Patent GB-879484-A (GB)
Title: Improvements relating to flameholder units
IPC: F23R3/18
Filed: 1958-11-18
Abstract: 879,484. Generating combustion products under pressure. UNITED AIRCRAFT CORPORATION. Nov. 18, 1958 [Nov. 18, 1957], No. 37115/58. Class 51 (1). [Also in Group XXVI] A flame-holder unit such as for use in reheat combustion equipment of an aircraft gas-turbine jet-propulsion engine comprises a large flameholder, a small flame-holder, a flame-spreader extending between the flame-holders and gas flow directing means located adjacent the flamespreader shaped to control gas flow along the flame-spreader. The reheat combustion equipment shown in Fig. 1 comprises an exhaust gas duct 16 to which fuel is supplied through injectors 24, an ignition device being provided at 28. The flame-holder unit 32 comprises an outer, trough section, ring member 38 and an inner trough section ring member 40, the ring members being disposed in planes which are relatively displaced along the axis 36 and being interconnected by one or more radiallyextending, trough section flame-spreaders 42. To control the flow along the flame-spreaders either exteriorly or interiorly thereof, vanes 56 as shown in Figs. 6 and 7, may be secured at spaced intervals along the leading edge portion 46 of the flame-spreaders, the vanes in this case being flat and acting to impede secondary flow along the flame-spreader. Alternatively, as shown in Fig. 8, the vanes 56 may be curved at their downstream ends so that in this case, the vanes act to induce or augment secondary flow along both the interior and exterior surfaces of the flame-spreader. The flame-spreader 42 in Fig. 9 is radially disposed in a plane normal to the axis 36 and is for use in interconnecting flame-holder rings lying in a common plane, flow controlling vanes 56 being disposed along the leading edge 46 of the trough to induce secondary flow along both the interior and exterior surfaces of the flame-spreader. The flame-holder unit shown in Fig. 13 is for use in a ducted fan engine, engine exhaust gases flowing through the duct 64, and air from the fan flowing through the surrounding duct 62. The flame-holder unit comprises an outer troughsection 38 disposed in the ducted air flow and an inner trough 40 disposed in the exhaust gas flow, the trough 40 being disposed rearwardly of the trough 38. The troughs 38 and 40 are interconnected by a trough section flame-spreader 42 which is inclined forwardly as opposed to the rearwardlyinclined arrangement shown in Fig. 1. Curved vanes 56 are mounted at the leading edge 46 of the flame-spreader trough so as to induce secondary flow towards the flame-holder trough 38. Strips 70, 72 may be secured to the vanes 56 as shown in Fig. 15, so as to supplement the effect of the vanes. In further arrangements, means are provided to prevent gas flowing outwardly along the flame stabilizers from spilling over the outer flameholder trough. Such means may be in the form of a vane projecting forwardly from the leading edge of the flame-holder trough, or alternatively the outer wall of the flameholder trough may be extended rearwardly. In another arrangement the flame-spreader trough is curved so as to connect with the flame-holder trough substantially tangentially. Specification 777,572 is referred to.