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특허 상세정보

Metric half-span model support system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G01M-009/00   
미국특허분류(USC) 73/147
출원번호 US-0145210 (1980-04-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 14  인용 특허 : 1
초록

The invention relates to a model support system used to support a model in a wind tunnel test section. The model comprises a metric, or measured, half-span 12 supported by a nonmetric, or nonmeasured half-span 11 which is connected to a sting support 13. Moments and forces acting on the metric half-span 12 are measured without interference from the support system during a wind tunnel test.

대표
청구항

A wind tunnel model and support system for use in a wind tunnel test section comprising in combination: a symmetrical model of an aircraft having wings; said symmetrical model comprising a metric half-span and a nonmetric half-span; said metric half-span being adjacent to said nonmetric half-span at the plane of symmetry of said model; sting support means attached to the wing tip of said nonmetric half-span and adapted for attachment to a wind tunnel test section; a strain gauge balance positioned within the fuselage of said symmetrical model and connect...

이 특허를 인용한 특허 피인용횟수: 14

  1. Chen, Ping-Chih. Dry wind tunnel system. USP2013038393206.
  2. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  3. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  4. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  5. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  6. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  7. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  8. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  9. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  10. Adamson, Eric Evin. Methods and systems for enabling wind tunnel models to transition between measuring aerodynamic forces and measuring acoustic signatures. USP2015099134195.
  11. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  12. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  13. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  14. Gibson,Thomas M. Wind tunnel testing. USP2006107127942.