Back to results
US 4,352,707 AGranted
Composite repair apparatus
AssigneeGrumman Aerospace Corporation
InventorsLeonard M. Wengler, Harold J. Wicker, Michael J. Masica, Jr.
Life of this patent
Estimating the term…
Abstract
A composite repair device including a plurality of resistive heating zones, each having independent temperature and rate of temperature rise controls, to compensate for the greater heat loss at the outer areas of a composite patch.
Claims7
A portable composite repair apparatus comprising:
- a flexible, non porous diaphragm which may be fitted over a composite patch which has been placed on a surface to be patched;
- a plurality of resistive heating elements, each of said resistive heating elements being integrally formed within the diaphragm and having a surface power density corresponding to a maximum heat loss density of an area on the surface to be patched with which said resistive heating element registers;
- and
- a like plurality of temperature control units, each of which may be adjusted to control a rate of temperature rise and an ultimate curing temperature in an associated resistive heating element.
1 more element
A portable composite repair apparatus comprising:
- a flexible, non-porous diaphragm which may be fitted over a composite patch which has been placed on a surface to be patched, said diaphragm having a series of concentric grooves on a side thereof which faces the surface to be patched;
- a means for applying a vacuum to the concentric grooves whereby a chamber formed by the diaphragm and the surface to be patched may be substantially evacuated to collapse the diaphragm against the surface to be patched;
- a plurality of resistive heating elements, each of said resistive heating elements being integrally formed within the diaphragm in an area within the periphery of the concentric grooves, each element having a surface power density corresponding to a maximum heat loss density of an area on the surface to be patched with which said resistive heating element registers;
- a plurality of temperature probes in one to one correspondence with the heating elements, each implanted in the area of the diaphragm of a corresponding heating zone to directly contact the surface to be patched;
- a plurality of control circuits in one to one correspondence with the heating elements, each including thermostat means electrically connected to a corresponding temperature probe and current limiting means adjustable to control a rate of temperature rise of an associated heating element, each of said thermostat means being adjustable to control an ultimate curing temperature to which the composite patch is subjected by the associated heating zones;
- and
- a timer control which may be set for a desired total curing cycle time and will shut off the resistive heating zones a predetermined period before the desired total curing cycle time has elapsed and will shut down the vacuum application means when the desired total curing cycle time has completely elapsed.
4 more elements
Dependencies are inferred from the claim text.