Abstract [Object] To provide a method of manufacturing a helical antenna for satellite communications which has no local bent, etc. in the completed helical coil even though the conductor wire used is of an extremely pliable material, so that a high-quality helical antenna for use in satellite communications is obtained. [Structure] A winding frame 10 in which supporting elements 12 are projected in the form of a cross from the outer circumferential surface of a rod-form base 11 is first obtained. Wedge members 71 through 74, each of which having a configuration of a cylindrical body divided into four sections along its axis, are installed between the supporting elements 12. Then, with the cylindrical surfaces of the wedge members 71 through 74 being used as a winding guide, a conductor wire is wound in helical form through conductor wire installation grooves 13 formed on the edges of the supporting elements 12. Thus, a helical coil 20 is formed. Afterward, the wedge members are removed from the winding frame 10; as a result, an antenna element of a helical antenna suitable for satellite communication is obtained.
A method of manufacturing a helical antenna for satellite communication comprising: obtaining a winding frame, said winding frame being obtained via four supporting elements projecting in a cross shape from an outer circumferential surface of a cylindrical base, each one of said four supporting elements being of a rectangular plate shape and being provided with conductor wire grooves at a prescribed pitch formed on an outer edge of said supporting element; installing wedge members between adjacent supporting elements of said winding frame coaxial with said cylindrical base, each one of said wedge members having a configuration formed by dividing a cylindrical body having an axial taper into four sections along two planes which include a center axis of said cylindrical base and intersect each other perpendicularly; winding a conductor wire in a helical configuration through said conductor wire grooves of said four supporting elements which are located between said wedge members cylindrical surfaces of said wedge members being used as a winding guide; and removing said wedge members from locations between said helical coil and said winding frame after said helical coil has been formed by withdrawing said wedge members in a direction opposite to said axial taper.
Claim 2
Independent Claim
198 words
A method of manufacturing a helical antenna for satellite communication comprising: obtaining a winding frame, said winding frame being obtained via four supporting elements projecting in a cross shape from an outer circumferential surface of a cylindrical base, each one of said four supporting elements being of a rectangular plate shape and being provided with conductor wire grooves at a prescribed pitch formed on an outer edge of said supporting element; installing wedge members between adjacent supporting elements of said winding frame coaxial with said cylindrical base, each one of said wedge members having a configuration formed by dividing a cylindrical body having an axial taper into four sections along two planes which include a center axis of said cylindrical base and intersect each other perpendicularly; winding a conductor wire in a helical configuration through said conductor wire grooves of said four supporting elements which are located between said wedge members cylindrical surfaces of said wedge members being used as a winding guide; and removing said wedge members from locations between said helical coil and said winding frame after said helical coil has been formed by withdrawing said wedge members in a direction opposite to said axial taper.