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For the injector faceplate to stay fastened to the manifold, the bolts must satisfy a factor of safety for both tensile and shear stress. A net upward pressure acting on the faceplate applied to the area of the injector requires all bolts on the injector manifold -both axial and radial- to withstand this force to maintain structural integrity. These calculations also pertain to the radial bolts keeping the faceplate attached to the combustion chamber.
Known Values:
For Injector:
Name | Value |
---|
Pressure (P_injector) | 640 psi |
Area (A_injector) | 9.42 in^2 |
Number of Inner Bolts (N_inner) | 10 bolts |
Major Diameter of Inner Bolts (D_major1) | 0.086" |
Thread Spacing of Inner Bolts (t_s1) | 0.01788" |
Number of Outer Bolts (N_outer) | 4 bolts |
Major Diameter of Outer Bolts (D_major2) |
|
Thread Spacing of Outer Bolts (t_s2) |
|
Ultimate Tensile Strength of Injector Bolts (sigma_steel1) | 70000 psi |
For Combustion Chamber:
Name | Value |
---|
Pressure (P_chamber) |
|
Area (A_chamber) |
|
Number of Radial Chamber Bolts (N_chamber) |
|
Major Diameter of Radial Chamber Bolts (D_major3) |
|
Thread Spacing of Radial Chamber Bolts (t_s3) |
|
Number of Radial Chamber Bolts Bolts (N_chamber) |
|
Major Diameter of Radial Chamber Bolts (D_major3) |
|
Thread Spacing of Radial Chamber Bolts (t_s3) |
|
Ultimate Tensile Strength of Radial Chamber Bolts (sigma_steel2) |
|
The area of the bolt can be determined by using its pitch diameter, which is calculated using its major diameter and the spacing between each thread:
\[ \begin{align*}
D_{pitch} & = D_{major} - (0.6495*t_s) \\
A_{bolt} & = πr^2 = π(\frac{d_{pitch}}{2})^2 = \frac{1}{4}πd_{pitch}^2
\end{align*} \]
Tensile Stress on Each Axial Bolt During Hot Fire (Standard Configuration):
\[ \begin{align*}
& F_{up} = P_{injector}*A_{injector} \\
& F_{up} + (N*F_{bolt}) = 0 \\
& |F_{bolt}| = \frac{P_{injector}*A_{injector}}{N_{axial}} \\
& \\
& \\
Stress_{Tensile}: σ_{hot} & = \frac{|F_{bolt}|}{A_{bolts}} = \frac{P_{injector}*A_{injector}}{N*A_{axial}} \\
& \\
σ_{steel1} & = σ_{steel1} \\
\end{align*}
\]
Tensile Stress on Each Axial Bolt During Hot Fire (Outer Bolt Configuration):
\[ \begin{align*}
& F_{up} = P_{injector}*A_{injector} \\
& F_{up} + (N*F_{bolt}) = 0 \\
& |F_{bolt}| = \frac{P_{injector}*A_{injector}}{N_{axial}} \\
& \\
& \\
Stress_{Tensile}: σ_{hot} & = \frac{|F_{bolt}|}{A_{bolts}} = \frac{P_{injector}*A_{injector}}{(N_{inner}*A_{smallaxial})+(N_{outer}*A_{largeaxial})} \\
& \\
σ_{steel1} & = σ_{steel1} \\
\end{align*}
\]
Shear Stress on Each Radial Bolt During Hot Fire and Approximation of Shear Strength:
\[ \begin{align*}
& F_{up} = P_{injector}*A_{injector} \\
& F_{up} + (N*F_{bolt})=0 \\
&|F_{bolt}| = \frac{P_{combustion}*A_{combustion}}{N} \\
& \\
& \\
Stress_{Shear}: τ_{hot} & = \frac{|F_{bolt}|}{A_{bolts}} = \frac{P_{combustion}*A_{combustion}}{N*A_{radial}} \\
& \\
σ_{steel2} & = σ_{steel2} \\
& \\
τ_{steel2} & ≈ \frac{σ_{steel2}}{\sqrt{3}} \\
\end{align*} \]
Factor of Safety for Tensile Stress on Injector Bolts During Hot Fire (Standard Configuration):
\[ \begin{align*}
FOS_{tensile} = \frac{σ_{steel1}}{σ_{hot}} & = \frac{σ_{steel1}N_{injector}A_{axial}}{P_{injector}A_{injector}} = \frac{σ_{steel}N_{injector}πD_{pitch1}^2}{4P_{injector}A_{injector}} \\
& \\
& = \frac{σ_{steel1}N_{injector}π(D_{major1} - (0.6495*t_{s1}))^2}{4P_{injector}A_{injector}}
\end{align*} \]
Factor of Safety for Tensile Stress on Injector Bolts During Hot Fire (Outer Bolt Configuration):
\[ \begin{align*}
FOS_{tensile} = \frac{σ_{steel1}}{σ_{hot}} & = \frac{σ_{steel1}((N_{inner}A_{smallaxial})+(N_{outer}A_{largeaxial}))}{P_{injector}A_{injector}} \\
& = \frac{σ_{steel1}π((N_{inner}(D_{pitch1})^2)+(N_{outer}(D_{pitch2})^2)))}{4P_{injector}A_{injector}} \\
& \\
& = \frac{σ_{steel1}π((N_{inner}(D_{major1} - (0.6495*t_{s1})^2)+(N_{outer}(D_{major2} - (0.6495*t_{s2})^2)))}{4P_{injector}A_{injector}}
\end{align*} \]
Factor of Safety for Shear Stress on Radial Bolts of Combustion Chamber During Hot Fire:
\[ \begin{align*}
FOS_{shear} = \frac{τ_{steel2}}{τ_{hot}} & ≈ \frac{σ_{steel2}}{\sqrt{3}*τ_{hot}} = \frac{σ_{steel2}N_{chamber}πD_{pitch3}^2}{4\sqrt{3}P_{chamber}A_{chamber}} = \frac{σ_{steel2}\sqrt{3}*N_{chamber}πD_{pitch3}^2}{12P_{chamber}A_{chamber}} \\
& \\
& ≈ \frac{σ_{steel2}\sqrt{3}*N_{chamber}π(D_{major3} - (0.6495*t_{s3}))^2}{12P_{chamber}A_{chamber}}
\end{align*} \]