LEGS
we have estimated that the maximum amount of stress any part of the legs are exposed to is around 8mpa. Although our calculations need to be refined it is unlikely that this value will not be greatly affected. Therefore i have put together a list of aluminium alloys that can be used.
alloy....................... ...compression yield stregnth (mpa)
Aluminum 2014-O .................................................185
Aluminum 2014-T4; 2014-T451 ............................425
Aluminum 2014-T6; 2014-T651 ...........................470
Aluminum 2048-T851 Plate .................................420
Aluminum 2618-T61.............................................370
Aluminum 5086-H112 ..........................................270
Aluminum 5086-H116; 5086-H32 .......................290
Aluminum 5086-H34 ..........................................325
Aluminum 5086-O ..............................................160
Aluminum 7039-T61 ..........................................390
Aluminum 7039-T64 ..........................................410
Aluminum 7178-T6; 7178-T651 ........................530
Aluminum 7178-T76; 7178-T7651 ...................460
Aluminum 7475-T7351 ...................................380
Aluminum A206.0-T7 Casting Alloy ..............372
Aluminum 206.0-T7 Casting Alloy ................372
Aluminum 208.0-F, Sand Cast .....................105
Aluminum 242.0-T21, Sand Cast ..................125
Aluminum 242.0-T571, Permanent Mold Cast .235
Aluminum 242.0-T571, Sand Cast ....................235
Aluminum 242.0-T61, Permanent Mold Cast ....305
Aluminum 242.0-T77, Sand Cast .....................165
Aluminum 295.0-T4, Sand Cast ......................115
Aluminum 295.0-T6, Sand Cast .....................170
Aluminum 295.0-T62, Sand Cast ...................235
Aluminum 296.0-T4, Cast ...............................140
Aluminum 296.0-T6, Permanent Mold Cast .180
Aluminum 296.0-T7, Cast ..............................140
Aluminum 319.0-F, Permanent Mold Cast .....130
Aluminum 319.0-F, Sand Cast ........................130
Aluminum 319.0-T6, Sand Cast ......................170
Aluminum 336.0-T551, Permanent Mold Cast 193
Aluminum 336.0-T65, Permanent Mold Cast ...296
Aluminum 354.0-T61, Permanent Mold Cast ....250
Aluminum 355.0-T71, Permanent Mold Cast .....215
Aluminum 355.0-T71, Sand Cast ........................205
Aluminum 355.0-T51, Permanent Mold Cast ....165
Aluminum 355.0-T51, Sand Cast .......................165
Aluminum 355.0-T61, Cast ................................215
Aluminum 355.0-T62, Permanent Mold Cast .....275
Aluminum 355.0-T6, Permanent Mold Cast ........185
Aluminum 355.0-T6, Sand Cast ..........................180
STEEL WIRE
I have calculted that if we use steel wire with a thickness of 1cm to lift the objects, it will be exposed to a maximum tension of 124.9 mpa. Therefore a medium carbon steel should be used to create the wire as it typically has a tensile strength much higher than this.
mass estimation of the legs and boom
using the dimensions given on the cad drawings i calculated a rough estimate of the mass of the crane legs and boom.
legs
given that all of the aforementioned alloys have a density between 2800 - 2650 kg/m^3
mass of the crane foot extender= 3.69-3.50kg
'' '' crane foot = 1.76- 1.67kg
'' ''crane leg = 3.25-3.08kg
'' ''crane shoulder = 5.00 - 4.74kg
Boom
when estimating the boom i came across something very worrying. i will show my calculations so someone can spot a mistake if i have made one.
density of carbon steel = 7800kg/m^3
cross sectional area of boom = (0.05x0.06)+2(0.02x0.07)= 5.8x10^-3 m^2
volume of boom = 5.1 x 5.8x10^-3 = 0.02958 m^3
mass of boom = 7800 x 0.02958 = 230.724 kg
here you can see that the boom is very heavy, therefore i suggest we make it thinner or shorter unless my calculations are wrong.
all facts and figures were obtained from http://www.matweb.com/
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