US2118082A - Compass alarm - Google Patents

Compass alarm Download PDF

Info

Publication number
US2118082A
US2118082A US64207A US6420736A US2118082A US 2118082 A US2118082 A US 2118082A US 64207 A US64207 A US 64207A US 6420736 A US6420736 A US 6420736A US 2118082 A US2118082 A US 2118082A
Authority
US
United States
Prior art keywords
compass
alarm
vessel
course
bowl
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
US64207A
Inventor
Jr John Hays Hammond
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 US64207A priority Critical patent/US2118082A/en
Application granted granted Critical
Publication of US2118082A publication Critical patent/US2118082A/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
    • G01C17/04Magnetic compasses with north-seeking magnetic elements, e.g. needles
    • G01C17/20Observing the compass card or needle
    • G01C17/26Observing the compass card or needle using electric pick-offs for transmission to final indicator, e.g. photocell
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S33/00Geometrical instruments
    • Y10S33/03Photoelectric

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Emergency Alarm Devices (AREA)

Description

y- 1938- J. H. HAMMOND, JR 2,118,082
COMPASS ALARM Filed Feb. 17, 1956 2 Sheets-Sheet l INVENTOR Y John Hays Hammond, Jr.
ATTORN EY May 24, 1938. J. H. HAMMOND, JR
COMPAS S ALARM 2 Sheets-Sheet 2 Filed Feb. 17, 1836 My \SNR.
INVENTOR John Hays Hammond, Jr.-
ATTORNEY Patented May 24, 1938 UNITED STATES PATENT OFFICE 1 Claim.
This invention relates to navigational instruments and more particularly to an improved system for automatically giving a warning when the vessel deviates from a given course.
More specifically the invention provides a system in which an alarm is automatically sounded when the vessel deviates more than a predetermined number of degrees from a set course fora definite interval of time.
10 An object of the invention is to provide a practical, dependable, and efficient system of the type above indicated.
Various other objects and advantages will be r apparent as the nature of the invention is more fully disclosed.
Although the novel features which are believed to be characteristic of this invention will be particularly pointed out in the claims appended hereto, the invention itself, as to its objects and 20 advantages, the mode of its operation and the manner of its organization may be better understood by referring to the following description taken in connection with the accompanying drawings forming a part thereof, in which I 25 Fig. 1 is a top plan view of the instrument with the casing removed and with the associated electrical circuits indicated diagrammatically, and
Fig. 2 is a sectional elevation of the instrument taken on line 2-2 of Fig. 1.
30 In the following description and in the claim parts will be identified by specific names for convenience, but they are intended to be as generic in their application to similar parts as the art will permit.
35 Referring more particularly to the accompanying drawings, a binnacle casing I is mounted on the bridge or other suitable'location on the vessel. A gimbal ring II is mounted in the cas ing ill on pivots I2 and ring i3 is'pivotally mount- 40 ed in the gimbal ring II by means of pivots l5.
Secured to the ring I3 is a second ring [6 on which is mounted a circular frame ll. Mounted in the frame I1 is a compass .bowl liiwhich is made of transparent material such for example as glass.
Over the top of the bowl I8 is mounted a circular lass plate is which is held in position by means of ring 2|. Mounted in the bowl i8 is a pivot 22,
on the point of which is rotatably mounted a 50 compass card 23 which may be of well known and standard construction. Attached to the compass card 23 directly below the north point thereof is a rectangular mirror 25, the width of which only extends a few degrees on either side of the north point of the compass. At the opposite side of the compass card 23 is located a counterweight 25 for balancing the weight of the mirror 25.
Rotatably mounted between the ring I6 and the frame I I is a second bowl 30. The upper edge of this bowl is inclined as shown at 3| and 5 is engraved with the points of the compass as shown in Fig. '1. A segmental hole 32 is cut through the frame I! so as to expose to view the points of the compass engraved on the surface 3i. A lubber line 33 is engraved on the frame I1 on the longitudinal line of the vessel.
Secured to the outside of the bowl 30 is a commutator 35 made of insulating material in which are mounted three slip rings 36, 31, and 38. Ber low the commutator 35 and secured to the bowl 30 is a beveled gear 39 with which meshes a beveled pinion 40. This pinion is secured to one end of a shaft 4|, which is rotatably mounted in a bracket 42 forming part of the ring l3. A knurled knob 43 is secured to the other end of the shaft 4|. A spiral compression spring 45 surrounds the shaft 4l between the pinion 40 and the bracket 42, thus locking the pinion 40 against the gear 39 to keep the latter from turning due to vibration, etc. A hinged door 46 is provided in the casing III in order to permit access to the knurled knob 43.
The slip rings 36 and 31 are connected to a lamp 41 which is mounted in the bowl 311. The light from this lamp is focused by means of a lens system 48 into a beam 49. This beam of light is reflected from a mirror 50 onto the mirror 25, mounted on the compass card 23. From the mirror 25 the beam of light is reflected by two mirrors 5i and 52 onto a photo-electric cell 53. This cell may be of the type known as a photronic cell manufactured by the Weston Electrical Instrument Company which does not need a source of power for its operation. The photo-electric cell 53 is connected to the two slip rings 31 and 38. 49
The three slip rings 36, 31', and 33 are engaged by three brushes 55, 56, and 51 which are mounted on a block of insulating material 58 which is secured to the ring i3. The three brushes 55,
56, and 51 are connected to a three conductor cable 62 having conductors 59, 60, and GI (Fig.
1-) This cable passes from the block of insulating material 53 along the under surface of the gimbal ring II and passes out through the casing Ill. The conductor 59 is.connected through a switch 63 to one side of a source of alternating current 55, the other side of this source being connected to the conductor 63. The conductor 50 is connected by a branch conductor 65 to one side of the winding of a sensitive relay-ii, the
other side of thewinding of which is connected to the conductor 6|.
The armature of the relay 6! is connected through a switch 88 to one side of the winding of a solenoid 69, the other side of the winding of which is connected through a battery 18 to the back contact of the relay 61. The solenoid 89 is provided with a core H to which is secured a collar I2. Between the collar 12 and the solenoid 89 is a spiral compression spring I3 which tends to hold the core 1| in its outmost position. Secured to the upper end of the core H is a piston I5 which reciprocates in a cylinder 16. This cylinder is provided with a large port l1 and a small port 18. A valve 19 is mounted over the large port I1.
Secured to the core H is an arm 8| of insulating material to which is attached a block 82 of con-' ducting material. Located in the path of travel of the block 82 are two contacts 85 and 86, the
former being connected to one'side of a battery 81 and the latter through a switch 88 to a lamp 89 and through a switch 98 to a bell 9|. The return circuits from the lamp 89 and the bell 9| are connected to the other side of the battery 81.
In the operation of the form of the invention.
just described, after it is determined upon which course the. vessel is to proceed, the door 48 in the binnacle' casing I8 is opened and the knurled knob.
88 is turned so as to cause rotation of the bowl 88 by means of the pinion 48 and the gear 89 ,until the desired course as shown by the compass scale engraved on the surface 3| registers with the lubber line 93. In the case shown in the accompanying figures, the desired course is due north so that this point registers with the lubber line 83. The helmsman then steers the vessel so that it is heading due north as indicated by the compass card 23. At this time the mirror 25 on the under surface of the compass card 23 will be in line with the optical system carried in-the bowl 38 so that light from the lamp 1 will impinge upon the photo-electric cell 58, thus energizing this cell which in turn will cause the energization of the sensitive relay 81. i
The switch 68 is then'closed and either or both of the switches 88 and 98'are closed as desired. As
. long-as the vessel remains on the predetermined course, in this case due north, the sensitive relay 8'! will remain energized thus preventing the em ergization of the solenoid 69. If, however, the vessel deviates more than a predetermined number of degrees from this course, the mirror 25 will move out of line with theoptical system, thereby shutting off the light to' the photo-electric cell 53 which in turn will cause deenergization of the sensitive relay 61. This in turn will close the circuit through the solenoid 89, thus causing the core of this solenoid to be moved slowly downward at a rate which is determined by the amount of-air entering the port 18.
If the vessel remains 01f its course for a prede, termined interval of time, the conducting block '82 will engage the contacts and 86, thereby tinue until the vessel is returned to its proper course, at which time the mirror 25 will again be in line with the optical system so that the photo-electric cell 53.will be again illuminated. This will energize the relay 81, thereby deenerglzing the solenoid 69. When this occurs, the core II will be moved rapidly upwards under the action of the spring 13 and due to the air freely passing out of the large port 11. The variation in azimuth required to interrupt the light beam is determined by the characteristics of the mirror 25 which may be designed to cause actuation of the warning signal after any desired angular deviation.
If the vessel deviates from its predetermined course sufficiently to energize the relay but is returned to the course before the core-1| of the solenoid-89 has moved sufilciently to cause the engagement of the contacts 85 and 88 by the conducting block 82,, the relay 8'! will be 'deenergized thereby allowing the core 'I| tomove rapidly upward to its initial position without causing the alarm to be sounded.
that it is not limited thereto, but any suitable number or type of systems may be employed which may be located at any part of the ship such as-in the captain's cabin or elsewhere to apprise the captain or other officers of the vessel that the proper course is not being maintained.
It is to be understood that any desired control mechanisms such as asteering control may be substituted for the alarm or may beconnected to the battery 81 in addition to the alarm signals set forth.- The circuits disclosed are merely illustrative of various control devices that can be actuated in response to a predetermined variation in azimuth of the vessel.
Although only a specific embodiment of the invention has been shown herein, it is to be understood that the invention is not limited to any specific construction but may be embodied in various forms without departing from the spirit of the invention or the scope of the appended claim.
What is claimed is:
In a navigational system, a housing, a compass card movable with respect thereto to indicate direction, a photoelectric system carried by said signal circuit when energized for a given time" interval, an energizing circuit for said electromagnetic means, a-relay biased to normally close said energizing circuit, and means controlled by said photoelectric cell to hold said relay open when said .light is focused thereon by said compass card, whereby said signal circuit is energized only in response to a deviation of said housing rela-.
tively to said card in either direction by more than a given angle and for said given time interval. JOHN HAYS HAMMOND, JR.
US64207A 1936-02-17 1936-02-17 Compass alarm Expired - Lifetime US2118082A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US64207A US2118082A (en) 1936-02-17 1936-02-17 Compass alarm

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US64207A US2118082A (en) 1936-02-17 1936-02-17 Compass alarm

Publications (1)

Publication Number Publication Date
US2118082A true US2118082A (en) 1938-05-24

Family

ID=22054290

Family Applications (1)

Application Number Title Priority Date Filing Date
US64207A Expired - Lifetime US2118082A (en) 1936-02-17 1936-02-17 Compass alarm

Country Status (1)

Country Link
US (1) US2118082A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2446258A (en) * 1943-11-29 1948-08-03 Lockheed Aircraft Corp Compass
US2447069A (en) * 1940-02-05 1948-08-17 Jr Philo Holcomb Signaling buoy
US2596994A (en) * 1944-12-09 1952-05-20 Ernest R Haberland Fluxmeter alarm
US2935792A (en) * 1957-09-23 1960-05-10 Garth B Huffaker Football position aligner
US3191306A (en) * 1963-03-18 1965-06-29 Kierans Martin De Valera Combination compass-clinometer and hand level
US3271754A (en) * 1963-07-09 1966-09-06 Johnson Service Co Monitoring system
US3802088A (en) * 1971-06-14 1974-04-09 Us Navy Guidance system for underwater swimmers
US6473979B2 (en) * 2000-12-05 2002-11-05 Clive S. Lu Electronic talking compass

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2447069A (en) * 1940-02-05 1948-08-17 Jr Philo Holcomb Signaling buoy
US2446258A (en) * 1943-11-29 1948-08-03 Lockheed Aircraft Corp Compass
US2596994A (en) * 1944-12-09 1952-05-20 Ernest R Haberland Fluxmeter alarm
US2935792A (en) * 1957-09-23 1960-05-10 Garth B Huffaker Football position aligner
US3191306A (en) * 1963-03-18 1965-06-29 Kierans Martin De Valera Combination compass-clinometer and hand level
US3271754A (en) * 1963-07-09 1966-09-06 Johnson Service Co Monitoring system
US3802088A (en) * 1971-06-14 1974-04-09 Us Navy Guidance system for underwater swimmers
US6473979B2 (en) * 2000-12-05 2002-11-05 Clive S. Lu Electronic talking compass

Similar Documents

Publication Publication Date Title
US2118082A (en) Compass alarm
US2133241A (en) Distance finder
US2608094A (en) Ground following map and navigation instrument
US2371606A (en) Bomb sight
US3668623A (en) Aircraft vertical flight position display instrument
US1885098A (en) Compass control system
US2472019A (en) Following and recording
US2112504A (en) Steering apparatus
US2319212A (en) Photoelectric control device
US2461075A (en) Pressure responsive indicating device
US3220252A (en) Integrated destination indicator
US1873579A (en) Aircraft control apparatus
US1692051A (en) Radio direction and position finder
US1880960A (en) Aerial camera
US3134295A (en) Pictorial display navigation equipment
US2323311A (en) Automatic altitude control
US3277484A (en) Aircraft flight instrument system
US2113947A (en) Automatic meter control
US2632882A (en) Alarm system for compass repeaters
US948424A (en) Ship-detector.
US2997895A (en) Control unit
US2437416A (en) Deep and shoal alarm
US2102512A (en) Automatic steering means
US2934690A (en) Automatic pilot
US2229004A (en) Remote control system