BR102017026579A2 - remotely piloted aircraft - Google Patents

remotely piloted aircraft

Info

Publication number
BR102017026579A2
BR102017026579A2 BR102017026579A BR102017026579A BR102017026579A2 BR 102017026579 A2 BR102017026579 A2 BR 102017026579A2 BR 102017026579 A BR102017026579 A BR 102017026579A BR 102017026579 A BR102017026579 A BR 102017026579A BR 102017026579 A2 BR102017026579 A2 BR 102017026579A2
Authority
BR
Brazil
Prior art keywords
remotely piloted
piloted aircraft
arp
fixed wing
configuration
Prior art date
Application number
BR102017026579A
Other languages
Portuguese (pt)
Inventor
Giglio Rodrigues Tiago
Original Assignee
Giglio Rodrigues Tiago
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 Giglio Rodrigues Tiago filed Critical Giglio Rodrigues Tiago
Priority to BR102017026579A priority Critical patent/BR102017026579A2/en
Priority to PCT/BR2018/050227 priority patent/WO2019010554A1/en
Publication of BR102017026579A2 publication Critical patent/BR102017026579A2/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft
    • B64C2039/105—All-wing aircraft of blended wing body type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

?aeronave remotamente pilotada?, compreendendo uma aeronave remotamente pilotada ? arp, dotada de partes e peças que permitem sua utilização em configurações distintas, sendo uma configuração de asa fixa, uma configuração de asa fixa vtol e uma configuração multirotor; sendo, ainda, a referida arp dotada de exclusivo e inovador sistema de compensação de centro de gravidade através de nariz e cauda contendo comprimento variável, capacidade de reposicionamento de massas no interior da fuselagem e prevendo momentos de força previamente calculados."remotely piloted aircraft" comprising a remotely piloted aircraft? arp, provided with parts and pieces that allow its use in different configurations, being a fixed wing configuration, a vtol fixed wing configuration and a multi-motor configuration; said arp having a unique and innovative center of gravity compensation system through nose and tail containing variable length, mass repositioning capability within the fuselage and providing previously calculated moments of force.

BR102017026579A 2017-07-10 2017-12-08 remotely piloted aircraft BR102017026579A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
BR102017026579A BR102017026579A2 (en) 2017-12-08 2017-12-08 remotely piloted aircraft
PCT/BR2018/050227 WO2019010554A1 (en) 2017-07-10 2018-07-06 Remotely piloted aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BR102017026579A BR102017026579A2 (en) 2017-12-08 2017-12-08 remotely piloted aircraft

Publications (1)

Publication Number Publication Date
BR102017026579A2 true BR102017026579A2 (en) 2019-06-18

Family

ID=67260840

Family Applications (1)

Application Number Title Priority Date Filing Date
BR102017026579A BR102017026579A2 (en) 2017-07-10 2017-12-08 remotely piloted aircraft

Country Status (1)

Country Link
BR (1) BR102017026579A2 (en)

Similar Documents

Publication Publication Date Title
IL274349A (en) Vtol aircraft having fixed-wing and rotorcraft configurations
IL266371A (en) Vtol aircraft using rotors to simulate rigid wing aero dynamics
EP3615420A4 (en) Vertical takeoff and landing airframe
EP3630601A4 (en) Auxiliary power system for rotorcraft with folding propeller arms and crumple zone landing gear
SG11201910744WA (en) Vertical take-off and landing unmanned aerial vehicle having foldable fixed wing and based on twin-ducted fan power system
EP3492377A4 (en) Vertical take-off and landing aircraft
PL3172130T3 (en) Aircraft with wing-borne flight mode and hover flight mode
EP3366585A4 (en) Vertical take-off and landing aircraft
EP3583027A4 (en) Vertical takeoff and landing light aircraft
EP3556939A4 (en) Drone takeoff and landing system
EP3760540A4 (en) Double-ring rotating wing spherical cabin aircraft
SG11202009516PA (en) Uav with frangible airframe structures
GB201617308D0 (en) Aircraft wing with aileron
EP3609783A4 (en) Vertical takeoff and landing aircraft
IL259600A (en) Simple pitch control device for dual-mode aircraft with vtol and fixed-wing flight
MA53107A (en) AIRCRAFT WING
GB201717994D0 (en) Aircraft wing and wing tip device with fairing
PL3059157T3 (en) Rotorcraft with cowling able to rotate and translate relative to the fuselage
HRP20200052T1 (en) Fastening system for attaching insulating boards or similar insulating material to a supporting base
FR3030442B1 (en) FRONT AIRCRAFT TIP EQUIPPED WITH A JUNCTION FRAME BETWEEN THE LANDING TRAIN BOX AND THE EXTERNAL SKIN OF THE FUSELAGE
FR3021625B1 (en) FLEXIBLE CONNECTION BETWEEN THE FLOOR STRUCTURE AND THE HULL STRUCTURE OF AN AIRCRAFT.
EP3434591A4 (en) Vertical takeoff and landing aircraft
EP3674212A4 (en) High-speed flying method and ring wing aircraft
BR102017026579A2 (en) remotely piloted aircraft
GB201719583D0 (en) Modifying the chord length of an aircraft wing

Legal Events

Date Code Title Description
B11K Dismissal acc. art. 17, par 2 of ipl - pending earlier application (priority claim) definitively shelved

Free format text: PRIORIDADE INTERNA DO BR102018013794-8 DE 05/07/2018.

B03F Publication of an application: publication of application definitely dismissed - article 216, par 2 and article 17, par 2 of industr. prop. law