Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position Solution

STEP 0: Pre-Calculation Summary
Formula Used
Direct Compressive Stress in crankweb = Force on Crankweb/(Width of Crank Web*Thickness of Crank Web)
σcd = Pweb/(w*t)
This formula uses 4 Variables
Variables Used
Direct Compressive Stress in crankweb - (Measured in Pascal) - Direct Compressive Stress in crankweb is the compressive stress in the crank web as a result of only the radial component of thrust force onto the connecting rod & crankpin.
Force on Crankweb - (Measured in Newton) - Force on Crankweb is the force acting onto the crankweb used in assembly of crankshaft & connecting rod, converts reciprocation of piston to rotation of crankshaft.
Width of Crank Web - (Measured in Meter) - Width of Crank Web is defined as the width of the crank web (the portion of a crank between the crankpin and the shaft) measured perpendicular to the crankpin longitudinal axis.
Thickness of Crank Web - (Measured in Meter) - Thickness of Crank Web is defined as the thickness of the crank web (the portion of a crank between the crankpin and the shaft) measured parallel to the crankpin longitudinal axis.
STEP 1: Convert Input(s) to Base Unit
Force on Crankweb: 6500 Newton --> 6500 Newton No Conversion Required
Width of Crank Web: 65 Millimeter --> 0.065 Meter (Check conversion here)
Thickness of Crank Web: 40 Millimeter --> 0.04 Meter (Check conversion here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
σcd = Pweb/(w*t) --> 6500/(0.065*0.04)
Evaluating ... ...
σcd = 2500000
STEP 3: Convert Result to Output's Unit
2500000 Pascal -->2.5 Newton per Square Millimeter (Check conversion here)
FINAL ANSWER
2.5 Newton per Square Millimeter <-- Direct Compressive Stress in crankweb
(Calculation completed in 00.004 seconds)

Credits

Created by Saurabh Patil
Shri Govindram Seksaria Institute of Technology and Science (SGSITS ), Indore
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9 Design of Crank Web at Top Dead Centre Position Calculators

Bending stress in central plane of crankweb
Go Bending Stress in Crankweb = (6*(Force on Crankweb*((Length of Crank Pin*0.75 )+(Thickness of Crank Web/2))))/(Thickness of Crank Web^2*Width of Crank Web)
Length of crankpin given bending stress in central plane of crankweb
Go Length of Crank Pin = ((((Bending Stress in Crankweb*Thickness of Crank Web^2*Width of Crank Web)/6)/Force on Crankweb)-(0.5*Thickness of Crank Web))/0.75
Thickness of crankweb given bending moment at bearing 1 of side crankshaft at TDC position
Go Thickness of Crank Web = (Bending Moment at Bearing1 of Crankshaft/Force on Crank Pin)-(0.75*Length of Crank Pin)-(0.5*Length of Bearing1 of Crankshaft)
Total compressive stress in central plane of crankweb of side crankshaft at TDC position
Go Compressive Stress in Crank Web Central Plane = (Force on Crankweb/(Width of Crank Web*Thickness of Crank Web))+(Bending Stress in Crankweb)
Bending stress in central plane of crankweb given bending moment
Go Bending Stress in Crankweb = (6*Bending Moment at Central Plane of Crank Web)/(Thickness of Crank Web^2*Width of Crank Web)
Thickness of crankweb given bending moment in central plane of crankweb
Go Thickness of Crank Web = ((Bending Moment at Central Plane of Crank Web/Force on Crankweb)-(0.75*Length of Crank Pin))/0.5
Length of crankpin given bending moment in central plane of crankweb
Go Length of Crank Pin = ((Bending Moment at Central Plane of Crank Web/Force on Crankweb)-(0.5*Thickness of Crank Web))/0.75
Bending moment in central plane of crankweb
Go Bending Moment at Central Plane of Crank Web = Force on Crankweb*((Length of Crank Pin*0.75 )+(Thickness of Crank Web/2))
Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position
Go Direct Compressive Stress in crankweb = Force on Crankweb/(Width of Crank Web*Thickness of Crank Web)

Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position Formula

Direct Compressive Stress in crankweb = Force on Crankweb/(Width of Crank Web*Thickness of Crank Web)
σcd = Pweb/(w*t)

What is a Crankshaft?

The crankshaft of an engine is mechanical equipment whose main function is to convert the Linear motion of the Piston to Rotational Motion. The reciprocating motion of the piston is transferred to the crankshaft through Connecting Rod. A crankshaft has crankpins, crank webs, balancing weights, and main journals. The big end of the connecting rod is connected to the crankpin of the crankshaft. In a 4 stroke engine, one complete rotation of the crankshaft takes place in two strokes of the piston. A crankshaft has the following main parts :
1. Crankpin
2. Main Journals
3. Crank Web
4. Counterweights
5. Thrust Washers
6. Oil passage & Oil Seals
7. Flywheel Mounting Flange

How to Calculate Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position?

Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position calculator uses Direct Compressive Stress in crankweb = Force on Crankweb/(Width of Crank Web*Thickness of Crank Web) to calculate the Direct Compressive Stress in crankweb, Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position is defined as the magnitude of force applied onto the crank web, divided by the cross-sectional area of the crank web in a direction perpendicular to the applied force. Direct Compressive Stress in crankweb is denoted by σcd symbol.

How to calculate Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position using this online calculator? To use this online calculator for Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position, enter Force on Crankweb (Pweb), Width of Crank Web (w) & Thickness of Crank Web (t) and hit the calculate button. Here is how the Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position calculation can be explained with given input values -> 2.5E-6 = 6500/(0.065*0.04).

FAQ

What is Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position?
Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position is defined as the magnitude of force applied onto the crank web, divided by the cross-sectional area of the crank web in a direction perpendicular to the applied force and is represented as σcd = Pweb/(w*t) or Direct Compressive Stress in crankweb = Force on Crankweb/(Width of Crank Web*Thickness of Crank Web). Force on Crankweb is the force acting onto the crankweb used in assembly of crankshaft & connecting rod, converts reciprocation of piston to rotation of crankshaft, Width of Crank Web is defined as the width of the crank web (the portion of a crank between the crankpin and the shaft) measured perpendicular to the crankpin longitudinal axis & Thickness of Crank Web is defined as the thickness of the crank web (the portion of a crank between the crankpin and the shaft) measured parallel to the crankpin longitudinal axis.
How to calculate Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position?
Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position is defined as the magnitude of force applied onto the crank web, divided by the cross-sectional area of the crank web in a direction perpendicular to the applied force is calculated using Direct Compressive Stress in crankweb = Force on Crankweb/(Width of Crank Web*Thickness of Crank Web). To calculate Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position, you need Force on Crankweb (Pweb), Width of Crank Web (w) & Thickness of Crank Web (t). With our tool, you need to enter the respective value for Force on Crankweb, Width of Crank Web & Thickness of Crank Web and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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