GB441370A - - Google Patents

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Publication number
GB441370A
GB441370A GB441370DA GB441370A GB 441370 A GB441370 A GB 441370A GB 441370D A GB441370D A GB 441370DA GB 441370 A GB441370 A GB 441370A
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United Kingdom
Prior art keywords
rectifiers
reversed
impulses
june
condenser
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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.)
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Publication of GB441370A publication Critical patent/GB441370A/en
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Abstract

441,370. Directive wireless signalling. TELEFUNKEN GES. FUR DRAHTLOSE TELEGRAPHIE, 12, Hallesches Ufer, Berlin. June 4, 1935, No. 16239. Convention date, June 4, 1934. [Class 40 (v)] In a cross-coil visual indicator for use when steering on an overlapping-beam system, the mean direct-current component of the co-operating signals, Figs. 2 and 3, is filtered out so that the final form of the impulses applied to the indicator is as shown in the bottom-line of those Figures. In this form the impulses are applied to the crossed coils S1, S2, Fig. 1, through reversed rectifiers G1, G2. The object is to prevent the growing strength of the impulses, as the aeroplane approaches the transmitting beacon, from affecting the accuracy of the readings. The system is applicable to modulated signals or to unmodulated signals received by a local heterodyne. The output from the last valve Nf, Fig. 1, of the receiver is rectified at GO and applied across a resistance R1 and condenser C1 to produce the voltageform UR1, Figs. 2 and 3. The direct-current component is then filtered out by a condenser C2, and applied across a resistance R2 to give the voltage-form UR2, which is applied to the crossed coils S1, S2 through reversed rectifiers G1, G2. To produce a dead-beat swing of the pointer P, each coil is shunted by reversed rectifiers G3, G4 and variable resistances r3, r4 ; also the gap of the magnet M is of elliptical cross-section.
GB441370D Active GB441370A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431317A (en) * 1942-07-28 1947-11-25 Int Standard Electric Corp Indicating system for radio blind landing systems
US2603779A (en) * 1945-12-27 1952-07-15 Sperry Corp Radio guidance system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2431317A (en) * 1942-07-28 1947-11-25 Int Standard Electric Corp Indicating system for radio blind landing systems
US2603779A (en) * 1945-12-27 1952-07-15 Sperry Corp Radio guidance system

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