ITTO20030702A1 - FIXED WING MICROVELIVEL - Google Patents

FIXED WING MICROVELIVEL

Info

Publication number
ITTO20030702A1
ITTO20030702A1 IT000702A ITTO20030702A ITTO20030702A1 IT TO20030702 A1 ITTO20030702 A1 IT TO20030702A1 IT 000702 A IT000702 A IT 000702A IT TO20030702 A ITTO20030702 A IT TO20030702A IT TO20030702 A1 ITTO20030702 A1 IT TO20030702A1
Authority
IT
Italy
Prior art keywords
microvelivel
fixed wing
wing
fixed
wing microvelivel
Prior art date
Application number
IT000702A
Other languages
Italian (it)
Inventor
Giorgio Guglieri
Barbara Pralio
Fulvia Quagliotti
Original Assignee
Torino Politecnico
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 Torino Politecnico filed Critical Torino Politecnico
Priority to IT000702A priority Critical patent/ITTO20030702A1/en
Priority to PCT/IB2004/002940 priority patent/WO2005025983A1/en
Publication of ITTO20030702A1 publication Critical patent/ITTO20030702A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/08—Stabilising surfaces mounted on, or supported by, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • 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
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/80—UAVs characterised by their small size, e.g. micro air vehicles [MAV]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/70—Constructional aspects of the UAV body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B64U2101/31—UAVs specially adapted for particular uses or applications for imaging, photography or videography for surveillance
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • 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)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Toys (AREA)
IT000702A 2003-09-15 2003-09-15 FIXED WING MICROVELIVEL ITTO20030702A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
IT000702A ITTO20030702A1 (en) 2003-09-15 2003-09-15 FIXED WING MICROVELIVEL
PCT/IB2004/002940 WO2005025983A1 (en) 2003-09-15 2004-09-10 Fixed wing micro aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT000702A ITTO20030702A1 (en) 2003-09-15 2003-09-15 FIXED WING MICROVELIVEL

Publications (1)

Publication Number Publication Date
ITTO20030702A1 true ITTO20030702A1 (en) 2005-03-16

Family

ID=34308152

Family Applications (1)

Application Number Title Priority Date Filing Date
IT000702A ITTO20030702A1 (en) 2003-09-15 2003-09-15 FIXED WING MICROVELIVEL

Country Status (2)

Country Link
IT (1) ITTO20030702A1 (en)
WO (1) WO2005025983A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL195977A (en) * 2008-12-16 2013-12-31 Abraham Abershitz Unmanned aerial vehicle having an improved aerodynamic configuration
JP2023504967A (en) * 2019-08-26 2023-02-08 ランドール エアロダイナミック エンジニアリング、グアンジョウ、エルエルシー Variable-span wings and related aircraft

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6565041B1 (en) * 2001-12-27 2003-05-20 Lockheed Martin Corporation Parachute assembly for a miniature aircraft

Also Published As

Publication number Publication date
WO2005025983A1 (en) 2005-03-24

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