Device for filling the forming chamber of semi-liquid mass of rocket inhomogeneous fuel to obtain a solid rocket propellant charge with a central longitudinal bore

摘要

the subject invention is device for filling chamber (7) outgoing semi-solid mass of rocket fuel (2) in order to obtain continuous non-uniform cargo rocket fuel (2) with a central longitudinal aperture constructed with dispenser (1) semi firm mass (2), equipped with zaw u00f3r triggercombined by the trigger (6) with a formuju0105cu0105 (7) covering the core (8) formuju0105cy completed from top stou017ckowym kou0142pakiem osu0142onowym (10) embedded centrally in its bottom, with a discharge channel (6) has a vacuum hole (11) next train made in the lateral wall, the u0105czu0105cy channel (6) of the vacuum system.and furthermore, in the tab (6) set is its flange (14) of the perforated disc (15) that distributes the stream of rocket fuel (2) situated on przelotowym of, open vacuum (11).the device is that the perforated disc (15) has three identical openings przelotowe (16) peripherally spaced equidistant from each other, with each opening (16) has two elongated walls, each lying equidistant from each other and from the circuit revolve ka (15) connected with both ends of the raised, favourably pu00f3u0142kolistymi wallsconical cowl (10) and a lid (8) formuju0105cego core has three arms (17) spaced equidistant around the circumference of the base conical flask, lying along the chamber (7) and affecting their outgoing edges of its inner wall, each arm ( 17) spinner osu0142onowego (10) has the shape of a cross section of an isosceles triangle of cairns.whose upper - wierzchou0142kowa edge (18) is located in a vertical plane passing through the perforated diaphragm (15) along a diameter lying between its two adjacent openings (16) in an equal distance from them and at the same time, passing through the third remaining symmetrically a hole (16).