O slideshow foi denunciado.
Utilizamos seu perfil e dados de atividades no LinkedIn para personalizar e exibir anúncios mais relevantes. Altere suas preferências de anúncios quando desejar.
PADEYE DESIGN
CALCULATION
TOPSIDE
PTS 34.19.10.30 ( Appendix IX )
• In lifting attachment design load the padeye shall be
designed for lateral load of a lea...
1.1 Design Calculation
Example1

= (MBL / Sling MBL)

TOPSIDE
O.75 X
Use min value 35 : 45
O.75 X

TOPSIDE

Use min value 25 : 26.25
=((radius of main plate-(pin hole/2))*(tm) +(radius cheekplate1-(pin
hole/2))*tce*2+(radius cheekplate2 -(pin hole/2))*tc2...
TOPSIDE
TOPSIDE
Próximos SlideShares
Carregando em…5
×

de

Padeye design calculation Slide 1 Padeye design calculation Slide 2 Padeye design calculation Slide 3 Padeye design calculation Slide 4 Padeye design calculation Slide 5 Padeye design calculation Slide 6 Padeye design calculation Slide 7
Próximos SlideShares
Padeye calculation example
Avançar
Transfira para ler offline e ver em ecrã inteiro.

11 gostaram

Compartilhar

Baixar para ler offline

Padeye design calculation

Baixar para ler offline

Livros relacionados

Gratuito durante 30 dias do Scribd

Ver tudo

Padeye design calculation

  1. 1. PADEYE DESIGN CALCULATION TOPSIDE
  2. 2. PTS 34.19.10.30 ( Appendix IX ) • In lifting attachment design load the padeye shall be designed for lateral load of a least 5% of this load. • Permissible stresses shall be as defined in AISC with following additional requirements : - Transfer of stresses through the thickness of the plate shall not be allowed unless the material has through thickness properties. In this instance through thickness stresses shall be limited to 0.2 Fy. TOPSIDE
  3. 3. 1.1 Design Calculation Example1 = (MBL / Sling MBL) TOPSIDE
  4. 4. O.75 X Use min value 35 : 45 O.75 X TOPSIDE Use min value 25 : 26.25
  5. 5. =((radius of main plate-(pin hole/2))*(tm) +(radius cheekplate1-(pin hole/2))*tce*2+(radius cheekplate2 -(pin hole/2))*tc2e*2)*2 = shear stress / Allowable shear stress =2*(2* radius of cheekplate(1)* tce)+2*(2* radius of cheek plate(2)* tc2e)+(radius of main plate*2* (tm))-2* pin hole* (tm) = Max static sling load *1000/ Area at tension failure =Tension stress / Allowable tensile stress =(tce/((tm) +2* tce+2* tc2e))* Max static sling load = F * 1000 / Aw = 0.7* (tc) = shear stress at weld / Allowable shear stress = ([B]-((tm) +2* 0.75tm+2* tc2e))/2 = 0.1*[B] = 0.2*[B]
  6. 6. TOPSIDE
  7. 7. TOPSIDE
  • indahningtyastuti

    Jun. 13, 2019
  • AdiYunizar

    Dec. 12, 2018
  • MarcoAlbanesi1

    Oct. 3, 2017
  • JangHyunLEE2

    Jul. 10, 2016
  • bkprodh

    Mar. 2, 2016
  • MinThuAung1

    Sep. 17, 2015
  • NAVNATHKAMTHE

    Jun. 24, 2015
  • musfarkhan

    Jun. 3, 2015
  • AvinashB2

    May. 28, 2015
  • sijish_ms

    Mar. 24, 2015
  • SaraHassan126

    Oct. 12, 2014

Vistos

Vistos totais

30.387

No Slideshare

0

De incorporações

0

Número de incorporações

62

Ações

Baixados

889

Compartilhados

0

Comentários

0

Curtir

11

×