$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

특허 상세정보

Supersonic business jet

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) 1207   
미국특허분류(USC) D12/333 ; D12/319 ; D12/331
출원번호 US-0101387 (1999-03-02)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Schruhl
인용정보 피인용 횟수 : 33  인용 특허 : 1
초록이 없습니다.
대표
청구항

We claim the ornamental design for: supersonic business jet, as shown and described.

이 특허를 인용한 특허 피인용횟수: 33

  1. Gopalaswami, Raghaven; Prahlada; Gyaneshwar, Yachareni; Gollakota, Satyanarayana; Venugopalan, Puthenmadhom; Panneerselvam, Subramanian; Kumar, Satish; Manna, Pulinbehari; Yedidi, Satyanarayana. Aerospace vehicle. USP200307D477806.
  2. Stuhr, Victor K.. Aircraft engine nacelles and methods for their manufacture. USP2003116651928.
  3. Stuhr, Victor K.. Aircraft engine nacelles and methods for their manufacture. USP2005116966524.
  4. Michael J. Andreyko. Airplane. USP200212D467217.
  5. Zha, Gecheng. Co-flow jet aircraft. USP201006D616805.
  6. Hagemeister, Corey; Aronstein, David C.; Schueler, Kurt L.. Design methods and configurations for supersonic aircraft. USP2009097581697.
  7. Hagemeister,Corey; Aronstein,David C.; Schueler,Kurt L.. Design methods and configurations for supersonic aircraft. USP2007087252263.
  8. Au, Chin Kau. Elevator of a plane. USP201002D610066.
  9. Nelson, Chester P.. High-speed aircraft. USP200309D479501.
  10. Eakins, Mark E.; Wojciechowski, Paul M.. High-speed aircraft and methods for their manufacture. USP2010017644888.
  11. Lugg, Richard H.. Hypersonic aircraft. USP20190310232937.
  12. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2005096938854.
  13. Nelson, Chester P.. Integrated and/or modular high-speed aircraft. USP2003066575406.
  14. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  15. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  16. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  17. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  18. Charlie Ko Chen Han. Long distance long range supersonic jet fighter. USP200212D467533.
  19. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  20. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  21. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  22. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  23. Morgenstern,John M.; Arslan,Alan E.; Moose,Garret A.. Methods for incorporating area ruled surfaces in a supersonic aircraft. USP2007127311287.
  24. Hartmann, Tom; Morgenstern, John M.. Passive aerodynamic sonic boom suppression for supersonic aircraft. USP2005116959896.
  25. Nelson, Chester P.. Supersonic aircraft. USP200307D477561.
  26. Rouleau, Bruce S.; Graham, David H.; Reynolds, Ross S.; Wainfan, Barnaby S.. Supersonic aircraft. USP200303D471854.
  27. Chase, James D.; Garzon, German Andres. Supersonic aircraft jet engine. USP2010117837142.
  28. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  29. Lugg, Richard H.. Supersonic aircraft with shockwave canceling aerodynamic configuration. USP2013068453961.
  30. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  31. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  32. Morgenstern, John M.. Tail-braced wing aircraft and configurations for achieving long supersonic range and low sonic boom. USP2004056729577.
  33. Dong, Lawrence Y.; Sankrithi, Mithra M. K. V.. Tandem wing aircraft and method for manufacturing and operating such aircraft. USP2004036705567.