rdamus
Marine/Ocean
- Apr 21, 2006
- 8
hello all,
i'm in the process of designing a payload section for an autonomous underwater vehicle (e.g.,
this section will be rated to 1000psi. it is Al 7075-T6.
My problem background:
the payload section must fit inline with the vehicle diameter, which is 12.75". however, the thin-walled pressure vessel that will house our electronics is only 10" OD (0.35" thick) and will not be a structural part of the assembly, i.e. it does not support a bending moment, it will only undergo compression from the hydrostatic pressure at depth. this means that when we pull the vehicle out of the water, the entire section weight will have to be transferred to a cross-member. At the moment, i have a 2" OD aluminum tube (0.2" thick) that runs the length of the assembly whose centerline is located roughly 4.5" from the longitudinal payload centerline.
My question:
I am interested in knowing whether the 2"OD tube can support the weight of the payload section. To determine this, I have used a uniform load that represents the weight of the section (~1000N/m) to calculate the bending of this tube, using the cross-sectional inertia and Young's modulus of the tube. It appears that the 2"OD tube might deflect too much, so i am interested in suggestions on how to increase the strength of this system.
Ideally, i would like to know how to model the deflection of two beams that are rigidily mounted to a common endcap in the same vertical plane, but are of different cross-sections and located an arbitrary distance from one another... very similar to a composite I-beam in my mind, but i have trouble modeling the constituitive end-condition.
thank you for any insight. below is a cross-sectional rendering
Cross section of payload:
| | | | | | | | | |Uniform Load 1000N/m
v v v v v v v v v v
---------------------\ 12.75"OD
---------------------|
10"OD electronics |
---------------------|
..........................|..............Payload Centerline
| }
---------------------| }offset is ~4.5"
2"OD tube |.............}
---------------------|
--------------------/
i'm in the process of designing a payload section for an autonomous underwater vehicle (e.g.,
this section will be rated to 1000psi. it is Al 7075-T6.
My problem background:
the payload section must fit inline with the vehicle diameter, which is 12.75". however, the thin-walled pressure vessel that will house our electronics is only 10" OD (0.35" thick) and will not be a structural part of the assembly, i.e. it does not support a bending moment, it will only undergo compression from the hydrostatic pressure at depth. this means that when we pull the vehicle out of the water, the entire section weight will have to be transferred to a cross-member. At the moment, i have a 2" OD aluminum tube (0.2" thick) that runs the length of the assembly whose centerline is located roughly 4.5" from the longitudinal payload centerline.
My question:
I am interested in knowing whether the 2"OD tube can support the weight of the payload section. To determine this, I have used a uniform load that represents the weight of the section (~1000N/m) to calculate the bending of this tube, using the cross-sectional inertia and Young's modulus of the tube. It appears that the 2"OD tube might deflect too much, so i am interested in suggestions on how to increase the strength of this system.
Ideally, i would like to know how to model the deflection of two beams that are rigidily mounted to a common endcap in the same vertical plane, but are of different cross-sections and located an arbitrary distance from one another... very similar to a composite I-beam in my mind, but i have trouble modeling the constituitive end-condition.
thank you for any insight. below is a cross-sectional rendering
Cross section of payload:
| | | | | | | | | |Uniform Load 1000N/m
v v v v v v v v v v
---------------------\ 12.75"OD
---------------------|
10"OD electronics |
---------------------|
..........................|..............Payload Centerline
| }
---------------------| }offset is ~4.5"
2"OD tube |.............}
---------------------|
--------------------/