US3234657A - Magnetic compass - Google Patents
Magnetic compass Download PDFInfo
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- US3234657A US3234657A US209570A US20957062A US3234657A US 3234657 A US3234657 A US 3234657A US 209570 A US209570 A US 209570A US 20957062 A US20957062 A US 20957062A US 3234657 A US3234657 A US 3234657A
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- housing
- compass
- card
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- magnetic
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C17/00—Compasses; Devices for ascertaining true or magnetic north for navigation or surveying purposes
Definitions
- the present invention relates to compasses, more particularly to magnetic compasses of the type suitable for use in boats, aircraft, motor vehicles and the like, and the p'rincipal object of the invention is' to provide new and improved compasses of the character described.
- the present invention provides a compass wherein a resilient wire-like member supporting a card and magnet assembly and at its intermediate portion providing a lubber line, has portions respectively underlying and overlying the assembly and held in predetermined position by resilient engagement in respective grooves formed in the compass housing, to provide a simplified construction.
- FIGURE 1 is a front elevational view of an embodiment of the improved compass
- FIGURE 2 is an enlarged, side elevational view thereof, the near side of the outer casing being removed and certain parts being shown in section to illustrate the interior construction
- FIGURE 3 is a sectional view of a detail prior to assembly
- FIGURE 4 is a perspective view of two details prior to their assembly with each other
- FIGURE 5 is a perspective view of another detail
- FIGURE 6 is an enlarged, fragmentary sectional view of still another detail.
- the present invention comprises an outer casing 10 of plastic or the like which encloses the about to be described compass mechanism.
- the casing it is preferable to form the casing to provide a front portion 11 and a rear portion 12 which are adapted to be secured together by screws or the like, not shown.
- an assembly Positioned substantially centrally of casing 10 is an assembly which comprises a housing 13 in which a compass card 14 is rotatably mounted.
- the front portion 15 of housing 13 is rounded at 16 and at least this portion of the housing is transparent so that the compass card may be seen and read through the housing wall.
- Front portion 11 of casing 10 is apertured at 17 to provide a window through which the front portion of housing 13 is visible.
- rounded portion 16 of housing portion 15 magnifies compass card 14 and makes it appear larger, thus making the compass easier to read.
- housing 13 rests upon an opaque plate 100.
- a light bulb 101 carried by a suitable socket 102 which is in turn carried by the rear portion 12 of outer casing 10, is positioned beneath plate 100.
- one or more suitable apertures 103 are formed in plate 100 to permit light from bulb 101 to escape to the interior of housing 13 so as to illuminate the compass card 14.
- aperture 103 is disposed adjacent the front wall 16 of the housing 13 intermediate the periphery of the compass card and the periphery of the housing so as to illuminate that portion of the compass card visible through the housing wall 16.
- Compass card 14 is conventional in that it comprises an inverted cup of non-magnetic material having a central depending stud 18 (see FIGURE 3) whose lower end tapers to a point to provide a low friction pivot.
- Card 14 has the usual magnets 19 secured thereto for making it responsive to the earths magnetic lines of force and the exterior of the card carries the usual indicia.
- stud 18 rests in a concavity formed in the upper surface of a jewel 20 which is secured inside a sleeve 21.
- the lower end of sleeve 21 is soldered or otherwise secured to an upstanding portion 22 of a supporting member 23 which is nonmagnetic and preferably somewhat resilient.
- supporting member 23 has a lower portion 24 which extends transversely of portion 22, an upper portion 25 which lies in substantially the same plane as portion 24, and an intermediate connecting portion 26.
- portion 25 of supporting member 23 is spaced apart sufficiently from portion 24 so that the compass card may be assembled, as shown, with the supporting member.
- subsequent assembly operations will spring portion 25 and maintain it in the dot-dash line position to prevent disassembly between the compass card and the supporting member.
- portion 26 serves not only to connect portions 24, 25, but also serves as a lubber line.
- compass card 14 is encased in a housing 13.
- This housing is preferably substantially flat on top and bottom and as best seen in FIG- URE 24, comprises the previously mentioned front portion 15 together with a rear portion 27. As will appear, these portions are adapted to be fused together to form the complete housing.
- the inside of housing portion 15 is formed to provide spaced, inwardly directed respective upper and lower grooves 28 and 29 for receiving the supporting member 23.
- supporting member portion 25 will be sprung to its dot-dash line position shown in FIGURE 3; and the assembly then slid into housing portion 15 with member portion 26 foremost.
- supporting member portion 24 will be slid into groove 29 while portion 25 will be slid into groove 28.
- the spacing between grooves 28, 29 is such that supporting member portion will be held in the dot-dash line position shown in FIGURE 3 and in the full line position shown in FIGURE 2, to prevent disassembly of the compass card from the supporting member.
- the resiliency of the supporting member will tightly wedge the latter and the housing portion 15 together against unintentional disassembly as will be clear.
- housing 13 is adapted to be filled with a suitable liquid to dampen oscillatory movement of the compass card and since the housing is sealed, means must be provided to permit expansion and contraction of the dampening liquid resulting from temperature variations.
- the present invention provides a highly effective, low cost construction for accommodation of this expansion and contraction and such construction possesses none of the disadvantages of the prior art constructions as hereinabove pointed out.
- the present invention is similar to one of the previously mentioned prior art constructions in that it provides a bubble of air or other compressible fluid within the housing; however, this bubble is trapped Within the housing and is hidden from view regardless of the position in which the assembled compass is held.
- the bubble is encased in a transparent, flexible envelope which is permanently secured in a predetermined position within the housing.
- a thin, preferably transparent membrane 30 of a suitable plastic or the like (which is, of course, insoluble in the dampening liquid) encloses the bubble.
- membrane 30 is cemented to the exterior of a thin, preferably transparent body 31 which is configurated similar to housing portion 27 but which is smaller so as to fit therewithin.
- body 31 In order to maintain body 31 in position, it is formed with a plurality of ears 32 (herein shown to be four in number) which engage the interior of housing portion 27 and which also engage respective lugs 33 which project from the interior of the curved side walls and from the flat, top and bottom walls of this housing portion.
- ears 32 herein shown to be four in number
- faces 34 of the housing portions will be sealed together.
- one or both faces 34 will be moistened with a suitable liquid which softens the material. The faces will then be pressed together and held until the liquid evaporates thus leaving the two housing portions fused together into an integral, leak-proof unit.
- the two housing portions may be secured together by means of a suitable cement. It will be seen in FIGURE 2 that after assembly, supporting member 23 engages body 31 and prevents shifting thereof within the housing.
- the completed housing With housing portions 15, 27 fused or otherwise secured together, the completed housing will be filled with the usual dampening liquid through an aperture 35 formed in housing portion 27. It is to be understood that it is important the interior of the housing be completely filled and that no free air bubble be entrapped therein because a free air bubble would create the impression that some of the dampening liquid had escaped from the housing.
- aperture 35 in housing 13 is adapted to be closed by means of a cap 36 which overlies aperture 35 and which is preferably formed of sub: stantially the same material as is housing portion 27.
- the underside of cap 36 is adapted to be moistened with a suitable softening liquid which may be similar to that used in fusing housing portions 15, 27 together. The cap will then be pressed against the exterior of housing portion 27, so as to overlie aperture 25, until the softening liquid evaporates to thereupon fuse cap 36 to the housing and provide a leak-proof joint therebetween.
- cap 36 In order to insure that no air bubbles will be trapped beneath cap 36 the cap is provided with a tapered projection which fits within aperture 35. As the cap is positioned in place, the projection will displace a quantity of liquid from the housing to insure that no air is entrapped beneath the cap. Further, projection 37, as it enters the aperture, insures that cap 36 is properlypositioned overlying the aperture.
- housing 13 With housing 13 assembled as heretofore described, a workable, accurate compass is provided. However, this compass would be accurate only when used in a locality free of local magnetic fields. In the event the compass is used in an automobile or aircraft or the like, it is necessary to provide means for neutralizing the effect of such local field on the compass in order to permit it to read accurately.
- a compass comprising a magnetic body, a wire-like member underlying and pivotally supporting said body and having vertically spaced portions, and a housing for said body having groove means for closely receiving respective member portions therein to hold said member and thus said body in predetermined position within said housing.
- a compass comprising a compass card having marklngs for, indicating various magnetic heading, a wire-like member having a first portion underlying said card and providing a pivotal support about which said card is rotatable about a generally vertical axis, a second portion overlying said card and limiting movement thereof away from said first member portion, and an intermediate portion connecting said first and second member portions and spaced transversely of said pivotal support axis to provide a lubber line, and a housing enclosing said card and said member and providing vertically spaced grooves for respectively receiving said first and second member portions to maintain said member and thus said card in predetermined position within said housing.
- ROBERT B. HULL Primary Examiner.
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- Radar, Positioning & Navigation (AREA)
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Description
Feb. 15, 1966 w. E. HULL MAGNETIC COMPASS 2 Sheets-Sheet 1 Original Filed April 29, 1957 a z 0 0 w 3 4/ w v 5 H :5 3 E w :5 U 1/ O D L 5 4 E a u a i 4 1 M 1 H awn/MM WALTER E. HULL Feb. 15, 1966 Original Filed April 29, 1957 W. E. HULL MAGNETIC COMPASS 2 Sheets-Sheet 2 3mm WALTL'R E. HULL United States Patent 3,234,657 MAGNETIC COMPASS Walter E. Hull, RD. 3, Cortland, Ohio Original application Apr. 29, 1957, Ser. No. 655,757, now Patent No. 3,079,698, dated Mar. 5, 1963. Divided and this application July 13, 1962, Ser. No. 209,570 4 Claims. (Cl. 33'222) The present invention relates to compasses, more particularly to magnetic compasses of the type suitable for use in boats, aircraft, motor vehicles and the like, and the p'rincipal object of the invention is' to provide new and improved compasses of the character described.
This application is a division of my co-pending application for Letters Patent entitled Magnetic Compass, Serial Number 655,757, filed April 29, 1957, now Letters Patent 3,079,698, and which is in turn a continuation-inpart of Letters Patent 2,943,398.
The present invention provides a compass wherein a resilient wire-like member supporting a card and magnet assembly and at its intermediate portion providing a lubber line, has portions respectively underlying and overlying the assembly and held in predetermined position by resilient engagement in respective grooves formed in the compass housing, to provide a simplified construction. This and other advantages will readily become apparent from a study of the following description and from the drawings appended thereto.
In the drawings accompanying this specification and forming a part of this application there is shown, for purpose of illustration, an embodiment which the invention may assume, :and in these drawings:
FIGURE 1 is a front elevational view of an embodiment of the improved compass,
FIGURE 2 is an enlarged, side elevational view thereof, the near side of the outer casing being removed and certain parts being shown in section to illustrate the interior construction,
FIGURE 3 is a sectional view of a detail prior to assembly,
FIGURE 4 is a perspective view of two details prior to their assembly with each other,
FIGURE 5 is a perspective view of another detail, and
FIGURE 6 is an enlarged, fragmentary sectional view of still another detail.
With reference to FIGURES 1 and 2, the present invention comprises an outer casing 10 of plastic or the like which encloses the about to be described compass mechanism. To facilitate assembly of the various parts, it is preferable to form the casing to provide a front portion 11 and a rear portion 12 which are adapted to be secured together by screws or the like, not shown.
Positioned substantially centrally of casing 10 is an assembly which comprises a housing 13 in which a compass card 14 is rotatably mounted. The front portion 15 of housing 13 is rounded at 16 and at least this portion of the housing is transparent so that the compass card may be seen and read through the housing wall. Front portion 11 of casing 10 is apertured at 17 to provide a window through which the front portion of housing 13 is visible. As will be apparent, rounded portion 16 of housing portion 15 magnifies compass card 14 and makes it appear larger, thus making the compass easier to read.
In the present embodiment and as seen in FIGURE 2, housing 13 rests upon an opaque plate 100. A light bulb 101, carried by a suitable socket 102 which is in turn carried by the rear portion 12 of outer casing 10, is positioned beneath plate 100. At the present time, one or more suitable apertures 103 are formed in plate 100 to permit light from bulb 101 to escape to the interior of housing 13 so as to illuminate the compass card 14. In order to provide a desirable soft lighting effect on the compass card, aperture 103 is disposed adjacent the front wall 16 of the housing 13 intermediate the periphery of the compass card and the periphery of the housing so as to illuminate that portion of the compass card visible through the housing wall 16.
As in conventional constructions, stud 18 rests in a concavity formed in the upper surface of a jewel 20 which is secured inside a sleeve 21. The lower end of sleeve 21 is soldered or otherwise secured to an upstanding portion 22 of a supporting member 23 which is nonmagnetic and preferably somewhat resilient.
In the present embodiment, supporting member 23 has a lower portion 24 which extends transversely of portion 22, an upper portion 25 which lies in substantially the same plane as portion 24, and an intermediate connecting portion 26. In the position of parts shown in full lines in FIGURE 3, portion 25 of supporting member 23 is spaced apart sufficiently from portion 24 so that the compass card may be assembled, as shown, with the supporting member. However, as will later be disclosed, subsequent assembly operations will spring portion 25 and maintain it in the dot-dash line position to prevent disassembly between the compass card and the supporting member. As will be understood, portion 26 serves not only to connect portions 24, 25, but also serves as a lubber line.
As heretofore disclosed, compass card 14 is encased in a housing 13. This housing is preferably substantially flat on top and bottom and as best seen in FIG- URE 24, comprises the previously mentioned front portion 15 together with a rear portion 27. As will appear, these portions are adapted to be fused together to form the complete housing. The inside of housing portion 15 is formed to provide spaced, inwardly directed respective upper and lower grooves 28 and 29 for receiving the supporting member 23.
To assemble compass card 14 and supporting member 23 with housing portion 15 and after compass card stud 18 has been inserted in sleeve 21 to rest upon jewel 20, supporting member portion 25 will be sprung to its dot-dash line position shown in FIGURE 3; and the assembly then slid into housing portion 15 with member portion 26 foremost. As indicated, supporting member portion 24 will be slid into groove 29 while portion 25 will be slid into groove 28. It is to be understood that the spacing between grooves 28, 29 is such that supporting member portion will be held in the dot-dash line position shown in FIGURE 3 and in the full line position shown in FIGURE 2, to prevent disassembly of the compass card from the supporting member. The resiliency of the supporting member will tightly wedge the latter and the housing portion 15 together against unintentional disassembly as will be clear.
As in conventional constructions, housing 13 is adapted to be filled with a suitable liquid to dampen oscillatory movement of the compass card and since the housing is sealed, means must be provided to permit expansion and contraction of the dampening liquid resulting from temperature variations. The present invention provides a highly effective, low cost construction for accommodation of this expansion and contraction and such construction possesses none of the disadvantages of the prior art constructions as hereinabove pointed out.
The present invention is similar to one of the previously mentioned prior art constructions in that it provides a bubble of air or other compressible fluid within the housing; however, this bubble is trapped Within the housing and is hidden from view regardless of the position in which the assembled compass is held. Briefly, the bubble is encased in a transparent, flexible envelope which is permanently secured in a predetermined position within the housing.
As best seen in FIGURES 2 and 5, a thin, preferably transparent membrane 30 of a suitable plastic or the like (which is, of course, insoluble in the dampening liquid) encloses the bubble. In the present embodiment, membrane 30 is cemented to the exterior of a thin, preferably transparent body 31 which is configurated similar to housing portion 27 but which is smaller so as to fit therewithin. In order to maintain body 31 in position, it is formed with a plurality of ears 32 (herein shown to be four in number) which engage the interior of housing portion 27 and which also engage respective lugs 33 which project from the interior of the curved side walls and from the flat, top and bottom walls of this housing portion. Under certain circumstances, it may be desirable to cement or otherwise secure membrane 30 directly to the interior of the housing portion.
With the support member and the compass card assembly positioned in housing portion 15 and with body 31 positioned in housing portion 27, faces 34 of the housing portions will be sealed together. In the present embodiment, one or both faces 34 will be moistened with a suitable liquid which softens the material. The faces will then be pressed together and held until the liquid evaporates thus leaving the two housing portions fused together into an integral, leak-proof unit. Obviously, instead of a softening liquid, the two housing portions may be secured together by means of a suitable cement. It will be seen in FIGURE 2 that after assembly, supporting member 23 engages body 31 and prevents shifting thereof within the housing.
With housing portions 15, 27 fused or otherwise secured together, the completed housing will be filled with the usual dampening liquid through an aperture 35 formed in housing portion 27. It is to be understood that it is important the interior of the housing be completely filled and that no free air bubble be entrapped therein because a free air bubble would create the impression that some of the dampening liquid had escaped from the housing.
As illustrated in FIGURE 2, aperture 35 in housing 13 is adapted to be closed by means of a cap 36 which overlies aperture 35 and which is preferably formed of sub: stantially the same material as is housing portion 27. Referring to FIGURE 6, the underside of cap 36 is adapted to be moistened with a suitable softening liquid which may be similar to that used in fusing housing portions 15, 27 together. The cap will then be pressed against the exterior of housing portion 27, so as to overlie aperture 25, until the softening liquid evaporates to thereupon fuse cap 36 to the housing and provide a leak-proof joint therebetween.
In order to insure that no air bubbles will be trapped beneath cap 36 the cap is provided with a tapered projection which fits within aperture 35. As the cap is positioned in place, the projection will displace a quantity of liquid from the housing to insure that no air is entrapped beneath the cap. Further, projection 37, as it enters the aperture, insures that cap 36 is properlypositioned overlying the aperture.
It should be pointed out that a more dependable closure is obtained by fusing cap 36 tothe exterior'of thehousing than by wedging a plug into the aperture as has been done in prior art devices. With the present construction, shrinkage of the housing'in the cap will not result in leak age since any stresses imposed by such shrinkage will be spread over a relatively large 7 area thus reducing the possibility of separation between the housing and the cap which would result in leakage of the dampening liquid from the housing.
With housing 13 assembled as heretofore described, a workable, accurate compass is provided. However, this compass would be accurate only when used in a locality free of local magnetic fields. In the event the compass is used in an automobile or aircraft or the like, it is necessary to provide means for neutralizing the effect of such local field on the compass in order to permit it to read accurately.
Neutralization of these local magnetic fields is accomplished by means of suitable compensating devices which are adjusted to set up a counter magnetic field which is, in its effect on the com-pass card, equal to and in the opposite direction to the local field, These compensating devices are contained within casing 10 and are indicated generally by the reference character 38 and since they are the subject of my co-pending application for Letters Patent herein above mentioned and form no part of the present invention, they will not herein further be described.
In view of the foregoing it will be apparent to those skilled in the art that I have accomplished at least the principal object of my invention and it will also be apparent to those skilled in the art that the embodiment herein described may be variously changed and modified, without departing from the spirit of the invention, and that the invention is capable of uses and has advantages not herein specifically described, hence it will be appreciated that the herein disclosed embodiment is illustrative only, and that my invention is not limited thereto.
I claim:
1. A compass comprising a magnetic body, a wire-like member underlying and pivotally supporting said body and having vertically spaced portions, and a housing for said body having groove means for closely receiving respective member portions therein to hold said member and thus said body in predetermined position within said housing.
2. The construction of claim 1 wherein said housing is formed of two housing parts secured together and wherein said groove means are formed in one of said housing parts.
3. A compass comprising a compass card having marklngs for, indicating various magnetic heading, a wire-like member having a first portion underlying said card and providing a pivotal support about which said card is rotatable about a generally vertical axis, a second portion overlying said card and limiting movement thereof away from said first member portion, and an intermediate portion connecting said first and second member portions and spaced transversely of said pivotal support axis to provide a lubber line, and a housing enclosing said card and said member and providing vertically spaced grooves for respectively receiving said first and second member portions to maintain said member and thus said card in predetermined position within said housing.
4. The construction of claim 3 wherein said first and second member portions are resiliently biased away from each other and wherein such portions are sprung into respective housing grooves.
References Cited by the Examiner UNITED STATES PATENTS 167,452 9/1875 Ile's 33-225 864,171 8/1907 Kean 33-222 1,972,708 9/1934 Hull 33-222 1,994,998 3/1935 Hull 33-22Z 2,020,905 11/1935 Robert 33'223' 2,202,154 5/1940 Kollsman 33223 2,242,126 5/ 1941 Holmes et al. 33--223- FOREIGN PATENTS 788,079 7/1935 France. 139,920 3/ 1920 Great Britain.
ROBERT B. HULL, Primary Examiner.
Claims (1)
1.A COMPASS COMPRISING A MAGNETIC BODY, A WIRE-LIKE MEMBER UNDERLYING AND PIVOTALLY SUPPORTING SAID BODY AND HAVING VERTICALLY SPACED PORTIONS, AND A HOUSING FOR SAID BODY HAVING GROOVE MEANS FOR CLOSELY RECEIVING RESPECTIVE MEMBER PORTIONS THEREIN TO HOLD SAID MEMBER AND THUS SAID BODY IN PREDETERMINED POSITIONS WITHIN SAID HOUSING.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US209570A US3234657A (en) | 1957-04-29 | 1962-07-13 | Magnetic compass |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US655757A US3079698A (en) | 1957-04-29 | 1957-04-29 | Magnetic compass |
US209570A US3234657A (en) | 1957-04-29 | 1962-07-13 | Magnetic compass |
Publications (1)
Publication Number | Publication Date |
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US3234657A true US3234657A (en) | 1966-02-15 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US209570A Expired - Lifetime US3234657A (en) | 1957-04-29 | 1962-07-13 | Magnetic compass |
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US (1) | US3234657A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3853089A (en) * | 1972-06-05 | 1974-12-10 | B Howard | Course selector and indicator |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US167452A (en) * | 1875-09-07 | Improvement in mariners compasses | ||
US864171A (en) * | 1905-08-31 | 1907-08-27 | Kelvin And James White Ltd | Mariner's compass. |
GB139920A (en) * | 1919-04-11 | 1920-03-18 | William Charles Gardiner | Improvements in and relating to magnetic compasses |
US1972708A (en) * | 1932-04-02 | 1934-09-04 | Walter E Hull | Magnetic compass |
US1994998A (en) * | 1934-03-23 | 1935-03-19 | Walter E Hull | Compensating device for compasses |
FR788079A (en) * | 1935-03-30 | 1935-10-03 | Aera Ets | Improvements to compasses intended for aeronautics |
US2020905A (en) * | 1933-01-12 | 1935-11-12 | Robert Guy Octave | Compensated compass, especially for aerial vehicles |
US2202154A (en) * | 1936-05-25 | 1940-05-28 | Square D Co | Aperiodic compass |
US2242126A (en) * | 1940-06-25 | 1941-05-13 | Bendix Aviat Corp | Remote indicator |
-
1962
- 1962-07-13 US US209570A patent/US3234657A/en not_active Expired - Lifetime
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US167452A (en) * | 1875-09-07 | Improvement in mariners compasses | ||
US864171A (en) * | 1905-08-31 | 1907-08-27 | Kelvin And James White Ltd | Mariner's compass. |
GB139920A (en) * | 1919-04-11 | 1920-03-18 | William Charles Gardiner | Improvements in and relating to magnetic compasses |
US1972708A (en) * | 1932-04-02 | 1934-09-04 | Walter E Hull | Magnetic compass |
US2020905A (en) * | 1933-01-12 | 1935-11-12 | Robert Guy Octave | Compensated compass, especially for aerial vehicles |
US1994998A (en) * | 1934-03-23 | 1935-03-19 | Walter E Hull | Compensating device for compasses |
FR788079A (en) * | 1935-03-30 | 1935-10-03 | Aera Ets | Improvements to compasses intended for aeronautics |
US2202154A (en) * | 1936-05-25 | 1940-05-28 | Square D Co | Aperiodic compass |
US2242126A (en) * | 1940-06-25 | 1941-05-13 | Bendix Aviat Corp | Remote indicator |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3853089A (en) * | 1972-06-05 | 1974-12-10 | B Howard | Course selector and indicator |
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