[go: up one dir, main page]

US1372043A - Apparatus for directing searchlights by the sound of aerial objectives - Google Patents

Apparatus for directing searchlights by the sound of aerial objectives Download PDF

Info

Publication number
US1372043A
US1372043A US306477A US30647719A US1372043A US 1372043 A US1372043 A US 1372043A US 306477 A US306477 A US 306477A US 30647719 A US30647719 A US 30647719A US 1372043 A US1372043 A US 1372043A
Authority
US
United States
Prior art keywords
sound
searchlight
post
training
searchlights
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
Application number
US306477A
Inventor
Routin Joseph Louis
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.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US306477A priority Critical patent/US1372043A/en
Application granted granted Critical
Publication of US1372043A publication Critical patent/US1372043A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21VFUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V14/00Controlling the distribution of the light emitted by adjustment of elements
    • F21V14/04Controlling the distribution of the light emitted by adjustment of elements by movement of reflectors

Definitions

  • This invention comprises, in combination, the following appliances:
  • a sound-detector enabling the direction of the object sought to be approximately ascertained.
  • a projector or Searchlight which, during the period of search, is directed by special means to be described hereafter, according to the direction given by the sound detector.
  • a control post located about 50 meters from the Searchlight, with means for keepin the latter directed upon the object.
  • the sound detector which may be of any suitable known type, or may consist of a pair of acousticreceivers arranged to receive the sound-waves emanating from an aircraft engine, and to indicate the direction thereof, is mounted for horizontal adjustment or training, on a vertical axle, vertical angular adjustment or tipping being effected by rotation upon a second axle which is perpendicular to. the former and takes part in the movement imparted for horizontal movement or training.
  • Figs. 2 and 3 a sound-detector for use in my invention in which D designates a sound-detector comprising, for example, a parabolic disk. of three meters diameter, provided with axles 22.
  • a crank 23 permits manipulation of the disk for point ing in elevation, that is to say, incliningit more or less to the vertical.
  • Axles 22 are carried by a forked support 24, the vertical portion 25 of which is supported in a base Specification of Letters Patent.
  • a second operator receives in one ear the noises received by horns 28 and 30 and in the other ear the noises received by horns 29 and 31.
  • the two operators regulate the position of' the apparatus by manipulating cranks 23 and 26" in such a manner that, by giving small displacements of 1 to 2 in one direction or the other, the noise which reaches them passes from one ear to the other and until this alternation ceases to be produced.
  • the adjustment of the sound-detector at any given instant does not correspond with the actual position of the object, but with the position which the object occupied when the sound received was emitted. It is, therefore, obvious that the searchlight must be pointed in a direction given by the horizontal angle of the sound-detector plus the angle through which/the object has traveled while the sound has been traveling to the receiver.
  • the necessary correction can be made with sufiicient accuracy by hand, by turning the rheostat 1 on the pivot 2, the distance being judged, for example, by the loudness of the noise made by the aircraft, and tables may be prepared 'for directly reading the angle of correction required'by the rheostat, this angle being a function of the. assumed speed of the air craft.
  • the direction thus given will generally be within the beam of the Searchlight 100
  • E designates a listen- 105 ing post
  • P designates a distant Searchlight post
  • C a control post about 50 meters from the Searchlight.
  • At posts E and P are rheostats 1 and 3 connected by electric conductors L L".
  • Rheostat 1 is providedwith a pair of brushes 5, 7 revolubly mounted on a. pivot 2, and rheostat 3 is likewise '4 and 5 wherein provided with a pair of similar brushes .8 are connected with each other through a companion coil 21 of the same voltmeter 9.
  • a battery 15 is bridged across the conductors L, L".
  • the position of the brushes 5 and 7 at l1s tening station E is determined by the position in azimuth of the sound-detector D, as here illustrated.
  • pivot 2 is provided with a gear 25" en aging a worm 26 on a drive shaft 26'.
  • second worm 26 on this shaft engages a pinion 25* on the vertical spindle 25 carrying the sound detector D.
  • the crank 26 By turning the crank 26", the detector D is rotated in a horizontal plane and a corresponding movement is imparted to brushes 5 and 7 of the rheostat 1, thereby causing a corresponding deflection of the needle of voltmeter 9 at the control station C.
  • the searchlight F is trained in accordance with the movements of the sound-indicator.
  • a motor N at the control post C is pro-- vided, whose field-coil and armature are connected to feed-wires S.
  • the commutator A of motor N is provided with a pair of supplementary brushes B, B which are electrically connected to the armature of a motor M and are adjustable by hand by means of the control-lever L. It will be clear that, when the brushes B, B are perpendicular to the axis of the neutral zone, the motor M will be at rest, and that its direction and speed can be controlled at will by moving the lever L one way or the other.
  • the shaft of motor M is adapted to rotate the brushes 8 and 6. on their pivot 4 and also to train the searchlight F through gear connections 32, 33, 34 and 35.
  • the operator at control station C operates the brush handle L in such direction and extent as to position contacts 6, 8 on the rheostat where they will give a zero reading to the voltmeter 9. At this position, the searchlight F will be given a training corresponding to that given the sound-detector D.
  • Figs. designates a table carryng volt-meters V, V one of which, V for example, corresponds with voltmeter 9 of Fig. 1 showing my system for training the searchlight in azimuth.
  • -V is the voltmeter which would control in an identical system not shown the searchlight in zenithal directionf Crank K corresponds to brush operating handle L Fig.
  • cranks K and J are independent of each other and belong to two identical systems one of which controls the searchlight in azimuth and the other in zenithal direction.
  • the tipping of the searchlight is accordingly like the training thereof, an intuitive action that is, for example, when the table is turned right-handed the luminous beam of the searchlight also turns to the right. This is a feature of great importance, and is indispensable for the purpose in view, especially when the pilot finds that he is detected and seeks to evade the searchlight.
  • the tipping of the searchlight is effected in a wholly similar manner, by means of a combination of mechanism including an electric transmitter at the listening post, a receiver at the searchlight post, and a voltmeter and control lever at' the control post; the brushes moved by this second lever may be mounted, on the commutator of the motor N or on the commutator of a second motor fed in the same manner as the motor N.
  • the two control levers must be mounted -so that they move, respectively, in a horizontal and in a vertical plane.
  • the two voltmeters, as well as the motors controlling the horizontal and vertical movements, with the respective levers, are mounted on a bed or platform turning on a vertical axle so that it can be turned by or with the operator or operators, to follow the training movement.
  • a simple device consists in providing the'operator with a belt attached to a lever or arm connected to said platform,
  • a frequent occurrence in connectlon with the training and tipping mechanism of searchlights is that the training movement reacts upon the tipping mechanism, that is to say, when the handle for training the light is actuated without actuating the tipping handle, the vertical angle is nevertheless slightly altered.
  • This error may be corrected by connecting the repeater rheostat of the tipping mechanism on the search-light apparatus to the training mechanism, by means of suitable gearing.
  • a listening post provided with sound-detecting and locating means, a distant post having a Searchlight, a control post having indicating means controlled by said sound-detecting means, -.and manually-controlled means for training said Searchlight in accordance with the indications of said indicating means.
  • a listening post provided with sound-detecting and locating means, a distant post having a searchlight, two rheostats provided with a common source of current and each provided with a pair of movable contacts, one pair having operating connections with said sound-detector, a control post having a voltmeter controlled in the contacts of both rheostats, a source of variable potential thereat, and

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)

Description

J. L. nounm. APPARATUS FOR DIRECTINGA SEARCHLIGHTS BY THE soumo 0F AERIAL OBJECTIVES.
APPLICATLON FILED JUNE 24, I919. 1,372,043., Patented Mar-22,1921.
2 SHEETS-SHEET I.
A I M IAI I I J. L. ROUTIN. APPARATUS FOR DIRECTING SEARCHLIGHTS BY THE SOUND OF AERIAL OBJECTIVES.
APPLICATION FILED JUNE 24, 1919.
Patented Mar. 22, 1921.
2 SHEET$-SHEET 2- Eq 2.
TES
PATENT OFFICE.
JOSEPH LOUIS ROUTIN, OF PARIS, FRANCE.
APPARATUS FOR DIREGTING SEARGHLIGHTS BY THE SOUND OF AERIAL OBJECTIVES.
Application filed June 24,
To all whom it may concern:
Be it known that I, J osnrn LouIs RoUTIN, a citizen of the Republic of France, a resident of Paris, in the Republic of France, have invented a new and useful Apparatus for Directing Searchlights by the Sound of Aerial Objectives, which invention is fully set forth in the following specification.
This invention comprises, in combination, the following appliances:
1. A sound-detector enabling the direction of the object sought to be approximately ascertained.
2. A projector or Searchlight which, during the period of search, is directed by special means to be described hereafter, according to the direction given by the sound detector.
3. A control post, located about 50 meters from the Searchlight, with means for keepin the latter directed upon the object.
11 order that the invention may be more readily understood, reference is had to the accompanaying drawings, in which Figure 1 is a diagrammatic view showing one constructional form of my invention;
The sound detector, which may be of any suitable known type, or may consist of a pair of acousticreceivers arranged to receive the sound-waves emanating from an aircraft engine, and to indicate the direction thereof, is mounted for horizontal adjustment or training, on a vertical axle, vertical angular adjustment or tipping being effected by rotation upon a second axle which is perpendicular to. the former and takes part in the movement imparted for horizontal movement or training. j
In Figs. 2 and 3 is shown a sound-detector for use in my invention in which D designates a sound-detector comprising, for example, a parabolic disk. of three meters diameter, provided with axles 22. A crank 23 permits manipulation of the disk for point ing in elevation, that is to say, incliningit more or less to the vertical. Axles 22 are carried by a forked support 24, the vertical portion 25 of which is supported in a base Specification of Letters Patent.
Patented Mar. 22, 1921. 1919. Serial No. 306,477.
27 and is adapted to receive a movement of rotation by aid of. a manually-operated spindle 26 through gearing 26. Near the focus ofthe parabolic disk are disposed receiving horns 28, 29, 30, 31, indicated diagrammatically. These horns are coupled together as follows For pointing in direction, the operator re-' ceives in his right ear, by aid of a rubber tube terminated in a fork, the noises received by horns '28 and 29, and in his left ear the noises received b horns 30 and 31.
For pointing 1n elevation, a second operator receives in one ear the noises received by horns 28 and 30 and in the other ear the noises received by horns 29 and 31.
The two operators regulate the position of' the apparatus by manipulating cranks 23 and 26" in such a manner that, by giving small displacements of 1 to 2 in one direction or the other, the noise which reaches them passes from one ear to the other and until this alternation ceases to be produced. The adjustment of the sound-detector at any given instant does not correspond with the actual position of the object, but with the position which the object occupied when the sound received was emitted. It is, therefore, obvious that the searchlight must be pointed in a direction given by the horizontal angle of the sound-detector plus the angle through which/the object has traveled while the sound has been traveling to the receiver. In practice, the necessary correction can be made with sufiicient accuracy by hand, by turning the rheostat 1 on the pivot 2, the distance being judged, for example, by the loudness of the noise made by the aircraft, and tables may be prepared 'for directly reading the angle of correction required'by the rheostat, this angle being a function of the. assumed speed of the air craft. The direction thus given will generally be within the beam of the Searchlight 100 Referring to Fig. 1, E designates a listen- 105 ing post, P designates a distant Searchlight post, and C a control post about 50 meters from the Searchlight. At posts E and P are rheostats 1 and 3 connected by electric conductors L L". Rheostat 1 is providedwith a pair of brushes 5, 7 revolubly mounted on a. pivot 2, and rheostat 3 is likewise '4 and 5 wherein provided with a pair of similar brushes .8 are connected with each other through a companion coil 21 of the same voltmeter 9. A battery 15 is bridged across the conductors L, L". I
The position of the brushes 5 and 7 at l1s tening station E is determined by the position in azimuth of the sound-detector D, as here illustrated. To secure this result, pivot 2 is provided with a gear 25" en aging a worm 26 on a drive shaft 26'. second worm 26 on this shaft engages a pinion 25* on the vertical spindle 25 carrying the sound detector D. By turning the crank 26", the detector D is rotated in a horizontal plane and a corresponding movement is imparted to brushes 5 and 7 of the rheostat 1, thereby causing a corresponding deflection of the needle of voltmeter 9 at the control station C.
At the searchlight post P, the searchlight F is trained in accordance with the movements of the sound-indicator. For this purpose, a motor N at the control post C is pro-- vided, whose field-coil and armature are connected to feed-wires S. The commutator A of motor N is provided with a pair of supplementary brushes B, B which are electrically connected to the armature of a motor M and are adjustable by hand by means of the control-lever L. It will be clear that, when the brushes B, B are perpendicular to the axis of the neutral zone, the motor M will be at rest, and that its direction and speed can be controlled at will by moving the lever L one way or the other. To keep the brushes B'.'8.I1d B and the commutator A in good condition, it is desirable to use very narrow and resistant carbon brushes, and to have commutator segments in such number that the potential difference between two consecutive segments be less than one volt. The shaft of motor M is adapted to rotate the brushes 8 and 6. on their pivot 4 and also to train the searchlight F through gear connections 32, 33, 34 and 35. The operator at control station C operates the brush handle L in such direction and extent as to position contacts 6, 8 on the rheostat where they will give a zero reading to the voltmeter 9. At this position, the searchlight F will be given a training corresponding to that given the sound-detector D.
At the control post the operator or operators in charge of the searchlight, and the levers which they have to control are lo-' cated on a turntable, so as to take part in the training movement of the searchli ht, so that the target is kept in front. he mounting of this a ,;rppai:atu-s is shown in Figs. designates a table carryng volt-meters V, V one of which, V for example, corresponds with voltmeter 9 of Fig. 1 showing my system for training the searchlight in azimuth. -V is the voltmeter which would control in an identical system not shown the searchlight in zenithal directionf Crank K corresponds to brush operating handle L Fig. 1 for controlling the potential applied to motor M for training the searchlight in azimuth and crank J controls identical brushes not shown for applying potential to a motor for training the searchlight in zenithal direction. It is to be understood that cranks K and J are independent of each other and belong to two identical systems one of which controls the searchlight in azimuth and the other in zenithal direction.
The tipping of the searchlight, is accordingly like the training thereof, an intuitive action that is, for example, when the table is turned right-handed the luminous beam of the searchlight also turns to the right. This is a feature of great importance, and is indispensable for the purpose in view, especially when the pilot finds that he is detected and seeks to evade the searchlight.
Instead of this motor control device any other equivalent motor control device may be used, for exam le one according to the well known Ward lleonard system.
The tipping of the searchlight is effected in a wholly similar manner, by means of a combination of mechanism including an electric transmitter at the listening post, a receiver at the searchlight post, and a voltmeter and control lever at' the control post; the brushes moved by this second lever may be mounted, on the commutator of the motor N or on the commutator of a second motor fed in the same manner as the motor N. The two control levers must be mounted -so that they move, respectively, in a horizontal and in a vertical plane.
One of the essential and characteristic features of the invention is that the two voltmeters, as well as the motors controlling the horizontal and vertical movements, with the respective levers, are mounted on a bed or platform turning on a vertical axle so that it can be turned by or with the operator or operators, to follow the training movement. I
' If a single operator located near the rotatable frame or platform is charged with (bothv directing movements horizontal and vertical), a simple device consists in providing the'operator with a belt attached to a lever or arm connected to said platform,
If there are two operators, one for the lever L and the other for the tipping lever, they may have seats fixed side by side upon the turning platform, and a third 0 orator may rotate the platform by following the beam. It may be noted that when the operators can see the object with the naked eye it is not essential that the direction given to the platform should correspond exactly with that of the beam, a deflection of 10 or 20 degrees being of no consequence.
A frequent occurrence in connectlon with the training and tipping mechanism of searchlights is that the training movement reacts upon the tipping mechanism, that is to say, when the handle for training the light is actuated without actuating the tipping handle, the vertical angle is nevertheless slightly altered.
This error may be corrected by connecting the repeater rheostat of the tipping mechanism on the search-light apparatus to the training mechanism, by means of suitable gearing.
What I claim is:
1'. In combination, a listening post provided with sound-detecting and locating means, a distant post having a Searchlight, a control post having indicating means controlled by said sound-detecting means, -.and manually-controlled means for training said Searchlight in accordance with the indications of said indicating means.
2. In combination, a listening post provided with sound-detecting and locating means, a distant post having a searchlight, two rheostats provided with a common source of current and each provided with a pair of movable contacts, one pair having operating connections with said sound-detector, a control post having a voltmeter controlled in the contacts of both rheostats, a source of variable potential thereat, and
motor means at the Searchlight post having I operating connections with said second set of contacts and with said Searchlight for operating the latter and controlledby said source 0 variable potential as indicated by said voltmeter.
In testimony whereof I have signed this specification.
JOSEPH LOUIS ROUTIN. Signed in the presence of PETER PETERSEN,
LoUIs GARDET.
US306477A 1919-06-24 1919-06-24 Apparatus for directing searchlights by the sound of aerial objectives Expired - Lifetime US1372043A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US306477A US1372043A (en) 1919-06-24 1919-06-24 Apparatus for directing searchlights by the sound of aerial objectives

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US306477A US1372043A (en) 1919-06-24 1919-06-24 Apparatus for directing searchlights by the sound of aerial objectives

Publications (1)

Publication Number Publication Date
US1372043A true US1372043A (en) 1921-03-22

Family

ID=23185477

Family Applications (1)

Application Number Title Priority Date Filing Date
US306477A Expired - Lifetime US1372043A (en) 1919-06-24 1919-06-24 Apparatus for directing searchlights by the sound of aerial objectives

Country Status (1)

Country Link
US (1) US1372043A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2415094A (en) * 1938-01-17 1947-02-04 Board Radio measurement of distances and velocities
US2454841A (en) * 1938-07-16 1948-11-30 Sackville William Apparatus for detecting the presence and position of an invisible body by infrared radiation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2415094A (en) * 1938-01-17 1947-02-04 Board Radio measurement of distances and velocities
US2454841A (en) * 1938-07-16 1948-11-30 Sackville William Apparatus for detecting the presence and position of an invisible body by infrared radiation

Similar Documents

Publication Publication Date Title
US2231929A (en) Tridimensional radio direction indicator
US2851643A (en) Apparatus for transmitting the movement of a point to a distance
US2416562A (en) Follow-up system
US2554119A (en) Stabilized radar scanner equipment mounted on vehicles of all kinds
US1957240A (en) Control system
US1372043A (en) Apparatus for directing searchlights by the sound of aerial objectives
US2911167A (en) Heat seeker
US2529468A (en) Radio range navigation apparatus for training aircraft personnel
US3016791A (en) Target indicating systems
US2003661A (en) Searchlight director
US2438126A (en) Mechanical signal and volume control for miniature radio ranges
US2377589A (en) Automatic aiming control
US1238503A (en) Automatic gun-pointing.
GB1160643A (en) Variable Lead Device for Line Tracers
US1077965A (en) Naval fire-control apparatus.
US2342938A (en) Antiaircraft fire control system
US2452038A (en) Photoelectric radio compass trainer control
US2413114A (en) Gun turret
US1850598A (en) Searchlight control
US2485301A (en) Wind drift instrument
US1356285A (en) Luminous indicating device for the night landing of aeroplanes
US1626824A (en) System of and apparatus for gun-fire control
US2472098A (en) Navigational map projection device
US2204553A (en) Automatic steering of ships
US2872272A (en) Automatic relative position plotter