[go: up one dir, main page]

PL398465A1 - Platform of constant cross-section, flying on the basis of air turbulence - Google Patents

Platform of constant cross-section, flying on the basis of air turbulence

Info

Publication number
PL398465A1
PL398465A1 PL398465A PL39846512A PL398465A1 PL 398465 A1 PL398465 A1 PL 398465A1 PL 398465 A PL398465 A PL 398465A PL 39846512 A PL39846512 A PL 39846512A PL 398465 A1 PL398465 A1 PL 398465A1
Authority
PL
Poland
Prior art keywords
section
constant cross
flying
platform
basis
Prior art date
Application number
PL398465A
Other languages
Polish (pl)
Inventor
Tadeusz Dobrocinski
Original Assignee
Bizgate-Aviation Spólka Z Ograniczona Odpowiedzialnoscia
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 Bizgate-Aviation Spólka Z Ograniczona Odpowiedzialnoscia filed Critical Bizgate-Aviation Spólka Z Ograniczona Odpowiedzialnoscia
Priority to PL398465A priority Critical patent/PL398465A1/en
Priority to PCT/PL2013/000029 priority patent/WO2013137754A1/en
Publication of PL398465A1 publication Critical patent/PL398465A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/144—Aerofoil profile including a flat surface on either the extrados or intrados
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Platforma latajaca charakteryzuje sie tym, ze posiada ksztalt kwadratu, rombu lub innej figury geometrycznej o stalym przekroju poprzecznym oraz kacie krawedzi natarcia zmieniajacym sie od 1° do 89°, zapewniajac utrzymywanie sie w powietrzu przy dowolnej predkosci.The flying platform is characterized by the fact that it has a square, diamond or other geometric shape with a constant cross-section and the leading edge angle varying from 1 ° to 89 °, ensuring it floats in the air at any speed.

PL398465A 2012-03-15 2012-03-15 Platform of constant cross-section, flying on the basis of air turbulence PL398465A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL398465A PL398465A1 (en) 2012-03-15 2012-03-15 Platform of constant cross-section, flying on the basis of air turbulence
PCT/PL2013/000029 WO2013137754A1 (en) 2012-03-15 2013-03-11 Flying platform with constant cross - section profile for exploiting air turbulences phenomenon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL398465A PL398465A1 (en) 2012-03-15 2012-03-15 Platform of constant cross-section, flying on the basis of air turbulence

Publications (1)

Publication Number Publication Date
PL398465A1 true PL398465A1 (en) 2013-09-16

Family

ID=48225104

Family Applications (1)

Application Number Title Priority Date Filing Date
PL398465A PL398465A1 (en) 2012-03-15 2012-03-15 Platform of constant cross-section, flying on the basis of air turbulence

Country Status (2)

Country Link
PL (1) PL398465A1 (en)
WO (1) WO2013137754A1 (en)

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1924996A (en) * 1929-11-16 1933-08-29 Langguth Wilhelm Tailless airplane
US3785595A (en) 1972-11-13 1974-01-15 Us Navy System for sensing and compensating for the disturbance forces on a spacecraft
US4015787A (en) 1975-11-17 1977-04-05 Fairchild Industries Inc. Aircraft wing
BE837212A (en) * 1975-12-31 1976-04-16 DIAMOND HOLDER FOR PROTECTION OF DECORATIVE DIAMONDS IN THEIR PACKAGING IN BATCH LETTERS
US4180221A (en) * 1978-01-16 1979-12-25 Harris Donald E Self propelled kite
US4742977A (en) * 1986-11-03 1988-05-10 Crowell Robert L Wing structure with self-induced camber
PL340469A1 (en) 2000-05-31 2001-12-03 Stanislaw Salnik Aerodynamic lift increasing apparatus
US6923403B1 (en) 2004-03-18 2005-08-02 Faruk Dizdarevic Tailed flying wing aircraft
NO325284B1 (en) * 2007-02-13 2008-03-17 Proxflyer As Flight direction control system
GB2492501B (en) * 2012-10-10 2013-05-22 Thales Holdings Uk Plc Air vehicle with rotatable wing

Also Published As

Publication number Publication date
WO2013137754A1 (en) 2013-09-19

Similar Documents

Publication Publication Date Title
EP2941754A4 (en) EVALUATION OF THE IMPACT ON SOCIAL MEDIA
DK3514371T3 (en) Wind turbine blade fitted with surface mounted device
PT3066201T (en) METHODS AND COMPOSITIONS RELATED TO CRISPR WITH REGULATORY RANGES
KR101815588B9 (en) Perovskite nanocrystal particles and optoelectronic devices using the same
AU365025S (en) Portable device
FR3022218B1 (en) AIRCRAFT NACELLE COMPRISING AN ENHANCED AIR INTAKE
PL3495473T3 (en) The method of hydrolytic cleavage of zearalenone and / or zearalenone derivatives with the polypeptide and its use
AU358420S (en) Hammer
FR3005453B1 (en) AIRCRAFT TURBO BOILER NACELLE
FR3017695B3 (en) AIR PURIFIER DEVICE
AU201612395S (en) Jet Regulator with Flow Regulator
FR3005684B1 (en) PROPELLER BLADE PIVOT
ZA201703152B (en) Method of calculating the surface speed of at least one ship and method for deduction of each vector derived at any point of the trajectory of said ship
MA40852A (en) WIND TURBINE BLADE WITH A SURFACE MOUNTED DEVICE
SI3330213T1 (en) UPPER FLIGHT AND LOWER FLIGHT AIRCRAFT
FR3029171B1 (en) AIRCRAFT TURBOMACHINE HAVING A VARIABLE SECTION AIR INTAKE
FR3016671B1 (en) OIL DISTRIBUTION DEVICE WITH ANTI-RETURN VALVE
AU359388S (en) Air conditioner
Kang et al. Boundary regularity criteria for suitable weak solutions of the magnetohydrodynamic equations
FR3012113B1 (en) ANTI-REGEL DEVICE FOR AIRCRAFT BLADES
FR3017708B1 (en) ACOUSTIC MEASURING DEVICE IN AIR FLOW
PL398465A1 (en) Platform of constant cross-section, flying on the basis of air turbulence
AU360282S (en) Hammer
PL2992295T3 (en) The device and method of classification of a food object with mature or irregular structure
EP3524528A4 (en) AIRCRAFT CARRIAGE IN NEAR SPACE

Legal Events

Date Code Title Description
REFS Decisions on refusal to grant patents (taken after the publication of the particulars of the applications)