Centrifugal rpm governor for internal combustion engines

#The invention relates to a centrifugal rpm governor for internal combustion engines as described in the preamble to the main claim. A centrifugal rpm governor of this general type is already known (Swiss Pat. No. 231,322), in which the flyweight mass of the flyweight, which is embodied as bent at an angle, is firmly screwed to a lever arm of a bell crank, the lever arm being disposed approximately parallel to the longitudinal axis of the governor. The lever arm which supports the flyweight mass represents the extreme radial limitation of the centrifugal rpm governor; accordingly, its outer contour must at least partially approximate a cylindrical jacket, if the full diameter of the circle described by the flyweight is to be utilized in optimal fashion. For this reason, this bell crank is preferably made from a forged or cast steel part and then subjected to appropriate further processing. The result is that tedious and expensive processing is required merely for the bell crank alone, and this results in high manufacturing costs overall. The known governor type has the further disadvantage that the lever arm carrying the flyweight mass, which protrudes over the entire length of the flyweight, is susceptible to denting and bending and is unable to transmit large centrifugal forces; the possible usage of this governor is accordingly quite limited.

#Other known flyweights in angled form for centrifugal rpm governors in internal combustion engines are manufactured either completely of cast iron, or from a piece of forged steel or a section of shaped steel, and they require tedious additional processing. These flyweights also have a relatively great mass in the area of the bell crank rotary point, for reasons of stability, which has an unfavorable effect on the centrifugal force curve. In order to attain a certain governor behavior on the part of the governor, it may, however, be necessary for the centrifugal force curve, plotted over rpm, to be arched at the top; to this end, the center of the flyweight mass must be located as far as possible from the rotary point, in the area of the outermost end of the lever arm of the bell crank.

#The centrifugal rpm governor according to the invention and having the characteristics of the main claim has the advantage over the prior art that, because the separate mode of embodying the bell crank and the flyweight mass permit free choice of the substance from which the flyweight mass is to be made and of its form or shape, the center of the flyweight mass can be located at such a distance from the rotary point of the bell crank that the desired centrifugal force curve, having an initially steep force increase, results. The design of the flyweights according to the invention furthermore makes it possible to produce it inexpensively and in great quantities, without requiring expensive subsequent processing or costly finishing apparatuses.

#FIG. 1 is a side view, partially in cross-section taken along the line I--I of FIG. 2, of the structural components essential to the invention in the first exemplary embodiment;

#FIG. 2 is a generally horizontal plan view of the structural components essential to the invention as seen in the direction of the arrow A in the first exemplary embodiment;

#FIG. 3 is a cross sectional view through the associated flyweight in the region of the securing screw;

#Turning now to the drawings, a flyweight carrier 11 is secured on the drive shaft 10 of the centrifugal rpm governor according to the invention and in a flange 12 it has two transverse bores 13, which are disposed in spaced-apart fashion and at right angles to the longitudinal axis of the centrifugal rpm governor. Bearing bolts 14 are rotatably supported in these transverse bores 13 and on their ends which protrude beyond the flange 12 of the flyweight carrier 11, each bearing bolt 14 has a bearing bore 15, acting as a bearing point, for a bell crank 16 manufactured from sheet steel. The bell crank 16 is a portion of a flyweight 17 made up of two structural parts, the flyweight mass 18 of which is firmly attached by securing screws 19 to a crosspiece 16e of one lever arm 16a of the bell crank 16. (See FIGS. 3 and 4 as well.) The lever arm 16a of the bell crank 16 bearing the flyweight mass 18 is embodied as an angle bracket open toward the flyweight carrier 11, the parallel arms 16c and 16d of which laterally enclose the flange 12 of the flyweight carrier 11 and each contain one of the bearing bores 15 which act as bearing points. The crosspiece 16e connecting the two arms 16c and 16d has an end face 16f, which faces away from the bearing bores 15 and extend, in the resting position of the flyweights 17 (see FIG. 1), at least approximately perpendicularly relative to the longitudinal axis of the rpm governor. The flyweight mass 18 is firmly fastened by the securing screws 19 to the end face 16f (see FIG. 3) under extremely high initial mechanical stress, designed to be at the yielding-stress threshold of the substance from which the screws are made.

#This high initial mechanical stressing of the securing screws 19 is attained by means of the so-called "yielding-stress threshold tightening method". This method permits the choice of screws of relatively small dimensions and results in the highest possible resistance to loosening on the part of the securing screws, because during yielding-stress threshold tightening the tightening torque is of secondary importance, and the effect of friction is also not involved. (On this method, see the article, "Optimale Schraubverbindung in der Werkstatt" [Optimal Screw Fastening in the Workshop] in the journal VDI-Nachrichten, No. 9, Mar. 2, 1979, page 4.) This method has the further advantage that, as a result of the electronically monitored tightening, defects in the flyweight mass substance become recognizable, because in this case the theoretical tightening torque is not attained. For instance, porous areas (hollow spaces) can be detected in flyweight masses 18 manufactured from cast metal, as can defects resulting from insufficient thickness in flyweight masses 18 manufactured from sintered steel. From the standpoint of molding and stability, the sinter-press method is very advantageous, because in mass production it produces inexpensive and exact parts. Sufficient stability is attained in sintered steel parts having a thickness, for example, of .ltoreq.6.9 kp/cm.sup.2.

#The flyweight mass 18 is provided with a groove 21 (see FIG. 3) which extends over the crosspiece 16e of the bell crank 16. The base 21a of the groove 21 is fastened securely against the end face 16f of the crosspiece 16e of the bell crank 16, as a result of which the mounting position of the flyweight mass 18 is fixed in a form-locking manner. The groove 21 does not, however, perform a holding function, because the entire holding force produced by the yielding-stress limit tightening of the securing screws 19 is exerted between the frictionally engaged groove base 21a and the end face 16f. While one arm 16d of the lever arm 16a of the bell crank 16 carries only the bearing bore 15, the other arm 16c is connected to a second lever arm 16b, which has a cap bolt 22 on its free end. The centrifugal force of the flyweights 17 is transmitted to a governor sleeve 23 (for this element, see again FIG. 1) via the hardened, precision-turned jacket surface 22a of the cap bolt 22.