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Volumn 28, Issue 2-3, 2004, Pages 206-213

Weight optimisation of hinges for light mechanisms: Criteria and design aspects

Author keywords

Articulated systems; Pin joint; Rolling bearings; Variable geometry; Weight penalty

Indexed keywords

COMPUTATIONAL GEOMETRY; FRICTION; FUNCTION EVALUATION; INDUSTRIAL APPLICATIONS; OPTIMIZATION; PRODUCT DESIGN; ROLLING; STATISTICAL METHODS;

EID: 5144232985     PISSN: 1615147X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s00158-004-0435-7     Document Type: Article
Times cited : (4)

References (16)
  • 2
    • 0034149102 scopus 로고    scopus 로고
    • The belt-rib concept: A structronic approach to variable camber
    • Campanile, L.F.; Sachau, D. 2000: The belt-rib concept: a structronic approach to variable camber. J Intell Mater Syst Struct 11, 215-224
    • (2000) J Intell Mater Syst Struct , vol.11 , pp. 215-224
    • Campanile, L.F.1    Sachau, D.2
  • 4
    • 85136425570 scopus 로고
    • Stress-concentration factors around a central circular hole in a plate loaded through pin in the hole
    • Frocht, M.M.; Hill, H.N. 1940: Stress-Concentration Factors around a central circular hole in a plate loaded through pin in the hole. J Appl Mech 7, A5-A9
    • (1940) J Appl Mech , vol.7
    • Frocht, M.M.1    Hill, H.N.2
  • 5
    • 5144232708 scopus 로고
    • Expanding wing for aeroplanes, US-Patent No. 389,987
    • Hannah, M.O. 1930: Expanding wing for aeroplanes, US-Patent No. 389,987
    • (1930)
    • Hannah, M.O.1
  • 9
    • 0042657537 scopus 로고    scopus 로고
    • Compliant systems using monolithic mechanisms
    • Kota, S. 2001: Compliant systems using monolithic mechanisms. Smart Material Bulletin 3, 7-10
    • (2001) Smart Material Bulletin , vol.3 , pp. 7-10
    • Kota, S.1
  • 10
    • 5144227264 scopus 로고
    • Variable shaped airfoil. US-Patent No. 3,179,357
    • Lyon, D.G. 1965: Variable shaped airfoil. US-Patent No. 3,179,357
    • (1965)
    • Lyon, D.G.1
  • 11
    • 5144227461 scopus 로고
    • Aile métallique á courbure et incidence variables, pour aéroplanes. French Patent No. 536,494
    • Mace, M.R.-D. 1921: Aile métallique á courbure et incidence variables, pour aéroplanes. French Patent No. 536,494
    • (1921)
    • Mace, M.R.-D.1
  • 12
    • 5144230363 scopus 로고
    • Fluid dynamic lift generating or control force generating structures. US-Patent No. 3,716,209
    • Pierce, D. 1973: Fluid dynamic lift generating or control force generating structures. US-Patent No. 3,716,209
    • (1973)
    • Pierce, D.1
  • 13
    • 5144232356 scopus 로고
    • Ottawa, Kansas: Roskam Aviation and Engineering Corporation
    • Roskam, R. 1986: Airplane design, Part 3, 199. Ottawa, Kansas: Roskam Aviation and Engineering Corporation
    • (1986) Airplane Design, Part 3 , vol.199
    • Roskam, R.1
  • 14
    • 5144226633 scopus 로고
    • Rowarth, R. 1981. Variable camber wing. UK-Patent application No. 2,059,368 A
    • (1981)
    • Rowarth, R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.