Design engineering discussion
Posted: Sat Oct 10, 2009 8:58 pm
I want to open up with my engineering techniques for the Striker to receive feedback, criticism and advice. I posted this as its own topic because the discussion could prove valuable to anyone designing a high pressure cannon. I will go over my choice of materials and the way I determined that the design is structurally sound to withstand the pressures of 5x combustion.
Chamber material choice is 3 1/2" x 10" SCH40 6061-T6 aluminum pipe and 5/8" thick 6061-T6 end caps. Six full length studs hold the end caps to the chamber. The studs are made of grade B7 studs, commonly used for pressure vessel applications. Stress analysis was conducted using Solidworks to determine that the chamber and end caps were strong enough to withstand a maximum theoretical pressure 600psi and an operating pressure of 375psi according to HGDT using a golf ball. The safety factor in the design for these components is as follows:
Chamber pipe @ 600psi : 3
End caps @ 600psi : 2.9
Chamber pipe @ 375psi : 4.6
End caps @ 375psi : 4.9
Next, I had to make sure the studs would be strong enough. This took a different approach to find the safety factor. I used a thread stress area calculator that multiplies the area of a given thread by the materials tensile strength. Since the studs are being pulled in 2 directions, the strength of each stud had to be divided by 2 in order to arrive at the correct value.
Using 5/16-24 studs, the min pitch diameter is 0.2806" and at 24 threads per inch, this results in a tensile stress area of 0.05602. It is this value that is multiplied by the materials tensile strength of a min. of 125,000 psi. This results in an ultimate tensile strength of each stud being 7002.5lbs. The studs are torqued to about 80%, so 80% of this strength value equals 5602lbs per stud. This is then divided in half since each stud is being pulled in two directions, equalling 2801lbs of strength per end cap. Six studs equals 16,806lbs of strength per end cap.
Each end cap is being pushed by 7,200lbs of force @600psi and by 4,500lbs of force @375psi. This results in a stud safety factor of 2.3 and 3.73 respectively. These values are conservative because the 125,000 of tensile strength per stud is a min value, and even if the 80% torque is exceeded by the combustion force, it doesn't mean the studs will break. They will simply extend briefly and then retract again. If this is repeated many times the studs can fatigue and eventually fail. So all of the safety factors appear to be inline and appropriate with each other.
The nuts holding the studs are grade 8, which are high strength nuts. Each nut is stronger than than the stud itself, and since the stud's effective strength is divided by 2, then that means that the nuts themselves would be the last of all things to fail.
Side note: This cannon uses pure O2 and MAPP. A modelling program predicts a max pressure of 440psi with pure O2 and MAPP. I used the higher value of 600psi predicted by HGDT assuming the use of air and MAPP to be on the safer side. I am not a math wizz by any means, so I have to rely in these modeling programs to do these chemistry oriented calculations for me. The 1 1/2 SCH10 6061-T6 barrel is not of much concern as there are no holes in it, unlike the chamber and thus results in a safety factor of 5.5 @ 600psi. All safety factors are yield based and not based on ultimate failure.
Lets stop here and begin the discussion.
Chamber material choice is 3 1/2" x 10" SCH40 6061-T6 aluminum pipe and 5/8" thick 6061-T6 end caps. Six full length studs hold the end caps to the chamber. The studs are made of grade B7 studs, commonly used for pressure vessel applications. Stress analysis was conducted using Solidworks to determine that the chamber and end caps were strong enough to withstand a maximum theoretical pressure 600psi and an operating pressure of 375psi according to HGDT using a golf ball. The safety factor in the design for these components is as follows:
Chamber pipe @ 600psi : 3
End caps @ 600psi : 2.9
Chamber pipe @ 375psi : 4.6
End caps @ 375psi : 4.9
Next, I had to make sure the studs would be strong enough. This took a different approach to find the safety factor. I used a thread stress area calculator that multiplies the area of a given thread by the materials tensile strength. Since the studs are being pulled in 2 directions, the strength of each stud had to be divided by 2 in order to arrive at the correct value.
Using 5/16-24 studs, the min pitch diameter is 0.2806" and at 24 threads per inch, this results in a tensile stress area of 0.05602. It is this value that is multiplied by the materials tensile strength of a min. of 125,000 psi. This results in an ultimate tensile strength of each stud being 7002.5lbs. The studs are torqued to about 80%, so 80% of this strength value equals 5602lbs per stud. This is then divided in half since each stud is being pulled in two directions, equalling 2801lbs of strength per end cap. Six studs equals 16,806lbs of strength per end cap.
Each end cap is being pushed by 7,200lbs of force @600psi and by 4,500lbs of force @375psi. This results in a stud safety factor of 2.3 and 3.73 respectively. These values are conservative because the 125,000 of tensile strength per stud is a min value, and even if the 80% torque is exceeded by the combustion force, it doesn't mean the studs will break. They will simply extend briefly and then retract again. If this is repeated many times the studs can fatigue and eventually fail. So all of the safety factors appear to be inline and appropriate with each other.
The nuts holding the studs are grade 8, which are high strength nuts. Each nut is stronger than than the stud itself, and since the stud's effective strength is divided by 2, then that means that the nuts themselves would be the last of all things to fail.
Side note: This cannon uses pure O2 and MAPP. A modelling program predicts a max pressure of 440psi with pure O2 and MAPP. I used the higher value of 600psi predicted by HGDT assuming the use of air and MAPP to be on the safer side. I am not a math wizz by any means, so I have to rely in these modeling programs to do these chemistry oriented calculations for me. The 1 1/2 SCH10 6061-T6 barrel is not of much concern as there are no holes in it, unlike the chamber and thus results in a safety factor of 5.5 @ 600psi. All safety factors are yield based and not based on ultimate failure.
Lets stop here and begin the discussion.