abstract

Invention herewith described refers to the rotor blade for the framed hydro and aero turbines. The new concept of blades (1) for the framed hydro turbines and aero turbines represents a new geometric principle of the blade shape for the highest degree of utilization of the fluid kinetic energy conversion in the framed turbines regardless of the fluid speed. In relation to this, the most similar concept of combined lift-thrust gas turbine blades with their reduced surface area of the blade upper part (3) provides a better flow of the fluid through the framed turbine, whereby in relation to the concept of gas turbine blades applied under the same conditions (in framed aero and hydro turbines applied in open systems - rivers, seas and oceans) a greater efficiency of the fluid energy conversion is achieved through the turbine blades to the rotor of the turbines especially with fluids with a small degree of compressibility i.e. with liquids.
RSP-2009/0068A 2009-02-12 2009-02-12 Rotor blade for framed hydro and aero turbines RS20090068A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RSP-2009/0068A RS20090068A (en) 2009-02-12 2009-02-12 Rotor blade for framed hydro and aero turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RSP-2009/0068A RS20090068A (en) 2009-02-12 2009-02-12 Rotor blade for framed hydro and aero turbines

Publications (1)

Publication Number Publication Date
RS20090068A true RS20090068A (en) 2011-06-30

Family

ID=44212226

Family Applications (1)

Application Number Title Priority Date Filing Date
RSP-2009/0068A RS20090068A (en) 2009-02-12 2009-02-12 Rotor blade for framed hydro and aero turbines

Country Status (1)

Country Link
RS (1) RS20090068A (en)

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