US2241915A - Direction-finding system - Google Patents

Direction-finding system Download PDF

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Publication number
US2241915A
US2241915A US226473A US22647338A US2241915A US 2241915 A US2241915 A US 2241915A US 226473 A US226473 A US 226473A US 22647338 A US22647338 A US 22647338A US 2241915 A US2241915 A US 2241915A
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United States
Prior art keywords
coil
instrument
pointer
signals
impulses
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Expired - Lifetime
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US226473A
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English (en)
Inventor
Kramar Ernst
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Alcatel Lucent Deutschland AG
C Lorenz AG
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Standard Elektrik Lorenz AG
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Publication date
Application filed by Standard Elektrik Lorenz AG filed Critical Standard Elektrik Lorenz AG
Priority to US359950A priority Critical patent/US2290974A/en
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Publication of US2241915A publication Critical patent/US2241915A/en
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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S1/00—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith
    • G01S1/02—Beacons or beacon systems transmitting signals having a characteristic or characteristics capable of being detected by non-directional receivers and defining directions, positions, or position lines fixed relatively to the beacon transmitters; Receivers co-operating therewith using radio waves

Definitions

  • radio beacon method In both cases two directional charac- .teristics are alternately produced which overlap each other, the desired course line agreeing with the line defined by the points of intersection of the two alternately generated directional characteristics or diagrams.
  • the method operating with the aid of di ectional transmitters is in general designated as radio beacon method, while the method operating with directional receivers is designated as destination steering method.
  • radio beacon method either directional antennae are used, these being alternately connected and disconnected, or a continuously fed energizing antenna and alternately keyed refiector antennae are employed, whereas in the destination steering method a combination of frame antennae and open antennae is used, either the frame antenna effect or the effect of the open antennae being periodically inversed.
  • the invention described hereafter relates to a method of indicating course line obtained by comparing the amplitudes.
  • the known methods of this employ either acoustic indication or visual indication.
  • the acoustic indication as long as the course line is followed thepilot hears a continuous tone in his headphones, whereas whenever he happens to be off the course line the signal of one or the other kind will preponderate.
  • the directional high frequency fields are not keyed in the rhythm of complementary signals, this mode being adopted for the acoustic indication, but are modulated with tone frequencies to which selective members connected with the receiving apparatus are tuned, such members being oscillating reeds, for example.
  • This method has the fundamental disadvantage that acoustic and visual indication cannot be effected both at the With the visual indicasame time. This, however, is necessary if the method is to be employed on board aircraft, since the pilot when observing his navigation instruments must make use of the acoustic indication while during a wireless intercommunication he is to depend upon the visual indication.
  • This instrument is influenced by induction pulses produced in a transformer by the signal flanks. that is, the peak voltages produced at the beginning and end of a D. C. impulse impressed on the transformer primary,
  • Such known method requires the keying to be in the rhythm of signals of the kind composed of elemental signals which are of the same length. This is only so if the keying is in the dot-dash rhythm, that is, if on one side only dots and on the other side only dashes are produced.
  • the dot-dash keying however has a disadvantage which is due to the nature of the human ear, because the summated signal of each side, that is, the integral value of the elemental signals thereof is different from that of theother side, whereby it is rendered difficult to compare the sound intensities with each other.
  • the letters A and N, or U and D or the like are signals of this kind. These signals when summated equal one another in a manner to allow of readily comparing them by hearing. They are however composed of dots and dashes, that is, are composed of elements which are different in length and thus render it impossible to make use of the indicating instru ment employed in connection with the dot-dash keying, namely an instrument which is very sensitive in its zero position while being little sensitive in the outer positions of its pointer.
  • the invention discloses a novel indicating method that enables acoustic and visual indication to be effected both at the same time even in the case of keying signals composed of differently long elemental signals.
  • the acoustic indication is facilitated, as the elemental signals may be so chosen that the integral Values of the two signals shall equal one another.
  • the induction pulses produced in a transformer by the signal flanks and employed in known manner for the dot-dash keying, are used in connection with keying methods of the kind employing signals composed of differently long elemental signals.
  • This novel application of such induction pulses should not be considered a mere mechanical skill since the induction pulses are different in direction and also are different in frequency.
  • By the invention methods are disclosed which shall enable such induction pulses to be utilized for effecting a visual indication.
  • Fig. 1 is a graphical representation that relates to the said induction pulses.
  • Fig. 2 is a wiring diagram showing one embodiment of the invention
  • Fig. 3 is a schematic view illustrating a form of the indicating instrument of an arrangement adapted for effecting the novel method.
  • Fig. 4 is a wiring diagram of such arrangement.
  • Fig. 5 is a schematic view representing another form of indicating instrument,
  • Fig. 6 shows the appertaim ing circuit arrangement.
  • Fig. '7 is a diagrammatic view of still another embodiment of the invention.
  • Fig. 1 On the left in Fig. 1 the particulars relating to the letter A are represented while on the right hand side thereof the inverse particulars, relating to letter N, are plotted.
  • the received and rectified signals, Fig. 1, a are conveyed to a transformer in which the signal flanks act to produce induction pulses, Fig. 1, b.
  • T If the keying period is designated T then two induction pulses originate which are different in direction.
  • the positively directed impulses are of the period T/ while the negatively directed impulses are of the period T/2.
  • the conditions are the reverse of the former. Therefore, the negatively directed impulses of the letter A have a frequency 21 and the positively directed impulses a frequency 4 where 1 denotesthe keying frequency.
  • the positively directed impulses of letter N have the frequency 2 while the negatively directed impulses thereof are of the frequency M.
  • the indicating method as provided by the invention is based on these relationships. Effecting the invention consists in rectifying the impulses and then delivering them to oscillatory circuits, the voltages or currents originated in these circuits being rendered effective by a differential indicating instrument.
  • the mode of action here is as follows:
  • the keying signals arriving in the receiver E are amplified and rectified and then conveyed to a transformer T which acts to transfer the signal flanks as induction pulses.
  • Such impulses are rectified in rectifiers GI, G2 and are then delivered to oscillatory circuits CI, LI and C2, L2 which are tuned to the frequency 2].
  • circuits CI, LI will be in resonance with the frequency of the received induction pulses whereas when letter N is received the rectification causes circuit C2, L2 to be resonant.
  • the resonant voltage of these circuits is in its turn rectified and conveyed to a differential indicating instrument which may be a standard moving coil instrument J having a potentiometer 'r allotted to it. According to which resonance voltage is higher the pointer of the instrument will be de- The method preferably adopted for flected either to the right or the left. Such instrument may of course be so connected as to utilize the current instead of utilizing the resonance voltage. Since the pointer deflection thereof is of special invariable values a proper calibration will enable the angle of deviation from the course line to be immediately ascertained by reading.
  • the other indicating methods here concerned are likewise based on the principle of induction pulses rendered effective in instruments of special kind.
  • the instrument represented in Fig, 3 has two magnet systems M I M2 provided with pointed pole pieces I, II, III, IV. Between these pole pieces a cross coil is arranged to move. As shown in Fig. 4, the coils RI, R2 thereof are connected in series with the receiving apparatus E over pulsing transformer T.
  • the mode of action of this instrument is explained with reference to the graphic representation shown in Fig. 1, c which is a graph of the pointer deflection. Let it be supposed that in the case of letter A a positive impulse arrives.
  • coils RI, R2 are in the maximum field of the pole pieces and are connected in series there results a maximum deflection with double the intensity of the arriving impulse, for instance a deflection to the right.
  • Coil RI therefore rotates to leave the two magnet fields while coil R2 moves out of the field of magnet MI to enter the oppositely directed field of magnet M2.
  • the pointer instrument slightly moves back, as will be seen from Fig. 1, c.
  • the next following negative impulse however rapidly moves the pointer back to the right, since only coil R2, now located in the oppositely directed field of magnet M2, is effective.
  • the coil is now likewise in a field of the two magnets which is of very low intensity so that the ensuing positive impulse entails only a small backward movement of the pointer.
  • the indicating device shown in Fig. 5 likewise comprises a cross coil instrument, with the difference however that the two systems are not located in one plane but are located one above the other, that is to say, system I, II and coil R1 are arranged in one plane whereas system III, IV and coil R2 are arranged in a second plane located either above or below the former.
  • the induction pulses are here rectified by the rectifiers GI, G2 and each impulse direction is only rendered effective either in coil RI or in the coil R2.
  • the curve of pointer deflection for this system is shown in Fig. 1d. Let use again suppose that the signal A is received in preponderance of signal N. Let the first positive impulse be supposed to become effective in coil R2, for instance.
  • the pole pieces III, IV are so shaped that with increasing deflection the coil R2, moving to the right, enters a field of increasing intensity.
  • the moving coil system is therefore rapidly moved to the right by such.
  • first positive impulse coil R2 entering a strong field while coil RI is moved out of the field of the pole pieces I, II belonging to it.
  • the negative impulse which now arrives and which in consequence of the rectification becomes effective in coil RI only, merely causes a slight retrograde movement.
  • the instrument in this way slowly moves back through a smallangle, coil R2 thus remaining in a strong eld.
  • the ensuing positive impulse therefore acts to move the pointer rapidly to the right, the deflection thereof having to be multiplied by the field increase.
  • the coil R! is still outside the field so that the negative impulse which then occurs only causes a small retrogradation, the pointer then slowly returning into the position of rest.
  • letter N the conditions are again the reverse of the former so that the deflection will be in the opposite direction.
  • the indicating instrument shown in Fig. 7 acts to utilize, for determining the direction of the pointer deflection, the first incoming impulse only, while the ensuing impulses merely serve to hold the pointer after deflection.
  • the pointer is rapidly deflected to the right while the ensuing impulses do not vary such position of the pointer but act to maintain it in this position.
  • the pointer is by the first negative impulse rapidly moved to the other side and is held in such position by the ensuing impulses, the direction of these being not of importance here.
  • This instrument is a combination of a moving coil instrument and a soft iron instrument.
  • the direction is determined in accordance with the first incoming impulse, whereas the other impulses act on the soft iron portion, thus being independent of directions.
  • the moving coil instrument is such that the incoming impulse acts to move it out of the field of the appertaining magnet system so that the additional impulses shall not be able to influence this instrument.
  • I, II denote two magnet poles while R, indicates the moving or rotary coil.
  • the soft iron portion comprises solenoids SI, S2. All of the coils are connected in series and are joined to receiver E over the pulsing transformer T.
  • Coil R carries a soft iron armature A which is under the influence of the solenoids. Let us suppose that at first a positive impulse arrives. This impulse causes coil R to turn to the right, thus leaving the field of the magnet system I, II. The magnetic fields of the solenoids are indicated in dotted lines in order to explain the mode of action. The movement of coil R entails that the armature A enters the field of solenoid S2.
  • This field is influenced by the ensuing impulses and thus caused to attract the armature A.
  • the impulse direction is not of importance in this regard.
  • the indication methods here disclosed are not restricted to the A-N keying, but may be suited to any other mode of keying effective through signals composed of differently long elemental signals, the attenuation having to be calculated accordingly.
  • a direction finding receiver for visual indication by comparison of two signals to determine the preponderance thereof, each signal including signal elements of different lengths, comprising means for receiving and detecting said signals, means for producing from the detected signal elements induction impulses of opposite polarity indicating the beginning and the end of each signal element, whereby the signals are distinguished from one another by the polarity and grouping of the produced signal impulses, an instrument having four magnetic poles and two crossed coils, arranged in the field of said magnetic poles, means for applying said produced impulses to said coils to cause said coils to deflect relative to said poles, the deflection of said coils being dependent upon the predominance of one of said received signals.
  • a direction finding system further comprising rectifying means for said impulses to distinguish between said signals arranged to rectify said impulses before application to said coils, and means separately coupling said instrument coils to said rectifying means.

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  • Engineering & Computer Science (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Indicating Measured Values (AREA)
US226473A 1937-08-28 1938-08-24 Direction-finding system Expired - Lifetime US2241915A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US359950A US2290974A (en) 1938-08-24 1940-10-05 Direction finding system

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DE2241915X 1937-08-28

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Cited By (3)

* 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
US2558945A (en) * 1947-06-20 1951-07-03 Edison Inc Thomas A Electrical indicating system
US2677100A (en) * 1950-12-05 1954-04-27 Boeing Co Electric conductor continuity testing apparatus and method

Cited By (3)

* 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
US2558945A (en) * 1947-06-20 1951-07-03 Edison Inc Thomas A Electrical indicating system
US2677100A (en) * 1950-12-05 1954-04-27 Boeing Co Electric conductor continuity testing apparatus and method

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BE429919A (en)van)

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