BR112018015818A2 - aeronave, conjunto de treinamento de aeronave, e, método para reconfigurar uma aeronave. - Google Patents
aeronave, conjunto de treinamento de aeronave, e, método para reconfigurar uma aeronave.Info
- Publication number
- BR112018015818A2 BR112018015818A2 BR112018015818-6A BR112018015818A BR112018015818A2 BR 112018015818 A2 BR112018015818 A2 BR 112018015818A2 BR 112018015818 A BR112018015818 A BR 112018015818A BR 112018015818 A2 BR112018015818 A2 BR 112018015818A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- fuselage
- handling
- engine
- changed
- Prior art date
Links
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 230000005484 gravity Effects 0.000 abstract 1
- 238000009434 installation Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
- B64C1/069—Joining arrangements therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/26—Attaching the wing or tail units or stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2211/00—Modular constructions of airplanes or helicopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0253—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0273—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for jet engines
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
- Tires In General (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
a presente invenção visa a fornecer uma aeronave a jato de treinamento modular (1) que pode ser reconfigurada para fornecer uma pluralidade de aeronaves de manuseios diferentes que serão particularmente benéficas para o treinamento de pilotos. por exemplo, a presente invenção fornece uma estrutura de base em que elementos podem ser mudados a fim de alterar as capacidades de manuseio, manobra e potência da aeronave. a aeronave pode ter uma primeira configuração básica (1) que permite que um piloto aprenda habilidades de manuseio relativamente básicas. o sistema de propulsões e/ou estruturas de asas podem, então, ser mudados para fornecer uma aeronave (11) com manuseio mais sofisticado e maior capacidade de potência. a invenção envolve o motor (17) localizado totalmente no exterior da estrutura de fuselagem (14) enquanto ainda é posicionado na linha central da fuselagem (14) e a linha de tração de motor direcionada através do centro da fuselagem e próximo ao centro de gravidade da aeronave. alcançando-se isso, o projeto dispendioso da fuselagem como estrutura primária ou em condições de voo críticas pode ser concluído independentemente da instalação do motor.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1602059.6 | 2016-02-04 | ||
GB1602059.6A GB2547020A (en) | 2016-02-04 | 2016-02-04 | Design relating to improving aircraft |
PCT/GB2017/050280 WO2017134459A1 (en) | 2016-02-04 | 2017-02-03 | Modular aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112018015818A2 true BR112018015818A2 (pt) | 2018-12-26 |
BR112018015818B1 BR112018015818B1 (pt) | 2024-05-28 |
Family
ID=
Also Published As
Publication number | Publication date |
---|---|
US20190039717A1 (en) | 2019-02-07 |
WO2017134459A1 (en) | 2017-08-10 |
EP3411293A1 (en) | 2018-12-12 |
GB2547020A (en) | 2017-08-09 |
KR20180113550A (ko) | 2018-10-16 |
AU2017215294B2 (en) | 2022-04-07 |
PL3411293T3 (pl) | 2022-01-03 |
ES2895276T3 (es) | 2022-02-18 |
CA3012237A1 (en) | 2017-08-10 |
JP2019503935A (ja) | 2019-02-14 |
US10988232B2 (en) | 2021-04-27 |
AU2017215294A1 (en) | 2018-09-20 |
EP3411293B1 (en) | 2021-07-28 |
GB201602059D0 (en) | 2016-03-23 |
JP6954575B2 (ja) | 2021-10-27 |
ZA201806368B (en) | 2019-11-27 |
IL260736B (en) | 2021-10-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112018073801A2 (pt) | aeronave elétrica pilotada automaticamente para executar decolagens e aterrissagens verticais e método para controlar uma aeronave | |
BR112017004139A2 (pt) | multi-rotor com asa inclinada | |
WO2017123346A3 (en) | Uav with wing-plate assemblies providing efficient vertical takeoff and landing capability | |
WO2016060827A3 (en) | Translation thrust system engagement and disengagment for rotary wing aircraft | |
NZ742223A (en) | Vertical takeoff and landing aircraft | |
BR112018009344A2 (pt) | veículo aéreo com componentes desdobráveis | |
CL2018003108A1 (es) | Métodos de reparación de alas de aeronaves y bujes consumibles para su utilización con ellos | |
WO2016003530A3 (en) | Vertical takeoff and landing (vtol) unmanned aerial vehicle (uav) | |
WO2016109003A3 (en) | Delta fuselage for vertical take-off and landing (vtol) aircraft | |
BR112015014692A2 (pt) | dispositivo auxiliar de aeronave voando em elevada altitude | |
BR112015025778A2 (pt) | hangar subterrâneo para helicópteros. | |
BR112018015818A2 (pt) | aeronave, conjunto de treinamento de aeronave, e, método para reconfigurar uma aeronave. | |
Szabolcsi | A new approach of certification of the airworthiness of the UAV automatic flight control systems | |
RU2013115878A (ru) | Способ управления, стабилизации и создания дополнительной подъемной силы дирижабля | |
ES2547361R1 (es) | Helicóptero con estructura de aletas en radio de palanca y aletas en las hélices | |
WO2013107946A3 (fr) | Aeronef | |
WO2016200458A3 (en) | Mono-cyclic swashplate | |
AR088412A1 (es) | Sistema de propulsion para un avion, que disminuye, cancela o invierte el vortice de extremo de las alas | |
Wilson et al. | Managing Risk: best practices for pilots | |
Сошин | Technical maintenance of aircraft and aircraft engines | |
RU2016116178A (ru) | Способ вертикального перемещения и зависания самолета в воздухе | |
Baida | FOREIGN LANGUAGES FOR SPECIFIC PURPOSES | |
Kozuba et al. | Human factor in relation to flight safety | |
van Niekerk | The Cost of Knowledge | |
RU2015135410A (ru) | Винтомоторный самолёт вертикального взлёта |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B350 | Update of information on the portal [chapter 15.35 patent gazette] | ||
B06W | Patent application suspended after preliminary examination (for patents with searches from other patent authorities) chapter 6.23 patent gazette] | ||
B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 03/02/2017, OBSERVADAS AS CONDICOES LEGAIS |