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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

Supersonic aircraft with spike for controlling and reducing sonic boom

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-030/00    B64C-007/00   
미국특허분류(USC) 244/001.N; 244/119; 181/211
출원번호 US-0104403 (2002-03-22)
발명자 / 주소
  • Henne, Preston A.
  • Howe, Donald C.
  • Wolz, Robert R.
  • Hancock, Jr., Jimmy L.
출원인 / 주소
  • Gulfstream Aerospace Corporation
대리인 / 주소
    Howrey Simon Arnold & White LLP
인용정보 피인용 횟수 : 24  인용 특허 : 63
초록
▼

An aircraft includes a spike projecting forward from the leading end of the fuselage and/or rearward from the trailing end of the fuselage. The spike can include a single section or two or more sections of varying cross-sectional area. Transition regions between sections of varying cross-sectional area are located and shaped to reduce coalescence of shock waves created thereby during supersonic flight. The spike can be collapsible and can be retracted into the fuselage. The spike can have a cross-sectional shape wherein the nose thereof lies on a line fo...

대표
청구항
▼

An aircraft includes a spike projecting forward from the leading end of the fuselage and/or rearward from the trailing end of the fuselage. The spike can include a single section or two or more sections of varying cross-sectional area. Transition regions between sections of varying cross-sectional area are located and shaped to reduce coalescence of shock waves created thereby during supersonic flight. The spike can be collapsible and can be retracted into the fuselage. The spike can have a cross-sectional shape wherein the nose thereof lies on a line fo...

이 특허에 인용된 특허 (63)

  1. Destuynder Roger (Noisy le Sec FRX) Bouttes Jacques (Paris FRX) Poisson-Quinton Philippe (Paris FRX), Active method and installation for the reduction of buffeting of the wings of an aircraft.
  2. Mark A. Hreha ; Gerard Schkolnik, Adaptive method to control and optimize aircraft performance.
  3. Taylor Thomas C. (P.O. Box 1547 Wrightwood CA 92397) Cerna Peter (2815 California ; #4 Dickinson TX 77539), Aerospike for attachment to space vehicle system.
  4. Buchsel Christian K. E. (Issaquah WA) King Gary E. (Snohomish WA) Burns Jerry J. (Mukilteo WA), Aft double deck airplane.
  5. Pierce, Donald, Aircraft having improved strake configuration.
  6. Peters ; Jr. Spence E., Aircraft structure to improve directional stability.
  7. Tracy Richard R., Aircraft wing and fuselage contours.
  8. Feifel Winfried M. (Seattle WA), Airfoil.
  9. Fujino Michimasa,JPX, Airplane.
  10. Inoue Kazuo (Nerima JPX) Fujino Michimasa (Komae JPX), Airplane.
  11. Graham ; Blair M. ; Hamrick ; Harry C., Airplane configuration designed for the simultaneous reduction of drag and sonic boom.
  12. Cichy Daniel R. (Reynoldsburg OH), Apparatus and method for increasing the angle of attack operating range of an aircraft.
  13. Masashi Shigemi JP; Teruomi Nakaya JP; Shigemi Shindo JP; Minoru Takizawa JP; Takeshi Ohnuki JP, Arithmetic processing method and system in a wide velocity range flight velocity vector measurement system using a square truncated pyramid-shape five-hole pitot probe.
  14. Frei Douglas R. (Stony Brook NY), Automatic camber control.
  15. West Harrison (Cincinnati OH) Delaney Bobby R. (Cincinnati OH), Compact multimission aircraft propulsion simulator.
  16. Lbert Gerhard (Baldham DEX) Bschorr Oskar (Munich DEX) Spies Hans (Pfaffenhofen DEX), Device for reducing the frictional drag of moving bodies.
  17. Friebel Gottfried O. (Bellevue WA) Kulfan Robert M. (Kirkland WA), Double parasol, favorable interference airplane.
  18. Falco Robert E. (East Lansing MI), Drag reduction method and surface.
  19. Seidel Gerhard E. ; Sankrithi Mithra, Dual upper deck airplane.
  20. Spillman John J. (Bedford GB2), Fluid stream deflecting members for aircraft bodies or the like.
  21. Spillman John J. (Bedford GB2), Fluid stream deflecting members for aircraft bodies or the like.
  22. Hakenesch Peter,DEX, Fuselage nose for controlling aerodynamic vehicles and method of utilizing same.
  23. Tracy Richard R. (3000 Old Ranch Rd. Carson City NV 89704), High efficiency, supersonic aircraft.
  24. Gioia G. Leonard (255 Fortenberry Rd. ; A Merritt Island FL 32952), High performance amphibious airplane.
  25. Tracy Richard R., High-efficiency, supersonic aircraft.
  26. Greene Vibert F. (19400 Sorenson Ave. Cupertino CA 95014), Jet airplane.
  27. Gerhardt Heinz Adolf ; Kerswell James Franklin ; Priestley Richard Thomas ; Gibson Berry Thomas, Laminar supersonic transport aircraft.
  28. Morgenstern John M, Low sonic boom shock control/alleviation surface.
  29. Palmer Steven D., Method and apparatus for flight parameter monitoring and control.
  30. Gleine Wolfgang,DEX ; Hilbig Reinhard,DEX ; Wendt Hans-Joachim,DEX, Method and apparatus for optimizing the aerodynamic effect of an airfoil.
  31. Stephen A. Huyer ; John R. Grant ; James S. Uhlman ; Jeffrey S. Marshall, Method for computing three dimensional unsteady flows by solution of the vorticity equation on a Lagrangian mesh.
  32. Benne Michael Edward ; Donovan John Francis ; Kelble Christopher Allen ; Kihlken Thomas Allen ; Morris Martin Jesse ; Pal Alexander, Method for determining pressure.
  33. Palmer Steven D., Method for flight parameter monitoring and control.
  34. Fujino Michimasa,JPX ; Kawamura Yuichi,JPX, Method for reducing wave resistance in airplane.
  35. Kumata Hirotaka,JPX ; Katahira Kiyoshi,JPX ; Wakita Shuichi,JPX ; Nishikawa Toshihiro,JPX, Method for reducing wave resistance in airplane.
  36. Maris John M. (6 Lakeview Crescent Cold Lake ; Alberta CAX T0A 0V2), Method of aerodynamic stall-turbulence indication.
  37. Jackson ; Jr. Charlie M. (Yorktown VA) Dollyhigh Samuel M. (Newport News VA) Shaw David S. (Newport News VA), Metric half-span model support system.
  38. Finch Thomas (San Antonio TX), Modifications to jet aircraft having aft fuselage-mounted nacelles overlapping the wing assemblies.
  39. Goldhammer Mark I. (Bellevue WA), Nacelle and wing assembly.
  40. Jones Robert T. (Los Altos Hills CA), Oblique-wing supersonic aircraft.
  41. Lind Richard C. ; Brenner Martin J., On-line .mu. method for robust flutter prediction in expanding a safe flight envelope for an aircraft model under flight test.
  42. Buisson Dominique (Villemur FRX) Irvoas Joseph (Cugnaux FRX), Process and system for determining the longitudinal position of the center of gravity of an aircraft provided with an ad.
  43. Stewart John S., Removable cutting blades for a helical cutterhead.
  44. Rona Thomas P. (Seattle WA), Removable external payload carrier for aircraft.
  45. Headley Jack W. (Rancho Palos Verdes CA) Skow Andrew M. (Hermosa Beach CA) Titiriga ; Jr. Andrew (Torrance CA), Shark nose for aircraft.
  46. Rising Jerry J. ; Vadyak ; Jr. Joseph, Shock suppression supersonic aircraft.
  47. Meston Vyacheslav A. (Altufievskoe Shosse ; d.86 ; kv. 275 Moscow RUX 127349), Spacecraft with a crew escape system.
  48. Boyadjian Lon (Igny FRX), Spoiler torque controlled supersonic missile.
  49. Komerath Narayanan M. ; Darden Leigh Ann ; Magill John C. ; Peterson Kevin G., Stagnation point vortex controller.
  50. Rethorst Scott (1806 Foothill St. Pasadena CA 91030), Supersonic aircraft shock wave energy recovery system.
  51. Rethorst Scott (South Pasadena CA), Supersonic aircraft shock wave energy recovery system.
  52. Rethorst Scott C. (South Pasadena CA), Supersonic aircraft shock wave energy recovery system.
  53. Hartmann Thomas M. ; Morgenstern John M. ; Sokol Daniel H., Supersonic business jet.
  54. Hartmann Tom ; Morgenstern John M. ; Sokol Daniel, Supersonic business jet.
  55. Gao Ge (Boca Raton FL), Surface for low drag in turbulent flow.
  56. Blackburn Ronald F. ; Warmkessel Barry M. ; Kawamoto Sonja M., System for increasing the aerodynamic and hydrodynamic efficiency of a vehicle in motion.
  57. Wille Robert Henry, Tail for an aircraft.
  58. Whitener Philip C. (Seattle WA), Tandem wing airplane.
  59. Braden John A. (2791 Okawana Dr. Marietta GA 30067) Dixon Charles J. (3261 Hickory Crest Dr. Marietta GA 30064), Terraced channels for reducing afterbody drag.
  60. Cunningham ; Jr. Atlee Marion, Trapped vortex airfoil nose.
  61. Kaniut Herbert (Orrerweg 33/35 5000 Cologne 71 DT), Travelling tail-unit with circular arc motion.
  62. Hirschel Ernst H. (Zorneding DEX) Fleckenstein Hubert (Grasbrunn DEX) Thiede Peter (Ganderkesee DEX), Wall with a drag reducing surface and method for making such a wall.
  63. Ellis Roger R. (Wichita KS) Gertsen W. Marvin (Wichita KS) Conley Norman E. (Wichita KS), Wing with improved leading edge for aircraft.

이 특허를 인용한 특허 (24)

  1. Kucherov, Yan R.; Hubler, Graham K., Blast wave effects reduction system.
  2. Grip, Robert Erik; Brown, John Joseph, Expandable nose cone.
  3. Lugg, Richard H., Hypersonic aircraft.
  4. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  5. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A., Isentropic compression inlet for supersonic aircraft.
  6. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  7. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Isentropic compression inlet for supersonic aircraft.
  8. Conners, Timothy R., Low shock strength inlet.
  9. Conners, Timothy R., Low shock strength inlet.
  10. Conners, Timothy R., Low shock strength propulsion system.
  11. Conners, Timothy R., Low shock strength propulsion system.
  12. Felter,John; Thacker,Michael; Laflin,Kelly, Method and system for gathering pressure signature data using a scaled model in a wind tunnel.
  13. Kobayashi,Hiroaki; Tanatsugu,Nobuhiro; Sato,Tetsuya; Hongo,Motoyuki; Maru,Yusuke, Method for reducing resistance of flying object using expandable nose cone.
  14. Morgenstern, John M.; Bach, James B.; Arslan, Alan E., Methods for configuring aircraft to meet performance goals and shock wave disturbance constraints.
  15. Arata,Allen A., Movable nose cap and control strut assembly for supersonic aircraft.
  16. Minick, Alan B., Rotary wing system with ion field flow control.
  17. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R., Sub-scale sonic boom modeling.
  18. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C., Supersonic aircraft jet engine installation.
  19. Lugg, Richard H., Supersonic aircraft with shockwave canceling aerodynamic configuration.
  20. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L., Supersonic aircraft with spike for controlling and reducing sonic boom.
  21. Freund, Donald, Systems and methods for controlling a magnitude of a sonic boom.
  22. Freund, Donald, Systems and methods for controlling a magnitude of a sonic boom.
  23. Freund, Donald, Systems and methods for controlling a magnitude of a sonic boom.
  24. Freund, Donald, Systems and methods for controlling a magnitude of a sonic boom.

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