BR112023018255A2 - Configurações de fuselagem de aeronaves para deflexão para cima da fuselagem de ré - Google Patents
Configurações de fuselagem de aeronaves para deflexão para cima da fuselagem de réInfo
- Publication number
- BR112023018255A2 BR112023018255A2 BR112023018255A BR112023018255A BR112023018255A2 BR 112023018255 A2 BR112023018255 A2 BR 112023018255A2 BR 112023018255 A BR112023018255 A BR 112023018255A BR 112023018255 A BR112023018255 A BR 112023018255A BR 112023018255 A2 BR112023018255 A2 BR 112023018255A2
- Authority
- BR
- Brazil
- Prior art keywords
- fuselage
- frame section
- aircraft
- twisted
- configurations
- Prior art date
Links
- 230000007704 transition Effects 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
- B64C1/22—Other structures integral with fuselages to facilitate loading, e.g. cargo bays, cranes
-
- 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
- B64C1/061—Frames
-
- 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
- B64C1/18—Floors
- B64C1/20—Floors specially adapted for freight
-
- 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
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D13/00—Assembly, mounting or commissioning of wind motors; Arrangements specially adapted for transporting wind motor components
- F03D13/40—Arrangements or methods specially adapted for transporting wind motor components
-
- 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
- B64C2001/0045—Fuselages characterised by special shapes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/02—Transport, e.g. specific adaptations or devices for conveyance
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Tires In General (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
configurações de fuselagem de aeronaves para deflexão para cima da fuselagem de ré. é divulgada uma aeronave de carga de asa fixa tendo uma fuselagem torcida. a fuselagem contém um compartimento de carga interno contínuo e inclui uma porção dianteira, uma porção traseira e uma porção torcida formando uma junção na fuselagem entre as porções dianteira e traseira. a porção torcida contém uma região de transição do compartimento de carga e define uma curva entre uma linha central dianteira e uma linha central traseira. a porção torcida é formada por uma seção de quadro transversal dianteira, uma seção de quadro transversal traseira separada, e uma pluralidade de elementos de quadro longitudinais que se estendem entre as seções de quadro dianteira e traseira, o quadro dianteiro sendo acoplado a uma extremidade traseira da porção dianteira e a seção de quadro traseira sendo acoplada a uma extremidade dianteira da porção traseira de tal modo que a seção de quadro traseira seja angulada em relação à seção de quadro dianteira em torno de um eixo lateral da aeronave de carga.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2021/021792 WO2022191838A1 (en) | 2021-03-10 | 2021-03-10 | Aircraft fuselage configurations for upward deflection of aft fuselage |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112023018255A2 true BR112023018255A2 (pt) | 2024-01-16 |
Family
ID=83194580
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112023018255A BR112023018255A2 (pt) | 2021-03-10 | 2021-03-10 | Configurações de fuselagem de aeronaves para deflexão para cima da fuselagem de ré |
Country Status (7)
Country | Link |
---|---|
US (3) | US11492094B2 (pt) |
EP (1) | EP4304929A1 (pt) |
CN (1) | CN117279831A (pt) |
BR (1) | BR112023018255A2 (pt) |
CA (1) | CA3213158A1 (pt) |
IL (1) | IL305696A (pt) |
WO (1) | WO2022191838A1 (pt) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA3153557A1 (en) * | 2019-09-05 | 2021-03-11 | Zsm Holdings Llc | Aircraft fuselage configurations for avoiding tail strike while allowing long payloads |
WO2022093452A2 (en) | 2020-09-23 | 2022-05-05 | Zsm Holdings Llc | Ram air turbine installations for low speed flight |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2134260A (en) | 1935-09-07 | 1938-10-25 | James H Nickerson | Aeroplane construction |
US2383935A (en) * | 1943-06-23 | 1945-09-04 | Budd Edward G Mfg Co | Aircraft or like hollow body with external reinforcement therefor |
US2425972A (en) * | 1944-05-13 | 1947-08-19 | Budd Co | Aircraft construction for handling cargo |
US2425499A (en) * | 1945-03-02 | 1947-08-12 | Budd Co | Wing-body structure for airplanes |
US2942812A (en) * | 1958-05-28 | 1960-06-28 | Lockheed Aircraft Corp | Combined loading ramp and interior pressurization door for aircraft |
US2998948A (en) * | 1959-07-28 | 1961-09-05 | Harold D Sisk | Cargo-carrying aircraft |
US3374972A (en) * | 1965-09-27 | 1968-03-26 | Lockheed Aircraft Corp | Hinged end section for cargo aircraft |
GB1152982A (en) * | 1966-02-21 | 1969-05-21 | Short Brothers & Harland Ltd | Improvements in Anti-Drag Arrangements for Aerial Bodies, or Bodies intended for Movement partly in an Aerial Medium |
US3972427A (en) * | 1974-09-25 | 1976-08-03 | The Boeing Company | Appendant elevatable loader for vehicles |
US5069402A (en) * | 1990-04-06 | 1991-12-03 | Istar, Inc. | Alleviation of aircraft fuselage form drag |
US6845944B2 (en) | 2003-04-11 | 2005-01-25 | The Boeing Company | Multi-positional tail skids and associated methods of use |
DE10343627B4 (de) * | 2003-09-20 | 2014-03-06 | Eads Deutschland Gmbh | Verschlusselement für einen Bereich der Außenhaut eines Luftfahrzeugs |
US8708282B2 (en) * | 2004-11-23 | 2014-04-29 | Biosphere Aerospace, Llc | Method and system for loading and unloading cargo assembly onto and from an aircraft |
FR2925739B1 (fr) | 2007-12-20 | 2010-11-05 | Airbus France | Procede et dispositif de prevention des collisions au sol pour aeronefs. |
DE102009016769B4 (de) * | 2009-04-07 | 2015-10-29 | Airbus Operations Gmbh | Rumpfbugtor |
EP2889213A1 (en) * | 2013-12-30 | 2015-07-01 | Airbus Operations S.L. | Canard aircraft with rear loading |
US10093406B2 (en) * | 2014-12-10 | 2018-10-09 | The Boeing Company | Aircraft frame for tailstrike angle enhancement |
US10266267B2 (en) * | 2016-06-07 | 2019-04-23 | The Boeing Company | Systems and methods for in-flight retrieval of unmanned aerial vehicles |
US11667385B2 (en) | 2019-01-02 | 2023-06-06 | The Boeing Company | Cargo loading system for an aircraft and method of operating same |
CA3153557A1 (en) * | 2019-09-05 | 2021-03-11 | Zsm Holdings Llc | Aircraft fuselage configurations for avoiding tail strike while allowing long payloads |
WO2021046554A1 (en) * | 2019-09-05 | 2021-03-11 | Zsm Holdings Llc | Systems and methods for optimization of packaging large irregular payloads for shipment by air vehicles |
US11932374B2 (en) * | 2019-11-01 | 2024-03-19 | The Boeing Company | Freighter aircraft system and container system |
EP4062051A4 (en) * | 2019-11-22 | 2023-11-29 | ZSM Holdings LLC | SYSTEMS AND METHODS FOR OPTIMIZING THE PACKAGING OF LARGE IRREGULAR PAYLOADS SHIPPED BY AIR VEHICLES |
US20230046394A1 (en) * | 2021-06-29 | 2023-02-16 | The Boeing Company | Structural arrangement for strut-braced wing assembly of an aircraft |
-
2021
- 2021-03-10 BR BR112023018255A patent/BR112023018255A2/pt unknown
- 2021-03-10 CN CN202180098040.2A patent/CN117279831A/zh active Pending
- 2021-03-10 CA CA3213158A patent/CA3213158A1/en active Pending
- 2021-03-10 WO PCT/US2021/021792 patent/WO2022191838A1/en active Application Filing
- 2021-03-10 EP EP21930554.7A patent/EP4304929A1/en active Pending
- 2021-03-10 IL IL305696A patent/IL305696A/en unknown
- 2021-09-02 US US17/465,779 patent/US11492094B2/en active Active
-
2022
- 2022-11-07 US US17/981,805 patent/US11851156B2/en active Active
-
2023
- 2023-12-21 US US18/393,100 patent/US20240124119A1/en active Pending
Also Published As
Publication number | Publication date |
---|---|
US20230182885A1 (en) | 2023-06-15 |
WO2022191838A1 (en) | 2022-09-15 |
US20220289359A1 (en) | 2022-09-15 |
CN117279831A (zh) | 2023-12-22 |
US20240124119A1 (en) | 2024-04-18 |
CA3213158A1 (en) | 2022-09-15 |
US11492094B2 (en) | 2022-11-08 |
US11851156B2 (en) | 2023-12-26 |
EP4304929A1 (en) | 2024-01-17 |
IL305696A (en) | 2023-11-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112023018255A2 (pt) | Configurações de fuselagem de aeronaves para deflexão para cima da fuselagem de ré | |
BR112022004138A2 (pt) | Configurações de fuselagem de aeronave para evitar batida de cauda ao permitir cargas úteis longas | |
BRPI0520435B8 (pt) | artigo absorvente com ajuste melhorado | |
BR112019023921A2 (pt) | artigo absorvente | |
PE20220032A1 (es) | Caracteristicas de estabilidad en un montaje de miembros de desgaste | |
BRPI0520434B8 (pt) | artigo absorvente com ajuste aperfeiçoado | |
BR112018075840A2 (pt) | peça de extremidade de conexão para uma linha flexível, linha flexível e método para montar uma peça de extremidade de conexão para uma linha flexível | |
BR112016001762A2 (pt) | construção de cobertura de corpo para uma mo-tocicleta | |
FR2884802B1 (fr) | Structure porteuse et aeronef a voilure tournante | |
PH12018550051A1 (en) | Absorbent article | |
BR112017002081B1 (pt) | Elemento de superfície de controle para uma aeronave | |
BR112021006311A2 (pt) | aeronave de pouso e decolagem curtos e verticais (vstol) | |
BR112017024549A2 (pt) | artigo absorvente | |
PE20150786A1 (es) | Estructura de luz trasera para un vehiculo | |
BR112016026077A8 (pt) | núcleo absorvente e processo para a produção de núcleo absorvente | |
CO2021006995A2 (es) | Artículo de higiene desechable con ajuste mejorado | |
BR112022006738A2 (pt) | Ônibus de piso baixo | |
BR112018073901A2 (pt) | cabeça extrusora e método para extrudar extrudado reforçado por cabo | |
BR112023018269A2 (pt) | Projetos de aeronave de carga de asa fixa de baixa densidade para transporte não flutuante encerrado de componentes de turbina eólica | |
RU2009128678A (ru) | Фюзеляж летательного аппарата | |
BR102019003004A8 (pt) | Porção de aeronave e aeronave | |
BR112012023770A2 (pt) | meia estrutura de suporte para uma nacela de motor de avião e neacela para um motor de avião | |
BR112017016770A2 (pt) | estrutura de extremidade traseira de veículo | |
BR112013026820A2 (pt) | quadro para motocicleta | |
ECSP22052493A (es) | Un artículo sanitario empaquetado de manera individual |