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Robot Construction
The extender links are made of composite materials and incorporate
four components:
1.
Foam Core
2. Inserts
3. Face Sheets
4. Motor Housings.
Foam core serves
a dual purpose: it provides shear stiffness and it defines the shape
of the final part. Because of the strength requirements and the
weight restrictions, polymethacrylimide (PMI) foam will be chosen
over other foam cores such as polyvinylchloride (PVC), polyurethane,
or polystyrene. Polymethacrylimide, when heat treated, is capable
of withstanding 100 psi at 250oF, which is required for manufacturing
the device links. Two-inch thick sheets of polymethacrylimide will
be bonded together with an epoxy adhesive until the desired thickness
is reached. Different densities of foam core will be used for different
areas of the links as dictated by the local stresses in those areas.
Once bonded, the foam blank will be machined to the required shape
and hand-sanded to the proper contours.
Carbon-epoxy inserts are laid-up on an aluminum mandrel to control
the critical surfaces (i.e., the connections to the motor housings).
This eliminates any costly carbon machining. An intermediate modulus
carbon pre-impregnated fabric (pre-preg) is chosen for its balance
of strength and stiffness. One ply of E-glass is used on surfaces
of the insert that contact aluminum to prevent any chance of galvanic
corrosion. Once cured, the inserts are potted into the foam core
using structural adhesive (Hysol EA9394). This two-part epoxy cures
at room temperature, but has a maximum operating temperature of
350oF which is well above the operating temperature of the enclosed
motors.
The face sheets are multi-directional fibers with a 50 MPSI modulus
which are pre-impregnated using a 250oF curing epoxy. It has an
average thickness of 0.060", and a maximum thickness of 0.120"
in several high-stress areas. In areas where the face sheets overlap
the carbon inserts, a co-curing film adhesive is used to promote
the bond. As each ply is laid-up, they are debulked at 29 inches
Hg for 1 hour at 100oF to eliminate any voids between plies. Once
all of the plies are consolidated, the part is jigged, vacuum bagged,
and autoclaved at 250oF and 100 psi for the final cure. The last
step to complete the project is bonding the aluminum motor housings
to the carbon inserts. Because of the poor bonding properties of
aluminum oxide, the surface of the housings is etched with chromic
acid and bonded within 16 hours to retain full bond strength. The
housings are potted into the carbon inserts using Hysol EA9394 adhesive,
completing the part.
Pictures
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