US989134A - Electromagnetic compass. - Google Patents

Electromagnetic compass. Download PDF

Info

Publication number
US989134A
US989134A US36077007A US1907360770A US989134A US 989134 A US989134 A US 989134A US 36077007 A US36077007 A US 36077007A US 1907360770 A US1907360770 A US 1907360770A US 989134 A US989134 A US 989134A
Authority
US
United States
Prior art keywords
frame
ship
brushes
pairs
deviation
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
US36077007A
Inventor
Louis Dominique Joseph Armand Dunoyer
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 US36077007A priority Critical patent/US989134A/en
Application granted granted Critical
Publication of US989134A publication Critical patent/US989134A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C17/00Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
    • G01C17/02Magnetic compasses
    • G01C17/28Electromagnetic compasses
    • G01C17/30Earth-inductor compasses

Definitions

  • This apparatus will be particularly useful for obviating the disturbing effect upon the needle compass: 1. Of the masses of iron or steelsurrounding the deck houses or central :stations on board ship. 9.. Of the considerable vibration which affects the magnetized needle in torpedo boats and motor boats.
  • the rotary frame may in fact be placed at a spot (for instance. on a mast) 1 where perfeet compensation can be made readily and i with certainty.
  • FIG. 1 in elevation, and in Fig. 2 in plan.
  • Figs. 3 and 4 are diagrammatic representations of tables containing previously determined values of-the coetlicicntsof the apparatus and theangles of deviation. .Figs.
  • Fig. .5 is. an elevation showing. the general arrange ment ofthe apparatus. Fig. (his an axial section through, the .frame and the. disks.
  • Fig. 7 is a plan thereof.
  • Fig. 8 is a dia-. themanner. in which the deviation is to beread off .from the appan ratus of Fig.6.
  • Fig. 9 is a separate view of the receiving and indicating apparatus The device shown in Figs. 1 and 2 is composed of a, preferably circular, frame A, of
  • a horizontal disk D of insulating material At right anglesto the axle and rigidly fixed to it there is provided a horizontal disk D of insulating material.
  • the circumference of the disk is covered with a metal band E cut in two places a a by very fine cuts situated at the ends of that diameter of the disk D which is perpendicular to the plane of the frame A.
  • periphery there rub several pairs of brushes H H; each pair is located at the ends of one and the same diameter. These two pairs of brushes are indispensable. If greater accuracy is desired according to the sensitiveness of the galvanoineter employed,other pairs of brushes may be utilized situated at the ends .of the intermediate diameters. There are always two pairs situated at the ends'of two diameters located at right angles to each other.
  • Each of these pairs of brushes is connected by means of two insulated wires H H to a suitable measuring instrument such as a galvanometer of any suitable type.
  • the amount of the galvanometric deflection will indicate the magnetic deviation of the ship.
  • the rotary frame is tobe placed in some convenient spot on the ship where the magnetic compensation of the masses of iron and steel constituting it may be effected in an eflicient manner; an especially suitable spot is on a'mast.
  • the frame is caused to rotate in a uniform manner, and by means of a multipolar switch the two brushes of one and the same pair are connected to the two terminals of the galvanometer; and the deviation 8 is read off the latter.
  • the apparatus may, be completed in the following manner :It then comprises two windings on the same frame, and two pairs of half rings, these pairs being each connected to a galvanometer through the medium of suitable brushes and con- (luctors. Upon the mirror of each galvanometer there will be reflected respectively two relatively perpendicular lines which form on a dull glassplate or other surface images whose point of intersection serves for obtaining the deviation as hereinafter described.
  • the apparatus consists of a frame A, preferably CIICHla-I," in which are formed two parallel grooves capable of receiving two similar windings Band B. On the pivotal axis C C of the frame there are fixed two disks 1) and D of insulating material,
  • the angle M03 is equal to the angle; the magnetic deviation of the ship.
  • the magnetic deviation is obtained here by simply reading the same on the indicated radius vector on the'plate P without the use of tables, whereas in the first arrangement the coetiicient A rendered the use of tables necessary.
  • the dull-glass plate to rotate in a suitable direction through an angle equal to the declination of the locality of observation, the geographical deviation will be obtained.
  • --the receivin apparatus formed of two galvanometers and G havlng a movable frame and having their',axes perpendicular to each other, and having mirrors that form on a dull glass plate P the images of two wires F and F or two incandescent filaments at right angles to each other, may serve in all cases where it is desired to measure the proportion between the intensities of two currents, because these intensities are proportionate to Z and Z. For this purpose it will be suiiicient to graduate the radius vectors in values of tan, a.
  • Fig. 9 is a sep arate view of such apparatus.
  • the galvanometers G and G are connected in any desired way with the'circuits of the two currents in question, and they throw upon the plate or screen P images f, f of a pair of lines F and F, shifting the positions of said lines according to the intensities of the two currents, so that the point of intersection of said two lines will fall upon different'radii upon the screen, according to the relative intensities of the two currents in question.
  • This mechanism serves the same purpose whether used in connection with the other elements of the electromagnetic compass described or not.
  • a compass for determining magnetic deviation including in combination a coil adapted to be rotated in a magnetic field and in which induced currents are generated, a
  • vcurrent collecting ring with gaps at diametrically opposite points, electrical connections between said coil and ring a galvanometer, and brushes connecting said coil through said ring to said galvanometer to cause the latter to indicate the intensities of said currents.
  • a compass for determining magnetic deviation including in combination an armature frame carrying at least one winding and adapted to receive a uniform rotary motion about a vertical axis, a pair of half rings and means for connecting them for rotation with said frame, at least two pairs of brushes contacting with said half rings and located on diameters at right angles to each other, one of these diameters being ada ted to be set parallel to the longitudinal axis of a ship, and the other at right angles thereto,
  • a galvanometer for connecting said pairs of, brushes alternately with said galvanometer, and means controlled by the galvanometer for indicating the angle between the axis of the ship and the magnetic meridian.
  • a compass for finding magnetic deviations including in combination a frame, a pair of windings carried thereon, separate pairs of half rings connected one pair to each of said windings, pairs of brushes for each of said pairs of half rings and adapted to be located on diameters one in the direction of the ship and another at right-angles thereto, galvanometers subject to simultaneous deflection, means connecting one of said galvanometers to each of said pairs of brushes, and an indicating apparatus controlled by said galvanometers for indicating the deviations of the direction of the ship.
  • An indicating apparatus includin two galvanometers having mirrors rotatab ie on horizontal axes perpendicular to each other, two wires arranged perpendicularly to each other and reflected by the respective mirrors of the galvanometers, a screen upon which said lines are reflected and upon which the position of the intersection of the line i11- dieates the relative positions of the mirrors, said screen being graduated in the manner of a mariners compass.

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)

Description

L. D. J. A. DUNOYER.
ELECTROMAGNETIC COMPASS. APPLICATION FILED 1mm, 1901.
989,134, I 4 Patented Apr. 11,1911.
3 SHEETS-BHBBT 1 -4- 1 4 J H I 1 .1 1 141' //vv/v TOR.-
L. D. J. A. DUNOYER. ELECTROMAGNETIC COMPASS. APPLICATION FILED MAB.5, 1907.
Patented Apr. 11, 1911.
3 SHEETS-SHEET 2.
INVENTORI WITNESSES:
fla MW L. D. J. A. DUNOYER.
ELECTROMAGNETIC COMPASS. APPLIOATION FILED Mum, 1907.
3 SHEETS-SHEET 3.
WITNESSES M/VE/VTOR:
Patented Apr. 11, 1911.
UNITED sTArnsggrENtr OFFICE.
LOUIS DOMINIQUE JOSEPH ARMANI) DUNOYEB, OF VERSAILLES, FRANCE.
ELECTROMAGNETIC COMPASS.
I Specification of Letters Patent. Patented Apr, 11, 1911.
Application filed March '5, 1907. Serial No. 360,770.
' To all whom it may concern:
magnetic field.
.this deflection which determines the angle inclosed by the longitudinal axis of the ship withthe magnetic meridian.
This apparatus will be particularly useful for obviating the disturbing effect upon the needle compass: 1. Of the masses of iron or steelsurrounding the deck houses or central :stations on board ship. 9.. Of the considerable vibration which affects the magnetized needle in torpedo boats and motor boats. The rotary frame may in fact be placed at a spot (for instance. on a mast) 1 where perfeet compensation can be made readily and i with certainty.
- An apparatus. embodying the invention is shown in the accompanying drawings, in
. gram. showing shown diagrammatically in Fig.5. 1
Figure 1 in elevation, and in Fig. 2 in plan. Figs. 3 and 4 are diagrammatic representations of tables containing previously determined values of-the coetlicicntsof the apparatus and theangles of deviation. .Figs.
5, 6, and 7 refer to a modification. Fig. .5 is. an elevation showing. the general arrange ment ofthe apparatus. Fig. (his an axial section through, the .frame and the. disks.
Fig. 7 is a plan thereof. Fig. 8 is a dia-. themanner. in which the deviation is to beread off .from the appan ratus of Fig.6. Fig. 9 is a separate view of the receiving and indicating apparatus The device shown in Figs. 1 and 2 is composed of a, preferably circular, frame A, of
insulating materialcor of a metallic substance in which slots are suitably made so .as'to. prevent the generation .of Foucault currents. Upon this frame is wound insulated copper wire .13. 'The frame is capable of rotating on a vertical axle C situated "in its plane and passing through its center,
this motion being imparted to it by any desired means. i
At right anglesto the axle and rigidly fixed to it there is provided a horizontal disk D of insulating material. The circumference of the disk is covered with a metal band E cut in two places a a by very fine cuts situated at the ends of that diameter of the disk D which is perpendicular to the plane of the frame A. 'Each of the two conducting semi-peripheries thus formed, is connected to one, end of the wire that is wound on the frame. periphery there rub several pairs of brushes H H; each pair is located at the ends of one and the same diameter. These two pairs of brushes are indispensable. If greater accuracy is desired according to the sensitiveness of the galvanoineter employed,other pairs of brushes may be utilized situated at the ends .of the intermediate diameters. There are always two pairs situated at the ends'of two diameters located at right angles to each other. Each of these pairs of brushes is connected by means of two insulated wires H H to a suitable measuring instrument such as a galvanometer of any suitable type. v
The amount of the galvanometric deflection will indicate the magnetic deviation of the ship.
The rotary frame is tobe placed in some convenient spot on the ship where the magnetic compensation of the masses of iron and steel constituting it may be effected in an eflicient manner; an especially suitable spot is on a'mast.
No part of the apparatus should be of iron.
To use the apparatus, the frame is caused to rotate in a uniform manner, and by means of a multipolar switch the two brushes of one and the same pair are connected to the two terminals of the galvanometer; and the deviation 8 is read off the latter.
.ssuming that use is made at first of the pair of brushes fixed at the ends of the diametcr'per endicularto the longitudinal axis of the ship, and let a. be the magnetic deviation of the ship that is to say, the angle inclosed by its axis with the magnetic meridian then we have tan. 8=A'. sin. It now by means of the multipolar switch,
On this conducting use he made of the-pair of brushes fixed to the ends of the diameter parallel to the axis of the ship, the deviation 8 is given by the equation tan. 8:A. cos. a.
We have then tan? S-l-tan? 8:A2.
These two values thus serve to determine the coeflicient'A- It is only necessary to determine those two .values from time to time forthe purpose of determining the value of the coefficient A which varies with the longi-,
tude the latitude and the rotation of the frame. I
In practice a table in double entry of the velocity of the values of A will be prepared beforehand,by arranging the values of the horizontal com-, ponent H of the earths field in vertical columns and arranging the values N of the number of revolutions per second-in horizontal lines. This table having been prepared, a second table 'is then prepared (see galvanometer.
the diagram Fig. 3) showing the values of A in a vertical column at the left as indicated and those of a. in a horizontal line at the top as indicated at 1. In the compart-' ments 4: 4 of this table will be found the values of 8 and of 8'. Finally a third table (see the diagram Fig. 4) contains in the left hand column 4, the values of 8. and in the top line 4 the values of 8, and in these compartments 1 the corresponding values of'A and of 0,. These two last tables are infront of the eyes of the steersman. They allow of solving the following two practical problems 1. To follo'w a give-n course-This consists in giving a at every moment. A is determined from time toiime by the method hereinbefore described. The second table alone thus gives the. deviation 8 which the steersman must keep in the galvanometer by suitable steering.
%. To take a gi ven course.A and 8 of the given course are determined; this gives a from the third table. It is necessary therefore to Veer by the angles u from the magneticdeviati'on a at the time. The second table is then inspected alon the topline to find the column correspondlng to the 'angle a+u,' the compartment thus found gives the deflection 8 which must be imparted to the With the object of obviating the two measurements of 8 as hereinabove stated, and also of dispensing with the use of the two tables, the apparatus may, be completed in the following manner :It then comprises two windings on the same frame, and two pairs of half rings, these pairs being each connected to a galvanometer through the medium of suitable brushes and con- (luctors. Upon the mirror of each galvanometer there will be reflected respectively two relatively perpendicular lines which form on a dull glassplate or other surface images whose point of intersection serves for obtaining the deviation as hereinafter described.
The apparatus consists of a frame A, preferably CIICHla-I," in which are formed two parallel grooves capable of receiving two similar windings Band B. On the pivotal axis C C of the frame there are fixed two disks 1) and D of insulating material,
on the circumference of which there are arloid or any other analogous selnl-tran'sparent substance) an image f of a fixed wire F parallel to its axis Likewise, the mirror m 'ofthe galvanometer G gives an image f of a straight line F parallel to its axis. If
the frame A of the transmitter be caused to rotate, these images 7 and f which ,are perpendicular to each other, will move over the dull glass plate P on which there is engraved a series of radius vectors spaced suitably apart in the form .of' a marmers compass card divided into 360 degrees; each radius vector bein marked with a sign such as N, NE, &c. all but one being omitted from Fig. Qfor the sake of clearness). The radius vector on which the crossing point of the two perpendicular images f and 7" stops, indicates the magnetic deviation of the ship. In fact, if u. be this. magnetic deviation, the diagram (Fig. 8) show that Z=A sin. d Z=A cos. a
the angle a. being indicated at the point 1. Z and Z representing the displacement of the images which is proportionate to the de fiection of the galvanometers, and A being a coefiicient which varies with the longitude, the latitude and the velocity of the rotation of the frame.
From the two preceding equations, there results %=tan.a.
If 03 and OX represent the two images f and f, and OM the radius vector upon which the crossing points of said images lie I then the angle M03 is equal to the angle; the magnetic deviation of the ship. Thus in this case, the magnetic deviation is obtained here by simply reading the same on the indicated radius vector on the'plate P without the use of tables, whereas in the first arrangement the coetiicient A rendered the use of tables necessary. Furthermore, by causing the dull-glass plate to rotate in a suitable direction through an angle equal to the declination of the locality of observation, the geographical deviation will be obtained. Finally,--the receivin apparatus formed of two galvanometers and G havlng a movable frame and having their',axes perpendicular to each other, and having mirrors that form on a dull glass plate P the images of two wires F and F or two incandescent filaments at right angles to each other, may serve in all cases where it is desired to measure the proportion between the intensities of two currents, because these intensities are proportionate to Z and Z. For this purpose it will be suiiicient to graduate the radius vectors in values of tan, a.
Applicant reserves the right of modifying the dimensions or the details of this apparatus for the purpose of applying it to the measuring of the proportion between the intensities of two currents. Fig. 9 is a sep arate view of such apparatus. The galvanometers G and G are connected in any desired way with the'circuits of the two currents in question, and they throw upon the plate or screen P images f, f of a pair of lines F and F, shifting the positions of said lines according to the intensities of the two currents, so that the point of intersection of said two lines will fall upon different'radii upon the screen, according to the relative intensities of the two currents in question. This mechanism serves the same purpose whether used in connection with the other elements of the electromagnetic compass described or not.
Claims.
1. A compass for determining magnetic deviation, including in combination a coil adapted to be rotated in a magnetic field and in which induced currents are generated, a
vcurrent collecting ring with gaps at diametrically opposite points, electrical connections between said coil and ring a galvanometer, and brushes connecting said coil through said ring to said galvanometer to cause the latter to indicate the intensities of said currents.
2. A compass for determining magnetic deviation, including in combination an armature frame carrying at least one winding and adapted to receive a uniform rotary motion about a vertical axis, a pair of half rings and means for connecting them for rotation with said frame, at least two pairs of brushes contacting with said half rings and located on diameters at right angles to each other, one of these diameters being ada ted to be set parallel to the longitudinal axis of a ship, and the other at right angles thereto,
a galvanometer, wires H and H for connecting said pairs of, brushes alternately with said galvanometer, and means controlled by the galvanometer for indicating the angle between the axis of the ship and the magnetic meridian.
3. A compass for finding magnetic deviations, including in combination a frame, a pair of windings carried thereon, separate pairs of half rings connected one pair to each of said windings, pairs of brushes for each of said pairs of half rings and adapted to be located on diameters one in the direction of the ship and another at right-angles thereto, galvanometers subject to simultaneous deflection, means connecting one of said galvanometers to each of said pairs of brushes, and an indicating apparatus controlled by said galvanometers for indicating the deviations of the direction of the ship.
4. An indicating apparatus includin two galvanometers having mirrors rotatab ie on horizontal axes perpendicular to each other, two wires arranged perpendicularly to each other and reflected by the respective mirrors of the galvanometers, a screen upon which said lines are reflected and upon which the position of the intersection of the line i11- dieates the relative positions of the mirrors, said screen being graduated in the manner of a mariners compass.
In witness whereof, I have hereunto signed my name this 22d day of February 1907, in the presence of two subscribing witnesses.
LOUIS DOMINIQUE JOSEPH ARMANI) DUNOYER. Witnesses:
ltL-uzcrn ARMENGAUD, J eune, Hmmanno DE Soro.
US36077007A 1907-03-05 1907-03-05 Electromagnetic compass. Expired - Lifetime US989134A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US36077007A US989134A (en) 1907-03-05 1907-03-05 Electromagnetic compass.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US36077007A US989134A (en) 1907-03-05 1907-03-05 Electromagnetic compass.

Publications (1)

Publication Number Publication Date
US989134A true US989134A (en) 1911-04-11

Family

ID=3057472

Family Applications (1)

Application Number Title Priority Date Filing Date
US36077007A Expired - Lifetime US989134A (en) 1907-03-05 1907-03-05 Electromagnetic compass.

Country Status (1)

Country Link
US (1) US989134A (en)

Similar Documents

Publication Publication Date Title
US2109283A (en) Instrument for indicating navigational factors
US2758377A (en) Navigation instrument
US989134A (en) Electromagnetic compass.
US2701875A (en) Resistance type of phase shifter
US2542018A (en) Compass
US1774458A (en) Compass
Barnett New researches on magnetization by rotation and the gyromagnetic ratios of ferromagnetic substances
US2679033A (en) Pictorial indicator
US1047157A (en) Device for determining direction.
US2067467A (en) Method of and means for indicating relative angular movements
US2085010A (en) Aircraft drift indicator
US2286406A (en) Telemetric device
US2264279A (en) Radio navigation device
US3486816A (en) Approach aid display system
US441973A (en) rapieff
US551295A (en) Fourths to george citismore and eugene p
US1067808A (en) Gyroscopic compass.
US2490102A (en) Magnetic field angular gradientometer
US533340A (en) Instrument for taking astronomical observations at sea
US3215823A (en) Pictorial position display and course line compouter
US2929553A (en) Automatic aircraft navigator
US691393A (en) Electrical measuring instrument.
US2857673A (en) Computer for solution of unknown sides or angles of a triangle or of triangles
US1626123A (en) Gyrocompass relay transmitter
US1837292A (en) Gyroscopic compass