GR1008767B - Method to prevent aircraft stalling - anti-stall equipment - Google Patents

Method to prevent aircraft stalling - anti-stall equipment

Info

Publication number
GR1008767B
GR1008767B GR20150100007A GR20150100007A GR1008767B GR 1008767 B GR1008767 B GR 1008767B GR 20150100007 A GR20150100007 A GR 20150100007A GR 20150100007 A GR20150100007 A GR 20150100007A GR 1008767 B GR1008767 B GR 1008767B
Authority
GR
Greece
Prior art keywords
wings
air flow
aircraft
stalling
smooth
Prior art date
Application number
GR20150100007A
Other languages
Greek (el)
Inventor
Κωνσταντινος Θεοδωρου Καστανας
Original Assignee
Κωνσταντινος Θεοδωρου Καστανας
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 Κωνσταντινος Θεοδωρου Καστανας filed Critical Κωνσταντινος Θεοδωρου Καστανας
Priority to GR20150100007A priority Critical patent/GR1008767B/en
Priority to PCT/GR2016/000001 priority patent/WO2016113579A1/en
Publication of GR1008767B publication Critical patent/GR1008767B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/08—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • 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)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Traffic Control Systems (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Method of prevention-avoiding aircraft roaming situation stalling (Anti stall equipment) mostly due to bad weather conditions and minimizing cruising speed, by placing a device that is able to produce and deliver continuously the appropriate amount of smooth air flow to the upper part of the wings and at the junction of the root of the wings with the main body of the aircraft, capable to replacethe possible turbulent air flow accompanying the detachment molecules from the wings of the aircraft with smooth analogue like thus avoiding roaming in a stalling situation. The device shall be connected to the proper air flow detector and even to the weather detector which already exists on advanced aircrafts and whenever required, it will be activated and will produce the appropriate amount of smooth air flow that of similar density and speed for each time required to maintain the necessary lift regardless of variable weather conditions or other phenomena and discussed above and eventually channel it at the upper part of the wings.
GR20150100007A 2015-01-12 2015-01-12 Method to prevent aircraft stalling - anti-stall equipment GR1008767B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GR20150100007A GR1008767B (en) 2015-01-12 2015-01-12 Method to prevent aircraft stalling - anti-stall equipment
PCT/GR2016/000001 WO2016113579A1 (en) 2015-01-12 2016-01-08 Method to prevent aircraft stalling - anti stall equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GR20150100007A GR1008767B (en) 2015-01-12 2015-01-12 Method to prevent aircraft stalling - anti-stall equipment

Publications (1)

Publication Number Publication Date
GR1008767B true GR1008767B (en) 2016-05-13

Family

ID=55453215

Family Applications (1)

Application Number Title Priority Date Filing Date
GR20150100007A GR1008767B (en) 2015-01-12 2015-01-12 Method to prevent aircraft stalling - anti-stall equipment

Country Status (2)

Country Link
GR (1) GR1008767B (en)
WO (1) WO2016113579A1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3480234A (en) * 1967-08-18 1969-11-25 Lockheed Aircraft Corp Method and apparatus for modifying airfoil fluid flow
US3779199A (en) * 1969-09-25 1973-12-18 R Mayer Boundary layer control means
US5255881A (en) * 1992-03-25 1993-10-26 Vigyan, Inc. Lift augmentation for highly swept wing aircraft
US7874525B2 (en) * 2006-05-04 2011-01-25 Lockheed Martin Corporation Method and system for fully fixed vehicle control surfaces

Also Published As

Publication number Publication date
WO2016113579A1 (en) 2016-07-21

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Legal Events

Date Code Title Description
PG Patent granted

Effective date: 20160628