the device according to fig1 contains a bearing part or housing 1 and a shaft 2 which may be adjusted with respect to the housing . two side rings 3 and 4 , extending in two radial planes , are welded to the shaft and define a central shaft portion which forms a reel 5 for winding up a band - shaped hauling means 6 secured to it . fig1 shows the hauling means 6 and / or the band at a point where it is already almost completely unwound . the flat , braided band can be coiled up on the reel 5 in several layers , thereby filling the space between side rings 3 and 4 , without the band getting jammed and , thus , causing problems upon unreeling . on either end of shaft 2 there is a braking device 7 / 8 . the latter consists of a brake rotor 9 / 10 formed by the respective end portion of shaft 2 , either rotor containing six wings 11 and a brake housing 12 / 13 which surrounds the wings 11 . as can be seen from fig1 the two braking devices 7 and 8 are designed identically and symmetrically with respect to the radial central plane of the roping - down device . the six wings of either braking device are mounted on the one - piece shaft 2 with equal angles , e . g . they may be welded to said shaft . the wings 11 are shown as radially extending rectangular or square wings . however , also other wing shapes and deviations from the radial extension are possible . for example , the wings may be bent in the form of a shovel and they may with their inner edge also be adjacent to shaft 2 under an inclination towards the axis of shaft 2 , the wings 11 preferably being placed alternately with equal inclination in opposite directions . in their respective inner radial sector the wings 11 are connected with each other by two reinforcing rings 14 and 15 at the sides and are thereby stabilized . the radial width of these reinforcing rings may be between half and a third of the radial length of the lateral edges 16 and 17 of the wings 11 . the reinforcing rings 14 and 15 at the sides thereby extend to the outer edge 18 of the wings 11 . the two brake housings 12 and 13 essentially form the bearing part or housing 1 . either housing consists of a circumferential surface 19 , which is radially spaced opposite the outer edges 18 of the wings 11 , and of two annular facings 20 and 21 which are axially spaced opposite the lateral edges 16 and 17 respectively . the facings 20 and 21 at their outer circumference verge into circumferential surface 19 and with their inner circumference are slipped on shaft 2 and / or the brake rotors 9 and 10 . on their inner circumference , either of the facings 20 and 21 has a ring flange 22 projecting to the wings 11 which flange substantially bridges the axial distance from the wings and which leaves only a narrow running groove . the two brake housings 12 and 13 on shaft 2 are secured in their position by a connecting rod 23 with a diameter of e . g . 10 mm which forms part of housing 1 which , on the lower side , touches the outer side of the circumferential surface 19 of the two brake housings 12 and 13 and which is rigidly connected with said housing e . g . by welding . also on the upper side of the housings 12 and 13 there may be provided a band - iron fixed link ( not shown ) which corresponds to connecting rod 23 . in this case it is useful to laterally offset this link by half of the diameter of shaft 2 and to provide it with a longitudinal groove which serves to guide hauling means 6 which passes through , but which , however , does not extend over the whole axial length of reel 5 , but should only be approximately half as long so that , upon unwinding of hauling means 6 , the roping - down device inclines less with respect to the horizontal central position shown in fig1 than corresponds to the given winding width . at the unwound upper end of the band - shaped hauling means 6 , which is not visible in fig1 there is provided an anchoring device ( not shown ) which renders possible that the device is secured , for instance , in the roof or window area of multistorey buildings , on towers , bridges or also on helicopters . on housing 1 a load suspension device 24 is shown which is linked to the connecting rod 23 in the form of a weldment and includes two bearing rods 25 and 26 which are inclined in opposite directions , a reinforcement 27 , and an eye hook 28 in the radial central plane . fig1 in reduced scale indicates a person which is suspended on the eye hook by means of a belt in order to be roped down . a protecting tube 29 of fire - proof synthetic material encloses the roping - down device with the exception of the anchoring means ( not shown ) and the load suspension device 24 . the protecting tube 29 is provided with an axial groove 30 through which the band - shaped hauling means 6 is guided . each brake chamber 31 defined in brake housings 12 and 13 , which receives the wings 11 of the respective brake rotor 9 or 10 is , in a manner not shown , partly or completely filled with a granular material such as silica sand which was drenched with oil -- in the case of the tested device approximately 10 % by volume oil in the sand . the granular material may occupy from about 75 % to 100 % of the free volume of the brake chamber 31 . in the case of the tested embodiment a hollow rope braided of poly - p - phenylene - terephtalamite ( ppd - d ) filament was used . this synthetic material has a tensile strength which is approximately five times as high as that of steel and it keeps its characteristic features up to approx . 200 ° c . the band - shaped hollow rope has profile dimensions of 12 × 2 mm . the length of the coiled - up rope may , for instance , be 25 or 50 or 100 m and more . the device may , for example , be welded together of sheet steel or aluminium sheets with a thickness of 1 mm and 2 mm respectively . the shaft is designed as sleeve shaft so that hauling means 6 can simply be passed through an aperture in the side of shaft 2 with one of its ends and may be secured on the shaft by a knot . in addition to that , the hollow shaft can be designed with a sufficiently large diameter without excessive increase of weight so as to avoid extreme bends of hauling means 6 which is made of the comparatively brittle synthetic filaments . good results have been achieved with a roping - down device in which the axial distance between the lateral edges 16 and 17 of the wings 11 and the facings 20 and 21 of the brake housings 12 and 13 is 5 mm and the radial distance between the outer edges 18 of the wings 11 and the circumferential surface 19 of the brake housings 12 and 13 is 10 mm , while the brake housings 12 and 13 have an axial width of 60 mm and an outer diameter of 170 mm as well as an inner diameter of 50 mm , which corresponds to the diameter of shaft 2 . the axial width of reel 5 with side rings 3 and 48 which is positioned in between , is approximately 120 mm . this means a length of 250 mm and a diameter of 172 mm for the protecting tube . it has been observed in tests with the above described device that excessive heating is avoided by means of the capacity for taking in the energy produced in roping - down , which capacity is available because of the oil - drenched sand filling and the metal construction . a medium increase of temperature of only about 2 ° k . per 100 kp roping - down load and 10 m roping - down height has been calculated . correspondingly , roping - down from a height of 100 m and more is no problem with respect to the heating , because the device may be provided with a protecting heat insulation . as has already been mentioned , the energy produced in roping - down as a consequence of centrifugal friction forces and non - centrifugal friction forces ( sand circulation ) is taken into the braking device . the non - centrifugal friction forces may be augmented by using less oil and / or more sand in brake housings 12 and 13 as well as by reducing the number of the wings 11 and / or their distance from the walls of the brake housings . the centrifugal friction force may in this case be smaller , which allows a smaller diameter of the brake housing and , thus , a roping - down device of especially practical dimensions , which , however , has the same efficiency . instead of doing so , it is certainly also possible to increase the load which may be roped down without rising of the roping - down velocity . according to fig3 and 4 a roping - down device is provided which is designed and which operates in a way corresponding to the above described roping - down device of fig1 and 2 . for this reason corresponding parts are designated with the same reference numbers , distinguished only by an apostrophe which is added to the respective number , and these parts are not described again . the special feature of the device as shown in fig3 and 4 is that there is provided a manual brake 32 in addition to the automatically operating braking devices in the brake housings 12 &# 39 ; and 13 &# 39 ;. the hand brake 32 includes a brake bar 33 extending through the hollow shaft 2 &# 39 ; which , on either side , projects slightly with respect to the brake housings 12 &# 39 ; and 13 &# 39 ;. on the end of the bar , which projects with respect to shaft 2 &# 39 ; and is positioned on the left - hand side in fig3 a brake plate 34 is attached and is either rigidly connected with brake bar 33 by welding or held on brake bar 33 by means of a bar flange . the brake plate 34 is designed as a long plate with a width which corresponds approximately to the outer diameter of shaft 2 &# 39 ; and is on either end provided with a bore by which it is guided unto guide journals 35 and / or 36 which project axially from the outer facing 20 &# 39 ; of brake housing 12 &# 39 ;. also on the right end of the bar there is a corresponding brake plate 37 , which is attached such that it may slide , said brake plate being guided by two guide journals in an appropriate manner and being supported at its outer side by means of a wing nut 38 which is srewed unto a threaded section 39 of brake bar 33 and is protected against loss by means of a cap 40 . as can easily be seen , the brake plates 34 and 37 , which , on their inner sides , can be provided with a brake lining , may be engaged or disengaged with the braking surfaces 41 and 42 which are defined by the facings of sleeve shaft 2 &# 39 ; by tightening or loosening wing nut 38 . the manual brake 32 allows not only an individual reduction of the roping - down velocity which develops as a consequence of the automatically operating braking devices , but , which is more , the person roped down can at any time cause an intermediate stop by srewing up the wing nut and can continue roping down after that . thus , this device is suited also for working at normally inaccessible fronts of buildings , for mountaineering and for other cases in which similar requirements are made . fig3 indicates also an upper connection 43 between the brake housings 12 &# 39 ; and 13 &# 39 ;, which is laterally offset by half of the diameter of shaft 2 &# 39 ; and is provided with a running groove 44 for the guide of hauling means 6 &# 39 ; the length of which is smaller than the distance between the two side rings 3 &# 39 ; and 4 &# 39 ; of the reel . while the invention has been illustrated and described as embodied in specific embodiments of a roping - down device , it is not intended to be limited to the details shown , since various modifications and structural changes may be made without departing in any way from the spirit of the present invention . without further analysis , the foregoing will so fully reveal the gist of the present invention that others can , by applying current knowledge , readily adapt it for various applications without omitting features that , from the standpoint of prior art , fairly constitute essential characteristics of the generic or specific aspects of this invention .
the device for roping down includes a shaft 2 with a central portion which forms a reel 5 for coiling up band rope 6 . the two end sections of shaft 2 form brake rotors 9 and 10 , which are equipped with wings 11 . the wings 11 , which rotate during the uncoiling of the band rope operate in brake chambers 31 enclosed by brake housings 12 and 13 , these brake chambers being partly or completely filled with sand . in case of roping down , braking devices 7 and 8 operate automatically and produce a comparatively high braking power which heavily increases as the rate of descending increases . thus , a constant roping - down rate as a function of the respective load is achieved which rate is used for a safe impact on the ground .