BR0110056A - Aeronave estratosférica movida a hidrogênio lìquido, sua asa, sistema de energia e método para o fornecimento de um reagente gasoso a uma célula de combustìvel numa taxa de fluxo de funcionamento desejada - Google Patents
Aeronave estratosférica movida a hidrogênio lìquido, sua asa, sistema de energia e método para o fornecimento de um reagente gasoso a uma célula de combustìvel numa taxa de fluxo de funcionamento desejadaInfo
- Publication number
- BR0110056A BR0110056A BR0110056-4A BR0110056A BR0110056A BR 0110056 A BR0110056 A BR 0110056A BR 0110056 A BR0110056 A BR 0110056A BR 0110056 A BR0110056 A BR 0110056A
- Authority
- BR
- Brazil
- Prior art keywords
- wing
- aircraft
- fuel cell
- fuel
- liquid hydrogen
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title abstract 6
- 239000007788 liquid Substances 0.000 title abstract 3
- 239000003153 chemical reaction reagent Substances 0.000 title abstract 2
- 238000000034 method Methods 0.000 title abstract 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical class [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 abstract 3
- 239000001257 hydrogen Substances 0.000 abstract 3
- 229910052739 hydrogen Inorganic materials 0.000 abstract 3
- 239000002828 fuel tank Substances 0.000 abstract 2
- 238000009835 boiling Methods 0.000 abstract 1
- 230000011514 reflex Effects 0.000 abstract 1
Classifications
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- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/10—Shape of wings
- B64C3/14—Aerofoil profile
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
- B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/30—Fuel systems for specific fuels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/32—Supply or distribution of electrical power generated by fuel cells
-
- 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
- B64D41/00—Power installations for auxiliary purposes
- B64D2041/005—Fuel cells
-
- 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
- B64U2101/20—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
-
- 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
-
- 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
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/60—Take-off or landing of UAVs from a runway using their own power
-
- 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
-
- 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
- Y02T50/30—Wing lift efficiency
-
- 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
- Y02T50/40—Weight reduction
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Combustion & Propulsion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Remote Sensing (AREA)
- Fuel Cell (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Tires In General (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Steroid Compounds (AREA)
- Physical Water Treatments (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
"AERONAVE ESTRATOSFéRICA MOVIDA A HIDROGêNIO LìQUIDO, SUA ASA, SISTEMA DE ENERGIA E MéTODO PARA O FORNECIMENTO DE UM REAGENTE GASOSO A UMA CéLULA DE COMBUSTìVEL TAXA DE FLUXO DE FUNCIONAMENTO DESEJADA". Apresenta-se uma aeronave, configurada para apresentar uma ampla gama de velocidades de vóo, consumindo baixos níveis de energia durante um período de tempo extenso, suportando concomitantemente uma plataforma para comunicações com uma vista para baixo desobstruída. A referida aeronave inclui uma lâmina extensível no bordo de ataque da asa, e um bordo de fuga reflexo. A aeronave compreende uma asa voadora estendendo-se lateralmente entre duas extremidades e um ponto central. A asa é inclinada e apresenta uma corda relativamente constante. A aeronave inclui também um módulo de energia configurado para proporcionar energia por meio de uma célula de combustível. A célula de combustível armazena hidrogênio líquido como combustível, porém utiliza hidrogênio gasoso na célula de combustível. Um aquecedor do tanque de combustível é utilizado para controlar a taxa de ebulição do combustível dentro do tanque de combustível. A aeronave da presente invenção inclui uma estrutura de suporte incluindo um conjunto de suportes, na qual os suportes formam um tetraedro que fica fixado à asa.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US19413700P | 2000-04-03 | 2000-04-03 | |
US24171300P | 2000-10-18 | 2000-10-18 | |
PCT/US2001/010876 WO2001076941A2 (en) | 2000-04-03 | 2001-04-03 | Liquid hydrogen stratospheric aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0110056A true BR0110056A (pt) | 2003-12-30 |
Family
ID=26889719
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0110056-4A BR0110056A (pt) | 2000-04-03 | 2001-04-03 | Aeronave estratosférica movida a hidrogênio lìquido, sua asa, sistema de energia e método para o fornecimento de um reagente gasoso a uma célula de combustìvel numa taxa de fluxo de funcionamento desejada |
Country Status (11)
Country | Link |
---|---|
US (3) | US6550717B2 (pt) |
EP (1) | EP1280700A2 (pt) |
JP (2) | JP4349771B2 (pt) |
KR (1) | KR100807036B1 (pt) |
CN (1) | CN1429165A (pt) |
AU (1) | AU2001276816A1 (pt) |
BR (1) | BR0110056A (pt) |
CA (2) | CA2403269C (pt) |
CZ (1) | CZ20023274A3 (pt) |
MX (1) | MXPA02009089A (pt) |
WO (1) | WO2001076941A2 (pt) |
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-
2001
- 2001-04-03 EP EP01954575A patent/EP1280700A2/en not_active Withdrawn
- 2001-04-03 CN CN01807471A patent/CN1429165A/zh active Pending
- 2001-04-03 WO PCT/US2001/010876 patent/WO2001076941A2/en not_active Application Discontinuation
- 2001-04-03 JP JP2001574429A patent/JP4349771B2/ja not_active Expired - Fee Related
- 2001-04-03 CA CA2403269A patent/CA2403269C/en not_active Expired - Fee Related
- 2001-04-03 US US09/826,424 patent/US6550717B2/en not_active Expired - Lifetime
- 2001-04-03 CA CA2647011A patent/CA2647011C/en not_active Expired - Fee Related
- 2001-04-03 MX MXPA02009089A patent/MXPA02009089A/es unknown
- 2001-04-03 KR KR1020027013167A patent/KR100807036B1/ko not_active IP Right Cessation
- 2001-04-03 CZ CZ20023274A patent/CZ20023274A3/cs unknown
- 2001-04-03 BR BR0110056-4A patent/BR0110056A/pt not_active Application Discontinuation
- 2001-04-03 AU AU2001276816A patent/AU2001276816A1/en not_active Abandoned
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2002
- 2002-02-11 US US10/073,518 patent/US20020070312A1/en not_active Abandoned
- 2002-02-11 US US10/073,828 patent/US20020070313A1/en not_active Abandoned
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2009
- 2009-05-21 JP JP2009122714A patent/JP5123249B2/ja not_active Expired - Fee Related
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CA2403269A1 (en) | 2001-10-18 |
WO2001076941A2 (en) | 2001-10-18 |
KR100807036B1 (ko) | 2008-02-25 |
CA2647011C (en) | 2011-04-05 |
CA2403269C (en) | 2010-06-15 |
JP4349771B2 (ja) | 2009-10-21 |
MXPA02009089A (es) | 2005-07-01 |
WO2001076941A9 (en) | 2002-12-27 |
US20020070313A1 (en) | 2002-06-13 |
EP1280700A2 (en) | 2003-02-05 |
JP2009179321A (ja) | 2009-08-13 |
CN1429165A (zh) | 2003-07-09 |
CA2647011A1 (en) | 2001-10-18 |
JP5123249B2 (ja) | 2013-01-23 |
US20020070312A1 (en) | 2002-06-13 |
JP2003530268A (ja) | 2003-10-14 |
WO2001076941A3 (en) | 2002-05-30 |
AU2001276816A1 (en) | 2001-10-23 |
CZ20023274A3 (cs) | 2003-03-12 |
US6550717B2 (en) | 2003-04-22 |
US20020005454A1 (en) | 2002-01-17 |
KR20020093883A (ko) | 2002-12-16 |
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