US2270117A - Radio receiver - Google Patents
Radio receiver Download PDFInfo
- Publication number
- US2270117A US2270117A US259649A US25964939A US2270117A US 2270117 A US2270117 A US 2270117A US 259649 A US259649 A US 259649A US 25964939 A US25964939 A US 25964939A US 2270117 A US2270117 A US 2270117A
- Authority
- US
- United States
- Prior art keywords
- coil
- shaft
- core
- tuning
- radio receiver
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F21/00—Variable inductances or transformers of the signal type
- H01F21/02—Variable inductances or transformers of the signal type continuously variable, e.g. variometers
- H01F21/06—Variable inductances or transformers of the signal type continuously variable, e.g. variometers by movement of core or part of core relative to the windings as a whole
- H01F21/065—Measures for obtaining a desired relation between the position of the core and the inductance
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18568—Reciprocating or oscillating to or from alternating rotary
- Y10T74/18832—Reciprocating or oscillating to or from alternating rotary including flexible drive connector [e.g., belt, chain, strand, etc.]
- Y10T74/18848—Reciprocating or oscillating to or from alternating rotary including flexible drive connector [e.g., belt, chain, strand, etc.] with pulley
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18888—Reciprocating to or from oscillating
- Y10T74/1892—Lever and slide
- Y10T74/18968—Flexible connections
Description
Z J 9L 9 m =E. y 1 M L w. z
Jan. 13, 1942. J. v. FILL RADIO RECEIVER Filed March 3, 1959 Patented Jan. 13, 1942 mimo nncnrvan John v. Fill, Dobbs Ferry, N. Y., asslgnor to Ferro- Corporation of America, Hastings on Endson, N. Y., a corporation of Delaware Application March a, 1939, Serial im-zsasia 1 Claim. I (or. 111-442) This invention relates to radio receivers and particularly to permeability tuned high frequency circuits for radio receivers.
The usual tuning controls for manual orautomatic operation take the form of a rotatable shaft but the movable coil or core of a permeability tuned circuit travels in a straight line. The prior proposals for converting the rotary motion of the control shaft into a linear motion of the coil or core have not been entirely satisfactory.
An object of this invention is to provide a radio receiver having simple and inexpensive tuning units includingone or more permeability tuned circuits, a tuning shaft, and relatively stiff but resilient couplings between a crank arm on the shaft and the movable element of the tuned circuit or circuits. An object is to provide a permeability tuned circuit including a coil on a tubular form of insulating material, a magnetic core slidable in the form and having a stiff wire extending axially therefrom, a control shaft extending normal to and spaced from the axis of the core and coil, and an operating member on the shaft for connection to the outer end of the wire. These and other objects and advantages of the invention will be apparent from the following specification when taken with the accompanying drawing in which:
Fig. 1 is a rear elevation, with parts in section, ofva tuning assembly embodying the invention; and
Fig. 2 is a side elevation of the same.
- In the drawing, the reference numeral l identifies the supporting plate uponjwhich'two permeability tuned circuits and the tuning mechanism therefor are mounted. The lower end! nals thus serving as the junction points for connecting the coils into the receiver circuits.
Cores ll of finely divided magnetic material a and an insulating binder have a fairly snug but of the plate is .reversely bent and spaced from the'bodyof theplate to form a rear support for the manual control shaft 3. A second shaft 4 is journalled on the central portion of plate I and carries a large diameter drum or pulley 5 that is connected to the shaft l by the usual flexible cable 8. I
Each tuned circuit includes a coil 1 in the form of a relatively long winding on a small diameter tubular coil form of thin-walled insulating material. The-outer ends .of the coil forms are securely anchored to brackets 8 that extend rearwardly from the supporting plate, and their inner ends extend through and are accurately positioned by the extruded sleeves 10 of brackets H. Trimming condensers i2 are mounted on the plate'l .and have terminals to which the ends of the associated coils are connected, the termifree sliding fit within the bores of the coil forms 8. These coil'forms are preferably extruded or molded from synthetic resins to eliminate variation in size and to obtain a highly polished inner wall surface. Each core II has secured thereto, preferably by embedding therein, one end of relatively stiff but resilient coupling member It. These coupling members are preferably piano wire of about 0.022 inch diameter. This material is suihciently rigid, in an axial direction, to move the core into the coil forms when pressure is exerted on the outer ends of the wires, butcan flex laterally to some extent to permit some variation in the direction of an applied pull or push for adjustment of the core.
, The outer ends 15 of the wires H are bent to form open eyes that seat in the grooved sections of disks it on the ends of crank arms I! that ,are secured to the shaft 4.
g The dimensions of the open eyes II are preferably suchthat the .wires grip the disks l8 tightly to prevent backshaft 4, the crank arms l-I may be a single bar,
that is secured to the end of the shaft I.
, The parts are shown in solid line in Figs. 1 and 2 in the positions that they occupy when the cores ii are midway between their end positions.
The crank arms I! are normal to the axes of the associated coil forms and may move about 45 to either side into the illustrated dotted line positions. The angular motion of the adjusting shaft 4 is thus limited to but it is desirable to indicate the tuning adjustment by a pointer that moves through a larger angle. The shaft 4 therefore carries the larger element of a motionmultiplying gearing is, the smaller gear being .on the shaft II which carries a pointer 20. The
shaft I 9 is rotatably' supported by the plate I and a strap 2| that is secured to the supporting plate; The illustrated gearing has a 2 to 1 ratio and the pointer has oppositely directed arms for movement along scales 22 that each extend over an arc of 180. Other ratios may be used, if desired, to spread the scale up to about 330.
The coils 1 may be the antenna and a radio frequency circuit in a tuned radio frequency receiver, or the antenna and the oscillator tuning coil in the case of a superheterodyne receiver. The wire employed is preferably a multistrand cable, for example 10/42 single Celanese" enamel wire, the windings being of the progressive universal type. Good results have been obtained when the axial length of the coil approximates the length of the core. Cylindrical cores of diameter and 1 long have covered the range or 1700 to 540 kilocycles with a travel of 1 inches, the Q value for the coil being fiat at approximately 100 throughout the range.
Other means may be employed for securing the actuating wire to a core, or a plurality of cores, and for coupling the wire to the rotary control shaft. It is therefore to be understood that various changes may be made in the parts of the tuning unit, their design, shapes and relative locations without departing from the spirit of my invention as set forth in the following claim.
I claim:
In a radio receiver, a permeability tuned circuit comprising a tubular coil form, a coil on said form, a magnetic core slidable in said coil form, a length of piano wire having one end rigidly secured to said core, and tuning means,
for adjusting said core; said tuning means comprising a shaft carrying a crank arm, a member rotatably mounted on the outer end of the crank arm, the other end of said piano wire having the form of an open eye extending. about and resiliently held to said member.
JOHN V. FILL.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US259649A US2270117A (en) | 1939-03-03 | 1939-03-03 | Radio receiver |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US259649A US2270117A (en) | 1939-03-03 | 1939-03-03 | Radio receiver |
Publications (1)
Publication Number | Publication Date |
---|---|
US2270117A true US2270117A (en) | 1942-01-13 |
Family
ID=22985789
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US259649A Expired - Lifetime US2270117A (en) | 1939-03-03 | 1939-03-03 | Radio receiver |
Country Status (1)
Country | Link |
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US (1) | US2270117A (en) |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2483105A (en) * | 1945-10-03 | 1949-09-27 | Zenith Radio Corp | Combined inductance and capacity tuner |
US2488375A (en) * | 1945-03-28 | 1949-11-15 | Admiral Corp | Permeability tuning slug support |
US2505111A (en) * | 1946-03-20 | 1950-04-25 | Stanley A Hall | Tuning mechanism |
US2538787A (en) * | 1945-12-29 | 1951-01-23 | Specialties Dev Corp | Valve control means |
US2542579A (en) * | 1945-03-22 | 1951-02-20 | Admiral Corp | Connector |
US2543551A (en) * | 1948-06-10 | 1951-02-27 | Stackpole Carbon Co | Variable inductance core structure |
US2555248A (en) * | 1946-08-12 | 1951-05-29 | Aladdin Ind Inc | Midget inductance tuning mechanism |
US2563664A (en) * | 1946-10-23 | 1951-08-07 | Radio Condenser Co | Sequential tuner for radio sets |
US2580895A (en) * | 1949-02-24 | 1952-01-01 | Aladdin Ind Inc | Tuning system |
US2778232A (en) * | 1952-09-24 | 1957-01-22 | Time Inc | Precision carriage displacement device |
US3077788A (en) * | 1963-02-19 | Device for transmission of curvilinear | ||
US3086757A (en) * | 1960-01-05 | 1963-04-23 | Acf Ind Inc | Carburetor |
-
1939
- 1939-03-03 US US259649A patent/US2270117A/en not_active Expired - Lifetime
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3077788A (en) * | 1963-02-19 | Device for transmission of curvilinear | ||
US2542579A (en) * | 1945-03-22 | 1951-02-20 | Admiral Corp | Connector |
US2488375A (en) * | 1945-03-28 | 1949-11-15 | Admiral Corp | Permeability tuning slug support |
US2483105A (en) * | 1945-10-03 | 1949-09-27 | Zenith Radio Corp | Combined inductance and capacity tuner |
US2538787A (en) * | 1945-12-29 | 1951-01-23 | Specialties Dev Corp | Valve control means |
US2505111A (en) * | 1946-03-20 | 1950-04-25 | Stanley A Hall | Tuning mechanism |
US2555248A (en) * | 1946-08-12 | 1951-05-29 | Aladdin Ind Inc | Midget inductance tuning mechanism |
US2563664A (en) * | 1946-10-23 | 1951-08-07 | Radio Condenser Co | Sequential tuner for radio sets |
US2543551A (en) * | 1948-06-10 | 1951-02-27 | Stackpole Carbon Co | Variable inductance core structure |
US2580895A (en) * | 1949-02-24 | 1952-01-01 | Aladdin Ind Inc | Tuning system |
US2778232A (en) * | 1952-09-24 | 1957-01-22 | Time Inc | Precision carriage displacement device |
US3086757A (en) * | 1960-01-05 | 1963-04-23 | Acf Ind Inc | Carburetor |
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