This invention relates to apparatus and procedures for instant disconnection of an electrical connector pair that has been threaded together.
Very broadly, two general kinds of connectors are known for connecting and disconnecting modules such as mating electrical circuits: threaded- or screw-type connectors, and bayonet-type connectors. Threaded connectors have the advantage of strength and stability, but unfortunately are time consuming to disconnect.
Bayonet or snap-together connectors are sometimes regarded as prone to accidental disconnection. Thus they pose a risk of possible damage to equipment—and in some cases more-serious adverse consequences.
Another reason for avoiding bayonet connector designs, however, is much more difficult to disregard: some devices must mate with apparatus that by law (or government-promulgated regulations) must have certain completely specified connection geometry. That geometry may include screw-together attachment components.
In particular one very commonly required standard military unit is known as a “D-38999 series III” connector. It has a triple-start Acme thread, and is designed to tolerate high vibration and shock; however, being a screw-together connector it is objectionably slow to disconnect.
Quick-disconnect variants of this connector are particularly favored for hostile subsystems, such as for example bombs and missiles, that are connected to aircraft and must automatically separate from the craft in flight. Under the conditions of such deployment, rapid but extremely reliable disengagement is necessary.
Neither time nor manual access is usually available for tending to the connectors manually if automatic release fails. As will be understood, midair failure to disengage can produce severe damage to the aircraft and potentially major hazards to its crew.
Three prior-art devices attempt to accommodate the general geometry of the D-38999 connector. A first of these requires a modified (i. e., not standard) version of the D-38999 plug, as well as the mating receptacle.
In this variant plug, three or more balls are captured between two metal pieces linked to the shell, and the mating receptacle is grooved rather than threaded. In a quiescent condition the balls lock the plug and receptacle together longitudinally—functioning in lieu of standard threads in the receptacle.
One of the metal pieces forms a cammed shape, so that when pulled back (by retracting the shell) it releases the balls. The balls thereby become loose and move in the groove of the receptacle. When the shell is released it forces the balls into the groove.
A second device that attempts to accommodate the general geometry of the D-38999 geometry also requires a variant of the plug as well as the receptacle. In this case the receptacle has a bayonet pin that projects from the receptacle.
To connect the plug and receptacle together, a slotted screw mechanism is screwed over the bayonet pin, locking the receptacle and plug together. Here it is this pin which functions in place of threads in the receptacle. For quick release, the slotted mechanism opens to release the bayonet pin.
A major drawback of both these first two devices is that they in fact require the modification. That is, neither can work with the standard D-38999 series III plug; hence the standard military specification is not applicable to either the receptacle or the plug.
A third prior device carries an internally threaded ring on the inside of the receptacle, generally like the standard receptacle, but the threaded ring is not continuous all the way around the receptacle. The ring instead takes the form of segments, or sections, usually six segments around the receptacle circumference.
To connect the two half-connectors together the plug is screwed into the threads, in the usual way. For quick disengagement the thread segments are retractable radially, so that in principle it is not necessary to unscrew the components from each other—they can simply come apart longitudinally.
Thus the receptacle of this third device, unlike the first two, undertakes to mate with a completely standard D-38999 series III plug. Only the receptacle is nonstandard. Unfortunately the release is unreliable: the segmented threads of the receptacle sometimes catch on the plug threads instead of retracting cleanly.
Since the standard threads are triple-start, the longitudinal spacing of adjacent threads is quite fine. Hence the interfitting of the plug and receptacle threads entails a relatively large total contact surface area at each segment.
Disengagement of such finely spaced large contact areas develops significant friction—so that the segmented threads tend to catch, in retraction, rather than separating smoothly. While it is not intended to unduly criticize the efforts of prior artisans in the field, this is a highly unacceptable mode of failure since it can rip the associated cabling and attached hardware bodily out of the host system.
As can be now understood, the prior art—although providing many thousands of different connector configurations—has left some refinements to be desired in the area of threaded electrical connectors that are very quickly disconnected.
The present invention provides just such refinements. In preferred aspects and preferred embodiments of the invention, mechanisms are provided that thread together with standard screw-together connector plugs in a way that appears conventional, and in fact can be unscrewed in a likewise conventional-seeming way—but that also can be instantaneously disconnected, either with one hand or by automatic machine operation of a rip cord or the like.
This result provides a significant improvement in terms of the compatibility of quick-disconnection devices with completely standard specifications of mating apparatus. All this is set forth in the Detailed Description section of this document, with reference to the accompanying drawings—of which:
In a preferred embodiment, the invention 11-19, 21-29′ (
The preferred embodiment of the invention does not use continuous threads as such, but rather engages the mating threads of the other half-connector 31 by a multiplicity of circumferentially distributed thread-engagement pins 21. Three such pins are illustrated (
As noted earlier, the plug 31 may be a multiple-start type—for instance a military-specification “D-38999 series III” half-connector, with a triple-start Acme thread. In such a case it is essential that the pins be positioned in the receptacle precisely, to properly engage the finely spaced plug threads.
In most cases the pins are ideally spaced equidistant about the periphery of the assembly 11-19, 21-29′, especially about a coupling sleeve 11 and outer sleeve 12. Holes 22 in both these sleeves hold each pin in a radial alignment.
Each pin also stands in a respective axial slot 27, 29′ (best shown in
A very generally central bulb or enlargement 24 is formed in each pin 21, between the radially outer and inner pin segments 23, 25. At the radially innermost end of each pin 21, the tip 28 is ideally shaped to match the cross-sectional thread profile of the mating connector 31—e. g. often but not necessarily tapered.
The central bulb 24 rests in angled grooves 26 formed in opposing faces of the corresponding actuator slot 27. Axial motion of the actuator sleeve cams the pin radially in or out through its alignment holes 22.
For connection, ideally the mating unit 31 is screwed in, or if preferred the lanyard sleeve 13 can be pulled out (
The coil spring seats against a retaining ring 19 that references the spring to the outer sleeve or shell 12 and thus to the pins 21. This method of engaging the half-connectors is somewhat undesirable in that the threads may not happen to be aligned precisely with the pins; to minimize the likelihood of problems due to use of this method, the threaded connector ring at least should be slightly rotated about the system axis to obtain a good engagement. With square-profile threads this technique may not be advisable.
To disengage the connectors, the lanyard 43 (
As the actuator sleeve retreats, each pin 21 rides up its ramped groove 26 in the corresponding slot 27. This cam action extracts all the pins simultaneously from the mating threads and thereby instantly releases the two half-connectors 17, 31 from each other—even if the threaded half 31 was initially screwed into place.
It has been found that this arrangement of pins provides an excellent solution to the previously mentioned prior-art problem of obtaining smooth, reliable and very fast disengagement. Yet this solution is achieved with a D-38999 series III plug 31 that is completely standard.
The foregoing details are intended to be merely exemplary, not exhaustive, and therefore should not be misinterpreted as limiting the invention or its applications to what has been specifically set forth. A person skilled in the field will understand that various other aspects and embodiments of the invention can be straightforwardly substituted.
This document claims priority of U.S. provisional patent application Ser. No. 60/615,670, filed Oct. 4, 2004.
Number | Date | Country | |
---|---|---|---|
60615670 | Oct 2004 | US |