![]() The bird deflector and air replacement system described in claim 5, wherein the smaller end of the frustum is shaped as one of a circle, rectangle, triangle, half-circle, or as required to conform to the inlet shape of the jet engine.ħ. The bird deflector and air replacement system described in claim 2, wherein the smaller end of the frustum is detachably connected adjacent the inlet of the jet engine.Ħ. The bird deflector and air replacement system described in claim 2, wherein said longitudinal and lateral members are shaped in one of round, rectangular, or triangular cross sections with a corner of each nonround member pointing outwardly for maximum air flow therepast.ĥ. The bird deflector and air replacement system described in claim 2, wherein the longitudinal members are sloped to meet at a forward end thereof, and the lateral members extend between respective adjacent longitudinal members at spaced intervals therealong.Ĥ. A bird deflector and air replacement system for an inlet of a jet engine, comprising longitudinal and lateral members forming a contoured perforated guard open at the rearward end thereof, and a frustum having a larger forward and a smaller rear end completely spatially outward of the inlet and having the larger end connected to the open end of the perforated guard, with the smaller end connected adjacent the inlet of the jet engine, wherein the total inside air flow through the frustum into the jet inlet substantially equals the total air flow blocked by the longitudinal and lateral members.ģ. A bird deflector comprising spaced interconnected elements, and an accompanying air replacement apparatus operatively connected to a frontal inlet cowl of a jet engine, said air replacement apparatus continuously receives air flow and directs said air flow via continuously open passages(s) into the frontal inlet of an operating jet engine substantially replacing the total air flow being blocked by the bird deflector elements, said air replacement apparatus continuously open passage(s) comprising one of a frustum having a large forward end, and a small rear end secured to the inlet cowl at the forward end thereof an inlet cowl formed as a frustum a cylinder secured at the rear end of the inlet cowl and extended over openings formed in the inlet cowl or an inlet cowl formed as a cylinder having a perforated flanged forward end, each respectively serving to supplement the air flow through openings between the spaced interconnected elements of the bird deflector to provide the total air flow required by the jet engine for all operating conditions.Ģ. HYDRAULIC SYSTEM OF CONSTRUCTION EQUIPMENT, HAVING FLOAT FUNCTIONġ. METHOD OF REDUCING THE LOAD OF ONE OR MORE ENGINES IN A LARGE HYDRAULIC EXCAVATORīurner assembly for particulate trap regenerationĮstimating Pre-Turbine Exhaust TemperaturesĮxhaust gas purification device of internal combustion engineĭEVICE AND METHOD FOR REGENERATING A PARTICULATE FILTER ARRANGED IN THE EXHAUST SECTION OF AN INTERNAL COMBUSTION ENGINE ![]() Submerged condenser for steam power plant FUEL INJECTOR FOR HIGH ALTITUDE STARTING AND OPERATION OF A GAS TURBINE ENGINE
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