Pendulum-type accelerometer for electrically-actuated braking systems

Abstract: A pendulum-type accelerometer for electrically actuated braking systems has a pendulum (10) which comprises a sandwich of two outer metal leaves (10a, 10c) and a central elastomeric layer (10b) bonded between them. Only one of the metal leaves is secured, by adhesive 70, to a supporting structure so that damped flexure of the sandwich can occur freely. The accelerator comprises a unitarily moulded base (26), living hinge (32) and support arms (14,16) and a cross-beam to which the pendulum is secured. Means are provided for adjusting and retaining the attitude of pendulum relative to the base by movement of the support arms about the hinge.

Description: This invention relates generally to electrically-actuated braking systems for towed vehicles and the like, in particular the control means for such systems. More particularly still, the invention pertains to inertially-responsive control means for such braking systems, and in particular to inertial sensors, or accelerometers, for use therein. Electrically-actuated braking systems for towed vehicles have, of course, been known and used for some time, as shown for example by earlier U.S. Patents Nos. US-A-3738710, 3953084, 3967863, 3981544, 3909075, and 4030756 (certain of which are related to one another) which show various attributes of such systems and additionally discuss the background and historical developments in this field. While early such systems were manually-controlled, subsequent developments utilized various means for achieving automatic actuation, and such automatic systems have come to rely upon inertial sensors as the most predominant such control means since they enable the towed vehicle ("trailer") brakes to be applied automatically as and when braking is desired. Of course, many particular developments have occurred over the years for enhancing and improving such inertial systems, as shown by the earlier patents noted above, together with those cited therein, etc. What is believed to be the most successful and most frequently-utilized state of the art inertial sensing system is one analogous to that shown in the aforementioned US-A-3967863 and 3981544. This system uses a pendulum-type inertial sensor, or accelerometer, which responds to braking of the tow vehicle by immediately causing a controlled application of the brakes on the towed vehicle. As disclosed in these patents, the pendulum utilized in this system comprises a "sandwich" of laminated members, e.g., a pair of outer layers of thin sheet metal, in particular beryllium copper, and a centre layer of yieldable, elastomeric material, to which the outer metal layers are adhered. This construction is utilized to provide self-damping pendulum deflection, since the pendulum is mounted from its top and flexes laterally from the bottom when subjected to orthogonally-oriented acceleration forces, the pendulum being weighted at the bottom to augment such flexure. This lateral deflection of the pendulum requires that its two sheet metal layers move longitudinally with respect to one another, and this causes the elastomeric layer adhered therebetween to undergo elastic deformation since it is subjected to shear forces as a result of its side extremities moving in opposite longitudinal directions. This elastic deformation of the resilient inner layer of the pendulum is intended to damp pendulum deflection in a desirable manner, and to augment return of the pendulum to its normal position as inertial forces diminish, thereby contributing to smooth and controlled braking response as well as helping to remove the braking effects as quickly as possible when they are no longer needed. It has now been perceived that the desirable effects just noted were to a considerable degree sacrificed by the particularities of the pendulum configuration and mounting techniques used heretofore, which in fact have been the source of undesirable but largely unappreciated problems occurring in actual usage. Thus, for example, prior art implementations of the multiple-layer leaf-type pendulum have failed to provide the desirable benefits of its inherent self-damping capability, and have in fact introduced eccentricities and irregularities in the inertial displacement of the pendulum, resulting in inappropriate and undesirable braking effects exerted upon the towed vehicle, erratic in nature and disproportionate to the actual inertial effect causing the response. Indeed, at times the resulting braking response would be too great, or too small, while at other times the result could be chatter (i.e., rapid on and off or increase and decrease of braking effect), caused by resonance or other vibratory mechanical oscillation in the sensing pendulum. To a considerable extent, the adverse effects just noted have resulted from the manner in which the laminate-form leaf-type pendulum was mounted for inertia-induced flexure. That is, the multi-layer "sandwich" structure of the pendulum was typically mounted by use of a clamping means by which the top of the pendulum was clamped to a fixed, rigid mount or support structure. While some such suspensions also used a right-angled offset portion of one or both of the sheet metal layers of which the pendulum was formed to provide a means for suspending the pendulum from its top, the pendulum has heretofore also been rigidly secured by a clamp, which in effect squeezed the various layers of the pendulum against one another at the uppermost end, holding them tightly against a support disposed parallel to the axis of the pendulum. While this captured the upper end extremity of the pendulum and supported it in a dependable manner, it also caused serious but unappreciated problems. That is, as noted above, the lower extremity of the pendulum carried a weight, whose purpose is to accentuate the inertial effect on the pendulum caused by braking of the towing vehicle, and the customary manner of securing this weight to the lower extremity of the pendulum securely captures the entire lower extremity of the latter, i.e., both metal layers as well as the elastomeric internal layer. Accordingly, both the upper and lower extremities of the pendulum were rigidly captured relative to one another, with the result that the different layers were unable to move longitudinally relative to one another as the pendulum underwent lateral flexure, except to the very limited extent that such motion was made possible through tensional lengthening of one metal layer accompanied by compressive shortening of the other, and the extent to which the metal layers could separate by bowing and moving away from one another, stretching the elastomeric intermediate layer laterally through tension. These unintended and unappreciated effects changed the spring action of the pendulum dramatically, making it uncoordinated and irregular, while at the same time substantially nullifying the otherwise-obtainable smooth, coordinated, elastically-damped flexure of the pendulum, causing it to act erratically, in extreme cases actually causing it to "oil-can," i.e., erratically snap over-centre, with resulting erratic braking action. A further anomaly, probably based upon misconception, exhibited by prior pendulum-type inertial sensors of the type described is the use of comparatively long pendulum blades, by which comparatively large flexural excursion was obtained. This was thought necessary in order to provide desired resolution in the system, since the pendulum excursion is used to produce a graduated, proportional response for use in controlling the application of the towed vehicle brakes. That is, the pendulum motion is used to produce a corresponding analog signal in accordance with which braking is effected. For example, the pendulum motion may be used to either occlude or open a path for a light beam extending between a source and a photo detector, such that higher inertial levels causing greater pendulum deflection correspondingly increase the amount of light sensed by the photodetector. However, while it may be thought to be easier, as an abstract matter, to obtain higher degrees of control resolution by use of larger pendulum deflection, this is not the case where the longer pendulum contributes directly to instability of the aforementioned nature, creating a situation in which deflection increments are not uniform in relation to the corresponding inertial effects, and are not consistent. The invention overcomes the problems presented by the prior art, and particularly by US-A-3981544 which describes a multi-layer cantilever-type inertial sensor which comprises a flexible multi-layer beam. In the sensor described in that specification the beam is clamped both at the top where it is secured to the mounting structure and at the bottom where it is secured to a weight. According to the present invention, a multi-layer cantilever-type inertial sensor comprises a flexible multi-layer beam having first and second sides; a generally rigid support structure for the beam, said support structure having a beam-mounting surface disposed adjacent said beam near one end thereof; means for securing said beam to said support structure at said beam-mounting surface; and means for fixedly connecting the layers of said beam to one another at not more than one common place along their mutual length so as to preclude relative longitudinal shifting of said different layers of said beam at said common place but allow such shifting at all other points along their corresponding lengths upon arcuate flexure of said beam in response to inertial forces. With this arrangement, the layers of the beam are able to move longitudinally with respect to one another throughout their length with the possible exception of one place at which they are fixedly connected to one another. The present invention thus provides novel and highly advantageous solutions for the problems described above, based upon new perceptions and recognition of the underlying problems. More particularly, the present invention provides subtle structural changes and enhancements in the basic form and suspension of multi-layer inertial sensing pendulum used in electric braking systems of the type described above, by which the eccentricities and irregularities of the resulting braking control system are obviated and precluded, with the result that inertial sensing is carried on in a much smoother, distortion-free and extremely reliable manner which in addition is not subject to disruption due to such effects as inertial surges, "jerks," and the like resulting from such things as road surface irregularities, etc. Indeed, the inertial sensing function provided in accordance with the present invention is so smooth, reliable and distortion-free that the resulting system does not require the customary interconnection with the tow vehicle brake light circuit, by which most state of the art inertially-actuated electric braking systems are maintained in a de-energized state until the tow vehicle brakes are actuated and their brake lights energized, notwithstanding the fact that the inertial sensor is supposed to be controlling the braking system. That is, practically all inertially-actuated prior art systems have had to guard against undesired inadvertent actuation of the braking system due to inadvertent and undesired inertial sensor operation resulting, for example, from road surface irregularity such as pot holes, railroad tracks, etc., or for example, from erratic inertial sensor response to momentary manual application of the braking system control by which towed vehicle sway and the like are corrected. Accordingly, it is a major objective and advantage of the present invention to provide a new physical configuration for pendulum-type inertial sensors of the type used in electric brake control systems and the like, pursuant to which the problems of prior such devices are avoided and made obsolete. This major objective and advantage is achieved through a number of more particularly-cognizable physical attributes of the pendulum and its mounting structure, pursuant to which the overall aspect ratio of the pendulum may be changed in order to make its natural frequency of vibration substantially higher than previous such units (the pendulum beam being made less flexible, to thereby exhibit lower flexure per unit inertial load). Further, and of considerable importance to the underlying concept and structure of apparatus in accordance with the invention, a novel and advantageous type of mounting means is provided for the inertial sensing pendulum, pursuant to which elastomeric damping is perfected and made uniform, such that the advantages of this effect are finally realized and made possible. In addition, the invention contemplates the provision of a new and advantageous form of pendulum-mounting structure, which provides for high efficiency and reliability in the manufacture and assembly of the resulting unit, while at the same time achieving increased effectiveness and ease in achieving attitude correction for pendulum positioning, by which the pendulum may be readily adjusted to a vertical orientation following installation of the control unit in the tow vehicle, during which the particularities of the position in which the control is mounted often are such as to otherwise place the pendulum in a non-vertical position and thus interfere with normal sensing of horizontally-directed inertia forces, as normally occur during vehicle braking. The invention may be carried into practice in various ways but one inertial sensor embodying the invention will now be described by way of example with reference to the accompanying drawings, in which: Fig. 1 is an enlarged side elevational view showing the inertial pendulum and its supporting structure; Fig. 2 is an overhead plan view of the apparatus as shown in Fig. 1; Fig. 3 is an end view thereof; Fig. 4 is an end view similar to Fig. 3, but showing the apparatus repositioned for attitude adjustment of the pendulum in a first direction; Fig. 5 is an enlarged, fragmentary end view of the apparatus showing how the pendulum is mounted; Fig. 6 is an end view pictorially showing the prior-art pendulum-mounting arrangement as well as showing the resulting flexural bending mode exhibited by the pendulum under some circumstances; and Fig. 7 is an end view similar to Fig. 4 but showing the apparatus repositioned for altitude adjustment of the pendulum in a second direction. As indicated previously, the general nature of the pendulum-type inertial sensor used in what is perhaps the most successful and most frequently-encountered electric braking system is shown in US-A-3981544 and its related US-A-3967863. As may be seen in such patents, this form of inertial sensing pendulum comprises a multiple-layered "sandwich" comprising, in the preferred embodiment, a pair of beryllium copper strips which are disposed along opposite sides of, and adhesively secured along their length to a layer of elastomeric material (for example, "double-faced" rubber-based or other such elastomeric tape, preferably a thin, adhesively-coated polyester film such as that manufactured by Morgan Adhesive Company of Stow, Ohio, and identified as "IB-1190"). As illustrated in the aforementioned prior patents, the way such a pendulum is typically mounted is by bending the top end extremities of the beryllium copper strips laterally at right angles, so that the pendulum may be supported from its top by resting such offsets upon a slot-like support, and then rigidly clamping the pendulum blade against an adjacent vertical surface located immediately beneath the splayed top of the pendulum. Such a mounting arrangement is shown pictorially or schematically in Fig. 6, in which the pendulum is designated by the numeral 1, the support 2, and the clamp 3. In such a mounting, the splayed upper portion of the pendulum is merely to help initially suspend the pendulum from corresponding support, and is not in and of itself suitable for actual operation in a vehicle since, in the first place, such a suspension would merely permit the pendulum to rock back and forth under the influence of braking inertia, and would not produce any flexure of the pendulum blade or any resilient damping effect, etc., and, in the second place, such a mounting would not secure the pendulum against vertical forces generated when the vehicle encountered road surface irregularities, etc. The present invention recognizes that the typical prior art pendulum mounting, such as that illustrated in Fig. 6, severely inhibits consistent and gradual pendulum flexure in response to inertial loading, since it forces the pendulum to act, in effect, as a multi-leaf spring having both of its ends rigidly secured together. In such a situation, the resulting spring action is irregular and erratic, for the reasons noted previously. Indeed, the pattern of flexure for such a pendulum is likely to be that indicated in Fig. 6, in which the pendulum blade 1 actually defines a somewhat S-shaped curve rather than the anticipated and desired smooth arcuate curve which would result from a single leaf or from multiple leaves which are not fixed to one another at both ends. As may be appreciated, the motion pattern characteristic of a pendulum which exhibits such flexure is complex and non-uniform; consequently, this erratic pattern will also be present in the analog output of any sensor used to monitor and represent the pendulum motion, as well as in the resultant actuation of the brake system so controlled, which will thus embody irregular application, chatter, and other undesirable attributes. While the lower extremity of the pendulum used in accordance with the present invention continues to maintain the presence of a centred weight or mass which enhances pendulum flexure under the influence of braking inertia, the pendulum itself is mounted in an entirely different way at the top, providing for free longitudinal movement of the metal leaves relative to one another, under the influence of viscous damping provided by the interposed elastomeric adhesive layer which interconnects the two metal strips. Furthermore, as may be seen in the appended drawings, the inertial sensing pendulum 10 in accordance with the present invention is comparatively short with respect to its width, particularly in relation to prior art structures (in which the "free" portion of which, between the mounting at the top and the weight block at the bottom, was of the order of about three times longer). In this regard, the preferred length-width ratio for this "free" portion of the pendulum in accordance herewith is of the order of about 1:2, for the particular embodiment being described. Other important attributes of this form of pendulum are set forth in more detail hereinafter. The pendulum 10 is mounted on a pivotal or support assembly 12 comprising a pair of mutually-spaced upwardly-extending support arms 14 and 16 which carry a crossbeam 18 from which the pendulum 10 is suspended, preferably in a particular manner described more fully hereinafter. The mutually-spaced support arms 14 and 16 are also interconnected by a small-section blocking bar 20 which is disposed directly in alignment with a weighting block 22 secured at the bottom of the pendulum, so as to prevent undue excursion of the pendulum in that direction. The block 22 comprises a rectangular member mounted on the end of the pendulum 10 and having a transverse passage 24 in which a metal or other weight is secured. In this connection, it is to be noted that the weighting block 22 receives the bottom of the pendulum in a slot and is secured in place by adhesive or the like in a manner which provides a unified structure that captures the lower end of the pendulum and secures its different component layers with respect to one another. An alternative arrangement will be noted hereinafter. It is to be expressly noted that the mounting assembly 12 preferably comprises an integrally-moulded structure which includes not only the elements mentioned above (i.e., suspension arms 14 and 16, and crossarm 18) but, in addition, a support base portion 26 having mutually-spaced support arms 28 and 30, upon which the suspension arms 14 and 16 are mounted. The manner in which this is preferably accomplished is by moulding the entire assembly as an integral one-piece unit and providing a thin "living hinge" section 32, which allows for pivotal movement of the suspension arms with respect to their corresponding support arms, the extent of such movement being limited to a predetermined range by corresponding angularly-disposed shoulders 34, 36 and 38, 40, respectively. A suitable material for the integrally-moulded mounting assembly 12 is nylon, but other generally rigid polymers or the like may be equally suitable. As illustrated in the various Figures, the support base 26 is preferably formed so as to be directly mountable upon a printed circuit (i.e., "p.c.") board 42, such that the entire inertial sensor may be so mounted for rapid assembly procedures. Previously, pendulum attitude adjustment was provided by mounting the pendulum in a manner permitting relative angular motion of the entire pendulum support structure with respect to the instrument housing in which it was contained, as opposed to the more limited type of adjustment provided in accordance herewith, as just described. This change brings about significant advantages during assembly, since the approach used previously, as just described (and as may be seen in the various prior patents identified above) requires the use of elongated, flexible electrical conductors between the optical components and the remainder of the circuitry, in order to permit the large-scale motion of the entire apparatus just noted. This in turn mandates the use of manual assembly procedures, which are comparatively expensive and which also represent a source of potential defect as a result of human error. In contrast with the foregoing, the present invention provides for mounting of the optical components (here designated by the numerals 44 and 46, and constituting an "optical pair," i.e., a light source such as a photodiode and a light detector such as a phototransistor) directly upon the pendulum mounting assembly support base 26, in a manner whereby the height of the light beam provided by the optical pair (here indicated by the circular passage 48) is readily aligned and located in its desired position with respect to the pendulum. That is, the electrical conductors 50 and 52 of the optical pair extend downwardly through appropriate passages in support base 26 and through the p.c. board 42, where they are accessible for connection to the other electrical components of the brake-actuation system. Furthermore, in a preferred embodiment of the invention, the optical pair is positioned and mounted by use of a support base 26 having a separately-formed, and separable, mounting block 26a (Figs. 1 and 2), which fits into a recess defined between leg portions 26b of the support base. This facilitates mounting of the optical pair 44, 46, since one need only place the mounting block 26a atop the circuit board in the desired position, separate and apart from the remainder of the mounting assembly 12, and insert the leads 50, 52 through the corresponding passages in the mounting block and the p.c. board, bending the protruding portions laterally as shown in Fig. 1 to hold the optical devices and mounting block in position on the circuit board and at the same time automatically set the desired location of the optical path 48. That is, the thickness of mounting block 26a may be made such that the optical pair is automatically indexed in position at a desired level above the top of the support base 26 when they are mounted in the manner just stated. The mounting assembly 12 is secured to the p.c. board 42 with leg portions 26b disposed on each side of mounting block 26a, as shown in Fig. 2. Preferably, the attachment of support base 26 to circuit board 42 is accomplished by one or more pairs of spaced posts 54 which are moulded integrally as part of the pendulum mounting assembly 12 and are of a stiffly flexible nature, the preferred assembly procedure being to place the integral mounting assembly 12 upon the p.c. board 42 in the position just noted, and push the posts 54 through corresponding passages provided in the p.c. board for this purpose. Thus, virtually no assembly is required for the pendulum mounting assembly 12, apart from the simple mounting of the optical pair 44, 46 upon mounting block 26a in the manner described, after which the electrical leads 50, 52 may be flow-soldered in place to establish their electrical connections and secure the mounting block and optical pair to the circuit board. As previously indicated, the pendulum 10 is secured to the mounting assembly 12 in a novel and distinctive manner. More particularly, the entire securement for the pendulum is preferably accomplished by adhesive attachment of one of its metal leaves to the face of the crossbeam 18 in the desired location (which may be denoted by an integrally-moulded recess in the face of crossbeam 18, or by a slightly protruding peripheral frame 68 [Figs. 1 and 2] having a size substantially corresponding to that of the end of pendulum 10). In this manner, only one of the metal strips comprising the laminate pendulum structure 10 is actually secured to the mounting assembly 12, i.e., the metal strip 10c (Fig. 5) disposed closest to crossbeam 18. The other laminate components in the pendulum 10 are therefore only secured to one another at the top of the pendulum by their integral structure, i. e., the adhesively-connected elastomeric strip lob disposed between the two metal layers. A preferred adhesive 70 for use in mounting the pendulum 10 in this manner is the resin adhesive sold by Morgan Adhesive Company and identified as "Dymax 029," using activator 535; however, many commercial adhesives would no doubt be satisfactory for such an application. With the weight-carrying pendulum end block 22 secured in place (adhesively, with the end of the pendulum disposed within a slot, as illustrated) at the bottom of the pendulum 10, it will therefore be understood that the particular manner in which the pendulum is preferably secured to the crossbeam 18, as described above, provides for damped but unrestricted floating movement of the different layers of the pendulum longitudinally with respect to one another during flexure of the pendulum. That is, as the pendulum weight 22, 24 swings the lower part of the pendulum to the left, as seen in Fig. 3, under the influence of inertia created by tow vehicle braking, a flag or shutter 56 carried with the weight block 22 moves correspondingly to the left, thereby progressively opening a light passage between the optical pair 44, 46, along path 48. As this occurs, the pendulum 10 flexes laterally in a smooth arcuate bending mode, requiring that the metal strip 10a disposed on the left as seen in Fig. 5 begins to describe a curve of shorter radius than the metal strip 10c disposed on the right side of the pendulum as seen in that Figure. Consequently, the metal strip 10a located on the left must not be precluded from moving longitudinally upwardly with respect to the other strip 10c, as seen in such Figure, and this capability is provided by the novel mounting in accordance with the present invention. Although not shown in Figure 5, suitable clearance may need to be provided between the upper edge of the metal strip 10a and the overhang of the block 18 to facilitate this or the overhang may be omitted. Accordingly, as may be understood upon reflection, if the upper portion of the pendulum 10 is rigidly secured across all of its layers in the manner shown by Fig. 6, as was in fact done heretofore, and if the bottom of the pendulum is also secured across all of its layers, as was also done heretofore, the left-hand strip of metal in the pendulum would have to exhibit compound flexure, potentially including even certain bending in the nature of elastic buckling, in responding to the inertial forces applied (e.g., as illustrated at least partially in Fig. 6). Accordingly, the manner in which the pendulum mounting provided by the present invention facilitates the free flexure of the two metal strips in the pendulum, together with enabling the consistent and unrestricted viscous damping characteristic provided by the elastomeric connecting layer, will be appreciated by those skilled in the art. At the same time, it should be noted that the bottom extremity of the pendulum may also be secured in this general manner, i.e., by securing only one of the metal leaves to the weight block 22, leaving the other free to move longitudinally with respect thereto. If this approach is used, the top end of the pendulum may, if desired, be secured in a different manner, even by clamping, but it will also be understood that the preferred adhesive mounting structure for the top of the pendulum disclosed above is a significant improvement, in and of itself, from the standpoint of effective, efficient, and reliable manufacturing techniques, the upper portion of the mounting assembly (suspension arms 14 and 16, crossbeam 18, etc.) already being secured to the lower portion (including the support base 26 and support arms 28, 30, etc.) upon initial forming of the component parts. Similarly, it will be noted that the means for rotating the pendulum suspension arms 14 and 16 with respect to the support base, etc., in order to adjust the attitude (e.g., verticality) of the pendulum in a given setting, is preferably comprised of an integrally-moulded stub shaft and eccentric assembly 60 (Figs. 1 and 2), which includes an adjustment shaft 62 which is secured to suspension arm 16 through an eccentric connecting link 64 and a stub shaft 66, the axis of shaft 62 being centred upon the hinge pivot axis 48a. An operating knob 68a is also preferably moulded integrally with the adjustment shaft 62, to provide a convenient means for the vehicle operator to effect rotational adjustment as required, shaft 62 extending outward through the case wall of the instrument by means of an appropriate aperture (not specifically shown). Preferably, shaft 62 is encircled by an appropriate split grommet (not shown) which interposes frictional forces between the shaft and the housing wall through which it extends, such that the entire adjustment assembly 60, together with support arms 14 and 16 and crossbeam 18, will automatically be held, by such frictional forces, in desired positions of adjustment once rotational correction has been made. In the foregoing regard, it is important to note that the axis 48a of the living hinge 32 is preferably aligned directly upon the axis of the light beam passage 48. Consequently, corrective pendulum attitude adjustment comprises rotation about the optical axis of the detection pair 44, 46, so that the verticality of the pendulum may be corrected under any anticipated mounting position without changing the relative position of the shutter flag 56 with respect to such optical axis and thereby changing the inertial sensitivity of the device. In order to accommodate such corrective pendulum attitude adjustment, the support base 26 (in particular, the mounting block portion 26a thereof) forms a recess 72 (Figs. 1 and 2) into which the projecting end of pendulum flag 56 may move upon corresponding rotational movement of adjustment knob 66. At the same time, the need for hand-wiring during assembly which was characteristic of prior art devices in order to provide the requisite long flexible conductors which enabled pendulum attitude adjustment, is completely obviated. It should be noted that a preferred optical pair 44, 46 for use in connection with the invention is that manufactured by Motorola and identified as MLED 71 (infrared L.E.D.) and MRD 701 (phototransistor), or equivalent, which provides a highly restricted (small diameter) optical beam for interaction with the pendulum shutter 56. In particular, such an optical pair provides a detection beam which has a width of the order of only about 0.5 mm (twenty thousandths of an inch), and this makes possible the use of the relatively short, stiff (minimum deflection) pendulum, as noted above. In turn, use of such a short pendulum, with a length-to-width aspect ratio as noted above (i.e., on the order of about 1:2, where the metal strips are about .025 mm [0.001''] thick and the elastomeric layer about .075 mm [0.003''] thick), provides a highly desired stiffness modulus for the pendulum by which it merely deflects (flexes) enough to clear the optical path 48, i.e., of the order of .5 to .75 mm (0.020'' to 0.030'') under the influence of about one unit of gravitational force (i.e., one "G"), which contributes substantially to detection stability. In combination with the novel pendulum-mounting arrangement discussed above and the resulting unrestricted viscous damping provided by the elastomeric interlayer and made possible in this manner (by which critical damping of the pendulum is achieved), inertial sensing stability is so improved that the braking control unit may entirely omit the customary interconnection with the vehicle brake light circuit, heretofore considered an indispensable part of electric brake control apparatus whether inertially-responsive or otherwise. Nonetheless, there is no need to fear the presence of erratic or inadvertent actuation resulting from rough driving surfaces, etc., due to the extreme stability provided by the present improvements. At the same time, braking actuation of the towed vehicle occurs smoothly and effectively, and only as a result of intentional or intended actuation, and is of substantially better quality and resolution than that characteristically provided by prior art devices. It is to be understood that the foregoing description of a preferred embodiment of the invention is provided for purposes of the description and illustration, and not as a measure of the invention, whose scope is to be defined by reference to the ensuing claims. Thus, those skilled in the art may devise embodiments of the particular concepts presented in the foregoing illustrative disclosure which differ somewhat from the particular embodiment shown and described in detail herein, or may make various changes in structural details to the illustrated embodiment, without departing from the invention.

Claims: A multi-layer cantilever-type inertial sensor, comprising a flexible multi-layer beam (10) having first and second sides; a generally rigid support structure for the beam, said support structure having a beam-mounting surface disposed adjacent said beam near one end thereof; means for securing said beam to said support structure at said beam-mounting surface; and means for fixedly connecting the layers of said beam to one another at not more than one common place along their mutual length so as to preclude relative longitudinal shifting of said different layers of said beam at said common place but allow such shifting at all other points along their corresponding lengths upon arcuate flexure of said beam in response to inertial forces. Apparatus according to claim 1 in which the said layers are connected to one another at one common place, said common place being near one or the other end thereof. Apparatus according to claim 1 in which the means for securing the beam to the support structure extends between and interconnects the beam-mounting surface and a selected number of layers of the flexible multi-layer beam which is less than the total number thereof. Apparatus according to claim 1 or claim 2 in which the securing means comprises an adhesive (70). A sensor according to any of claims 1 to 4 in which one side of the beam and the beam-mounting surface are disposed generally parallel and contiguous to one another and are secured together by the securing means. A sensor according to any of the preceding claims which includes a weighting member secured to the beam at a point spaced from the location at which the beam is secured to the beam-mounting surface. A sensor according to claim 6 in which the weighting member is secured to only one layer of the beam. Apparatus according to any of claims 1 to 7 in which the support structure comprises in combination: an integrally-moulded structure of polymeric material defining a support base (26) and at least one generally rigid support arm (14,15) projecting from the base; a support beam (18) extending from the arm and providing the beam-supporting surface; means (32) for movably connecting the support beam (18) to at least one of said support arm and support base to provide a range of attitude-adjustment motion for said inertial sensor; and means for securing the integrally-moulded structure to a fixed support in a substantially non-movable manner whereby non-flexing electrical conductors may be used to connect components carried by said support means with other components carried by said fixed support. Apparatus according to claim 8 in which means for movably connecting the support beam (18) comprises an integrally-moulded hinge (32) formed unitarily with said integrally-moulded structure. Apparatus according to claim 8 or claim 9 in which the integrally-moulded structure includes means for mounting an optical component pair (44,46) comprising a light source and a light receiver disposed in mutually-aligned relation along a light axis. Apparatus according to claim 9 or claim 10 in which the fixed support comprises a circuit board and the means for securing the moulded structure comprises at least one integrally-formed member for engaging portions of said circuit board and in which the means for securing the integrally-moulded structure to a fixed support comprises at least one integrally-moulded attachment member formed unitarily with moulded structure and comprising a projecting lug adapted to extend into a recess formed in said circuit board. Apparatus according to any of claims 1 to 11 in which the multi-layer beam (10) is sufficiently stiff to have a deflection of less than about 1.27 mm (0.050'') when subjected to inertial forces of about 1.0 G. Apparatus according to any of claims 1 to 11 in which the multi-layer beam (10) is sufficiently stiff to have a deflection of from about 0.5 mm to 0.76 mm (0.020'' to 0.030'') under an inertial force of about 1.0 G. Apparatus according to any of claims 1 to 13 in which the multi-layer beam (10) comprises at least two thin blades juxtaposed with respect to one another and secured on opposite sides of a resilient damping member.

Inventors: AUSTIN BARRY GENE, ECCLESTON LARRY, AUSTIN, BARRY GENE, ECCLESTON, LARRY
Applicants: TEKONSHA ENGINEERING CO, TEKONSHA ENGINEERING COMPANY
Application year: 1990
Main classification: G01P1
IPC codes: G01P1, G01P15