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특허 상세정보

Independent power generation in aircraft

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-041/00   
미국특허분류(USC) 244/058; 244/134D; 290/007
출원번호 US-0056568 (2013-10-17)
등록번호 US-8950703 (2015-02-10)
발명자 / 주소
  • Bayliss, Andrew J.
  • Paterson, John T.
  • Retz, Kevin
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Toler Law Group, PC
인용정보 피인용 횟수 : 7  인용 특허 : 121
초록

A method includes generating thrust at one or more engines of an aircraft. The method includes generating first electricity at a first power unit concurrently with generating second electricity at a second power unit. The first power unit and the second power unit are independent of the one or more engines of the aircraft. The first electricity has a first set of electrical characteristics and the second electricity has a second set of electrical characteristics, where the first set of electrical characteristics is different than the second set of electr...

대표
청구항

1. A method comprising: generating thrust at one or more engines of an aircraft;generating first electricity at a first power unit that is independent of the one or more engines of the aircraft, the first electricity having a first set of electrical characteristics;concurrently with generating the first electricity, generating second electricity at a second power unit that is independent of the one or more engines of the aircraft, the second electricity having a second set of electrical characteristics, wherein the first set of electrical characteristics...

이 특허에 인용된 특허 (121)

  1. Cronin Michael J. (Sherman Oaks CA), AC Motor-starting for aircraft engines using APU free turbine driven generators.
  2. Moffat, George H.; Stubbs, Gene Woodard; Voll, William Albert, Acoustic muffler for turbine engine.
  3. Cicon Dennis E. (Manchester CT), Acoustic treated exhaust plug for turbine engine.
  4. Teraoka Masao (Tochigi-ken JPX), Air conditioning system.
  5. Schorn, Juergen, Air feeding system for an internal-combustion engine.
  6. Albero, Jose; Lents, Charles E.; Sahm, Michael K.; Welch, Richard C., Aircraft architecture with a reduced bleed aircraft secondary power system.
  7. Bescoby Frank A. (Rancho Palos Verdes CA) Araki Roy T. (Redondo Beach CA), Aircraft cabin air conditioning system with improved fresh air supply.
  8. Horstman Raymond H. (Auburn WA) Monda Damian G. (Seattle WA) Peash Douglas E. (Enumclaw WA) Yorozu Arthur S. (Seattle WA), Aircraft cabin ventilation system.
  9. Bernier, Alan T., Aircraft electrical power distribution network.
  10. Latos Thomas S. ; Nelson Jeffrey D. ; Dickes Gary E., Aircraft electrical system providing emergency power and electric starting of propulsion engines.
  11. William H. Hogeboom ; Gerald W. Bielak, Aircraft engine acoustic liner and method of making the same.
  12. Christoff William J. (Thousand Oaks CA), Aircraft environmental control system with auxiliary power output.
  13. Zywiak, Thomas; Bruno, Louis J.; Drew, Diane; Christians, Douglas L., Aircraft galley chiller system.
  14. Zywiak,Thomas; Bruno,Louis J.; Drew,Diane; Christians,Douglas L., Aircraft galley chiller system.
  15. Nozari Farhad, Aircraft hydraulic pump control system.
  16. Gregory Earl M. (Centerville OH) Tschantz James S. (Bellbrook OH), Aircraft power unit with elective mechanical coupling.
  17. Glennon Timonthy F., Aircraft secondary power system.
  18. Cronin Michael J. (Sherman Oaks CA), All electric environmental control system for advanced transport aircraft.
  19. Hoffjann,Claus; Schuldzig,Hansgeorg; Heinrich,Hans Juergen, Arrangement and method for the generation of water on board an aircraft.
  20. Nguyen,Phuong H.; Sikora,Joseph A.; Campbell,Thomas A., Automatic control systems for aircraft auxiliary power units, and associated methods.
  21. Turner William W., Automatic generator start up and shut off device.
  22. Hoag Michael S. ; Plank Steven K., Auxiliary power unit passive cooling system.
  23. Krebs Mark E. (Chardon OH), Bottoming cycle.
  24. Tolman Alan G. (Phoenix AZ), Broad band acoustic attenuator.
  25. Zywiak,Thomas; Bruno,Louis J., Cabin air conditioning system with liquid cooling for power electronics.
  26. Ross David F. (Scottsdale AZ) Lyon Craig A. (Mesa AZ), Compact muffler apparatus and associated methods.
  27. Faulkner Dennis T. (Rockford IL) Glennon Timothy F. (Rockford IL) Markunas Albert L. (Roscoe IL), Compressor load control for an auxiliary power unit.
  28. Castelli Vittorio (Scottsdale NY) Chai Stephen T. (Carson CA), Contaminant trapping in rotating disk devices.
  29. Suttie, Peter; Schmidt, Dennis E.; Mehrer, Michael E.; Mack, Tarrence LaMar, Control system for an auxiliary power unit.
  30. Baker Roy S. (Rockford IL) Nuechterlein Paul E. (Rockford IL), Converter enhanced variable frequency power bus architecture.
  31. Wright,Kevin P.; Lombardi,Steven A., Decentralized energy demand management.
  32. Liston Laurence D. N. ; Schoepf Joseph L., Detachable integral aircraft tailcone and power assembly.
  33. Liston Laurence D. N. ; Schoepf Joseph L. ; Royalty Charles Michael, Detachable integral aircraft tailcone and power assembly.
  34. Liston Laurence D. N. ; Schoepf Joseph L. ; Royalty Charles Michael, Detachable integral aircraft tailcone and power assembly.
  35. Chang, Jie; LeMond, Charles H.; Wang, Anhua, Distributed system and methodology of electrical power regulation, conditioning and distribution on an aircraft.
  36. Carl Udo (Bremen DEX), Drive control for a vertical rudder of an aircraft.
  37. Hein,Jeffrey M.; Williams,Nicholas A.; Sheoran,Yogendra Y.; Lam,Cecilia S.; Cowans,Ora Morency; Higuera,Benjamen Kurt; Peduchi,Andrew Stephen; Sellahewa,Ravisha Pramod; Brown,Daniel, Dual action inlet door and method for use thereof.
  38. Campbell,Thomas A.; Chambers,David S.; Willie,Robert H.; Rust,Charles W., Dual flow APU inlet and associated systems and methods.
  39. Ross David F. (Scottsdale AZ) Royalty Charles M. (Tempe AZ), Dual flow turbine engine muffler.
  40. Cronin Michael J. (Sherman Oaks CA) Seid Gordon (Los Angeles CA), ESC energy recovery system for fuel-efficient aircraft.
  41. Asfia, Julie F.; Williams, Kenneth R.; Atkey, Warren A.; Fiterman, Charles J.; Loukusa, Steven M.; Ng, Casey Y., Electric air conditioning system for an aircraft.
  42. Atkey, Warren A.; Bernier, Alan T.; Bowman, Michael D.; Campbell, Thomas A.; Cruse, Jonathan M.; Fiterman, Charles J.; Meis, Charles S.; Ng, Casey; Nozari, Farhad; Zielinski, Edward, Electric-based secondary power system architectures for aircraft.
  43. Atkey,Warren A.; Bernier,Alan T.; Bowman,Michael D.; Campbell,Thomas A.; Cruse,Jonathan M.; Fiterman,Charles J.; Meis,Charles S.; Ng,Casey Y. K.; Nozari,Farhad; Zielinski,Edward, Electric-based secondary power system architectures for aircraft.
  44. Atkey,Warren A.; Bernier,Alan T.; Bowman,Michael D.; Campbell,Thomas A.; Cruse,Jonathan M.; Fiterman,Charles J.; Meis,Charles S.; Ng,Casey Y. K.; Nozari,Farhad; Zielinski,Edward, Electric-based secondary power system architectures for aircraft.
  45. Kojori,Hassan A.; Michalko,Rodney G.; Konyukhova,Sophia V., Electrical energy management system on a more electric vehicle.
  46. Jeffrey Ronald Coles GB; Marc Holme GB; James Patrick Doyle GB, Electrical generator an aero-engine including such a generator, and an aircraft including such a generator.
  47. Michalko,Rodney G., Electrical power distribution system and method with active load control.
  48. Shander, Mark S.; Cote, Richard A.; Drake, Michael L.; Carter, III, Howard; Peters, John T.; Ng, Casey Y. K.; Hoag, Michael S.; Paterson, John T., Electrical systems architecture for an aircraft, and related operating methods.
  49. Lents, Charles E.; Squier, Steven E.; Thresher, Wayne A., Electrically driven aircraft cabin ventilation and environmental control system.
  50. Lents, Charles E.; Squier, Steven E.; Thresher, Wayne A., Electrically driven aircraft cabin ventilation and environmental control system.
  51. Williams Kenneth Roy, Electrically powered differential air-cycle air conditioning machine.
  52. Carl Udo (Bremen DEX), Elevator control system especially for an aircraft.
  53. Cronin Michael J. (Sherman Oaks CA), Energy efficient ECS powered by a variable voltage/variable frequency power system.
  54. Cronin, Michael J., Energy efficient ECS powered by a variable voltage/variable frequency power system.
  55. Graage Klaus,DEX, Energy supply unit on board an aircraft.
  56. Cronin Michael J. (Sherman Oaks CA) Seid Gordon (Los Angeles CA), Energy-efficient all-electric ECS for aircraft.
  57. Derouineau,Jean Luc, Engine power extraction control system.
  58. Douglas S. Walkinshaw CA; Gintautas P. Mitalas CA; Campbell S. L. McNeil CA; Keith F. Preston CA, Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions.
  59. Biagini Guido (Cherry Valley IL), Environmental control system for aircraft with improved efficiency.
  60. Kawamura Hideo (Samukawa JPX), Exhaust energy recovery and generator for use with an engine.
  61. Hanson Roger D. (Jackson MI), Exhaust gas silencing device.
  62. Brunskill Michael R. (Rollings Hills Estates CA) McKelvey Wilfred G. (Rancho Palos Verdes CA), Fluid conditioning system and apparatus.
  63. Hansen Robert C. (East Peoria IL), Fluidborne noise attenuator.
  64. Woodhouse Geoffrey D. (Prescott AZ), Fully integrated environmental and secondary power system.
  65. Itoh, Kazuo; Makino, Masahiro; Hirata, Toshiyuki, Grid interconnection device and power control system.
  66. Hoehne,Merle; Hoehne,Joachim; Heinrich,Hans Juergen, Heating system for use in on-board kitchens in means of transport and a method for heating food on board means of transport, in particular aircraft.
  67. Atkey,Warren A.; Fiterman,Charles J., High efficiency aircraft cabin air supply cooling system.
  68. Farrington Franklin D., High efficiency environmental control systems and methods.
  69. Durandeau Michel,FRX ; Foch Etienne,FRX, Hybrid control system for an aircraft aerodynamic surface.
  70. Daggett, David, Hybrid solid oxide fuel cell aircraft auxiliary power unit.
  71. Young ; Richard N., Independent power generator.
  72. Sheoran Yogendra Y., Inlet vortex bustor and ice protector for auxiliary power units.
  73. Williams Kenneth R., Integrated air conditioning and power unit.
  74. Malohn Donald A. (Scottsdale AZ), Integrated air cycle-gas turbine engine.
  75. Christoff William J. (Thousand Oaks CA), Integrated auxiliary power and environmental control unit.
  76. Campbell,Thomas A.; Voll,William A.; Diamond,John A., Integrated axially varying engine muffler, and associated methods and systems.
  77. Karimi, Kamiar J.; Breit, Joseph S.; Helton, Steven B.; Laib, Trevor M., Intelligent energy management architecture.
  78. Karimi, Kamiar J.; Breit, Joseph S.; Helton, Steven B.; Laib, Trevor M., Intelligent energy management architecture.
  79. Glahn,Wolfgang; Dueser,Gerd; Koenig,Axel; Finck,Mathias; Reitmann,Joerg, Intelligent power distribution management for an on-board galley of a transport vehicle such as an aircraft.
  80. Hirt William J. (Bellevue WA) Caldwell Jack H. (Kent WA) Stachowiak Claude R. (Renton WA) Rushwald Ira B. (Seattle WA) Kumasaka Henry A. (Seattle WA), Jet engine noise suppressor.
  81. Huffman Joseph G. (Lincoln NE) Seidl Thomas L. (Lincoln NE), Lightweight auxiliary power and forced air supply unit.
  82. Raymond Eugene T. (Kent WA), Load-adaptive hybrid actuator system and method for actuating control surfaces.
  83. Breit, Joseph Sherman; Witting, Michael Neil; Laib, Trevor; Rankin, Richard L.; Trela, John Anthony; Gates, Markland T.; Mansouri, Ali Reza, Localized utility power system for aircraft.
  84. Blaser Dwight A. (Sterling Heights MI) Goding David J. (Willow Springs IL) Ingard Karl U. (Kittery Point ME), Low back pressure exhaust silencer for diesel locomotives.
  85. Kraai Leon A. (Jackson MI) Sager ; Jr. Robert L. (Grass Lake MI) Hill William E. (Ann Arbor MI), Low backpressure straight-through reactive and dissipative muffler.
  86. Rumford Kimball J. (Fairfield CT) Ben-Porat Avi (Norwalk CT) Hudson George (Great Barrington MA), Management of electrically driven engine accessories.
  87. Trikha, Arun K., Method and apparatus for controlling aircraft devices with multiple actuators.
  88. Harvell John K. ; Michalski ; Jr. Joseph W. ; Freeman Craig A., Method and apparatus for controlling the inlet duct leading to an auxiliary power unit.
  89. Aberle, Markus; Blum, Joachim; Boehmisch, Mathias; Schetter, Thomas, Method and apparatus to regulate the supply of power to an electric drive using a hybrid energy supply system in a vehicle.
  90. Fiorini, Paolo; Sedky, Sherif; Caymax, Matty; Baert, Christiaan, Method of fabrication of an infrared radiation detector and infrared detector device.
  91. Eriksson Larry J. (Madison WI), Muffler construction.
  92. Ferri Alain,FRX, Muffler for internal combustion engines, especially in aviation of improved geometry and material.
  93. Cronin Michael J. (Sherman Oaks CA), Multi role primary/auxiliary power system with engine start capability for aircraft.
  94. Williams Kenneth R., Multi-mode secondary power unit.
  95. Aldrich Allyn M. (Rockford IL), Multi-motor actuation system for a power drive unit.
  96. Weber Kent ; Short Keith E., Multi-path secondary power system for an aircraft.
  97. Criswell David R. (4003 Camino Lindo San Diego CA 92122), Multi-use launch system.
  98. Cronin Michael J. (Sherman Oaks CA), Multifunction power system for an aircraft.
  99. Snyder, Philip H., Particle separator for a turbine engine.
  100. Campbell Thomas A. (Seattle WA) Dummeyer David M. (Snohomish WA) Yahyavi Mohammad (Bellevue WA), Passive cooling device and method for cooling an auxiliary power unit on an airplane.
  101. Dionne, Luc, Passive cooling system for auxiliary power unit installation.
  102. Jones Adrian D. (Edwardstown AUX), Perforate tube muffler.
  103. Hehmann ; Horst W. W. ; Kraft ; Robert E., Phased treatment noise suppressor for acoustic duct applications.
  104. Sarlioglu,Bulent; Huggett,Colin E., Rectification system for improving power quality of electrical power systems.
  105. Mark Paul Eisenhauer ; Gary Bowman, Redundant electrical DC power system for aircraft.
  106. Glennon Timonthy F., Redundant starting/generating system.
  107. Robinson Curtiss W. (Seattle WA) Raymond Eugene T. (Seattle WA), Rotary digital electrohydraulic actuator.
  108. Vanderleest Siebold (Seattle WA), Scoop and inlet for auxiliary power units and method.
  109. Tseo Gudin (San Diego CA), Slanted cavity resonator.
  110. Pettersson Henrik (Mynmki FIX), Sound attenuator for low frequencies, in particular for air ducts in paper mills.
  111. Hanson Roger D. ; Sterrett Dale E., Straight through muffler with conically-ended output passage.
  112. Duces, Marc; Lando, Jean-Louis; Foch, Etienne, System for electrical generation, conversion, distribution, and starting on board an aircraft.
  113. Curry Michael J.,CAX ; Kuipers Alison J.,CAX ; Chappell Laurie M.,CAX ; Emmett Paul L.,CAX, System for improving the well-being of humans in a commercial aircraft.
  114. Frost,Gordon Scott; DiPasquale,Michael T.; Parks,John W., System for monitoring and controlling fuel cell-based power generation units.
  115. Mouton Pierre,FRX, System for restarting an aircraft engine in flight after loss of engine power.
  116. Zielinski, Edward; Bernier, Alan T.; Knechtel, Kent W.; Campbell, Thomas A.; White, Jeffrey J.; Ralston, Mark D., Systems and methods for starting aircraft engines.
  117. Sheoran, Yogendra Y.; Brown, Daniel V.; Edmonds, David H., Tortuous path quiet exhaust eductor system.
  118. Thompson, Robert G., Turbocharged auxiliary power unit with controlled high speed spool.
  119. Herman Gerald T. (Seattle WA), Turbojet engine nozzle for attenuating core and turbine noise.
  120. Breit, Joseph S.; Szydlo Moore, Joanna A.; Lorhammer, Kurt, Vehicular power distribution system and method.
  121. Markwart Michael (Halstenbek DEX) Petry Klaus (Georgetown TX) Scherer Thomas (Hamburg DEX), Ventilating system for reducing contaminations in the air of an aircraft.