BR102017026579A2 - remotely piloted aircraft - Google Patents
remotely piloted aircraftInfo
- 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
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.
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) |
-
2017
- 2017-12-08 BR BR102017026579A patent/BR102017026579A2/en not_active Application Discontinuation
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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 |