초록 ▼

A propeller shroud or nozzle, made with airfoil section of high lift to drag ratio, increases thrust, speed and efficiency of a fixed or controllable pitch propeller operating inside the shroud. Shroud section is designed with continuously curved inside and outside surface to create maximum lift and

A propeller shroud or nozzle, made with airfoil section of high lift to drag ratio, increases thrust, speed and efficiency of a fixed or controllable pitch propeller operating inside the shroud. Shroud section is designed with continuously curved inside and outside surface to create maximum lift and minimum drag. For the larger propellers used on ships, and for lower cost of construction, shroud is fabricated using plates of steel and stainless steel or other suitable material, built as a number of straight airfoil segments forming a polygon approximating circular ring. Low shroud drag makes possible improving thrust and speed of vessels, even when operating at high speed, compared to optimally designed propeller without the shroud.

대표청구항 ▼

In a marine propulsion apparatus including a shaft having a propeller thereon and a shroud surrounding said propeller, the improvement comprising: said shroud including a plurality of adjacent segments abutting one another, each said segment comprising an outside surface and an inside surface each h

In a marine propulsion apparatus including a shaft having a propeller thereon and a shroud surrounding said propeller, the improvement comprising: said shroud including a plurality of adjacent segments abutting one another, each said segment comprising an outside surface and an inside surface each having a leading and trailing edge. said outside and inside surfaces substantially laterally flat, said inside and outside surface leading and trailing edges respectively connected together to provide an airfoil section with said inside and outside surfaces continuously curved from said connected leading and trailing edges, said inside and outside surfaces spaced apart between said leading and trailing edges to define a cavity therebetween, each said segment airfoil section having a camber in the range of 0 to 0.025 of the the chord length thereof, said outside surface including a concave area thereon, said section thickness ranging from 0.05 to 0.24 of the chord length and having a maximum thickness located 0.25 to 0.35 of the chord length from said leading edges, each said segment airfoil section having a maximum camber located from 0.25 to 0.35 of the chord length from said connected leading edges, said segment airfoil section having a chord length between 0.3 and 0.6 of the diameter of the propeller surrounded by said shroud, said segment airfoil sections disposed such that the angle between the chord thereof and the propeller shaft ranges between -6 to +6 degrees, at least one ring frame member disposed transversely within said cavities of said segments, said ring frame member connected respectively to said segment inside and outside surfaces and laterally connecting together said plurality of segments to provide said shroud, and a longitudinal frame member connected to each said connected inside and outside surfaces and said ring frame member of each said segment.