US3366923A - Vehicle direction indicating luminous indicator - Google Patents
Vehicle direction indicating luminous indicator Download PDFInfo
- Publication number
- US3366923A US3366923A US464363A US46436365A US3366923A US 3366923 A US3366923 A US 3366923A US 464363 A US464363 A US 464363A US 46436365 A US46436365 A US 46436365A US 3366923 A US3366923 A US 3366923A
- Authority
- US
- United States
- Prior art keywords
- screen
- panel
- bores
- direction indicating
- vehicle direction
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V11/00—Screens not covered by groups F21V1/00, F21V3/00, F21V7/00 or F21V9/00
- F21V11/08—Screens not covered by groups F21V1/00, F21V3/00, F21V7/00 or F21V9/00 using diaphragms containing one or more apertures
- F21V11/14—Screens not covered by groups F21V1/00, F21V3/00, F21V7/00 or F21V9/00 using diaphragms containing one or more apertures with many small apertures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2111/00—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00
- F21W2111/06—Use or application of lighting devices or systems for signalling, marking or indicating, not provided for in codes F21W2102/00 – F21W2107/00 for aircraft runways or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO THE FORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THE LIGHT EMITTED
- F21Y2105/00—Planar light sources
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21Y—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO THE FORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THE LIGHT EMITTED
- F21Y2115/00—Light-generating elements of semiconductor light sources
- F21Y2115/20—Electroluminescent [EL] light sources
Definitions
- the present invention refers to a differentiatedvisibility indicator device, particularly suitable for providing the right landing direction in heliports located on dry land or on board of ships.
- the object of the invention is to provide a device f the mentioned kind, suitable for providing with immediacy the helicopters pilot, during night-time hours and under conditions of poor visibility, with a luminous display indicative of the axis of the landing zone.
- the divice according to the invention has a variable visibility, which appears as complete only in a predetermined direction, coinciding with the landing direction.
- a device comprising, in combination, an electroluminescent panel arranged perpendicularly to the predetermined direction, and an opaque screen, having a corresponding shape and a predetermined thickness, superimposed on said panel and containing a plurality of axial bores, parallel to said direction, and of a diameter decreasing from the periphery toward the center of the screen, so that the complete visibility of said panel is obtained only when the observer is aligned with said direction, with an approximation which is given by the ratio of the diameter of the central bores to their length.
- FIGURE 1 is a cross-sectional view of the device
- FIGURE 2 is a front elevation.
- the numeral 2 designates an electroluminescent panel, applied on a protective bottom 3 housed within a recess 4 of an annular support 5 provided with holes 6 for fastening the assembly on a wall or a pivotable support not illustarated because already known.
- the electroluminescent panel 2 Above the electroluminescent panel 2 is mounted a cylindrical screen of an opaque material having a predetermined thickness, and provided with a plurality of axial bores designated by the numerical 7, extending throughout the thickness of the screen. As shown in FIGURE 2, the screen is ideally divided into concentric annular zones, in which the bores 7 have a diameter of a decreasing value from the periphery toward the center, where the bores are closer and have the smallest value.
- a transparent rim 9 covering an outer annular zone of the panel 2 so that said zone is visible from any direction substantially in front of the device.
- the transparent rim 9 is fastened 3,356,923 Patented Jan. 30, 1968 by jaws 8 provided with bolts to the support 5.
- a protective transparent covering may be provided, the purpose of which is to prevent the entrance of dust or other foreign materials into the bores 7.
- the zone of the electroluminescent panel 2 in which the larger bores are provided is visible within a range having an angular amplitude of about 9, while the concentric zones have a progressively smaller range of visibility up to the bores of the central zone which is visible through an angular amplitude of about 1.
- the device is mounted in proximity to the landing strip, with the central axis oriented according to the desired direction.
- the pilot sees only the outer annular band of the electroluminescent panel, that is the zone covered by the transparent rim 9. If the sight forms an angle smaller than 9, the pilot perceives the annular zone in which the larger bores are provided. Then he shall so maneuver as to discern the whole electroluminescent panel, insofar only under these conditions one has virtually the coincidence of the flight direction with the landing direction.
- the device disclosed is suitable for use also in other fields having the same requirements.
- the system is shaped as a disk, being however, obvious that it may take any shape and size, in connection to the specific modes of use, the luminous panel may be also illuminated as well, by means of a conventional luminous source.
- a differentiated-visibility luminous indicator device comprising, in combination, an electroluminescent panel arranged perpendicularly to a predetermined direction, and an opaque screen, having a corresponding shape and a predetermined thickness, superimposed on said panel and provided with a plurality of axial bores, parallel to said direction, and of a diameter decreasing from the periphery toward the center of the screen, so that the complete visibility of said panel is obtained only when the observer is aligned with said direction, with an approximation which is given by the ratio of the diameter of the central bores to their length.
- a device wherein a circumferential band of said panel is positioned outwardly to the screen and is protected by a transparent element, so that said circumferential band is visible from substantially any position in front of the device.
- a device wherein said panel is shaped 'as a disk, and said screen is ideally divided into concentric annular zones, every one of which has a plurality of bores of a constant diameter.
- a device wherein said electroluminescent panel is mounted on a support, and said screen is protected in the fore part by a protective transparent layer.
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Illuminated Signs And Luminous Advertising (AREA)
Description
Jan. 30, 1968 M. PANERAI ET AL 3,366,923
VEHICLE DIRECTION INDICATING LUMINOUS INDICATOR Filed June 16, 1965 //VVEN 70 66 MARJA DANERA! GIUSEPPS 'PnNsRm mamfimcajgmw.
United States Patent 3,366,923 VEHICLE DiRECTIGN INDZCATING LUMINOUS INDICATQR Maria Panerai and Giuseppe Panerai, both of No. 2 Piazza Galileo Ferraris, Florence, itaiy Filed June 16, 1965, Ser. No. 464,363 Claims priority, application Italy, June 22, 19nd, 13,471/64 4 Ciaims. (Cl. 349-25) ABSTRAQT 0F THE DISCLOSEURE A direction indicating luminuous panel provided with an adjacent opaque screen having a plurality of bores of decreasing diameter as measured from points adjacent the periphery of the screen progressively toward the center of the screen.
The present invention refers to a differentiatedvisibility indicator device, particularly suitable for providing the right landing direction in heliports located on dry land or on board of ships.
The object of the invention is to provide a device f the mentioned kind, suitable for providing with immediacy the helicopters pilot, during night-time hours and under conditions of poor visibility, with a luminous display indicative of the axis of the landing zone. In other words, the divice according to the invention has a variable visibility, which appears as complete only in a predetermined direction, coinciding with the landing direction.
According to the invention, it is provided a device comprising, in combination, an electroluminescent panel arranged perpendicularly to the predetermined direction, and an opaque screen, having a corresponding shape and a predetermined thickness, superimposed on said panel and containing a plurality of axial bores, parallel to said direction, and of a diameter decreasing from the periphery toward the center of the screen, so that the complete visibility of said panel is obtained only when the observer is aligned with said direction, with an approximation which is given by the ratio of the diameter of the central bores to their length.
The invention will now be described with reference to the attached drawings, showing by way of illustration and not of limitation a preferred embodiment of the invention.
In the drawings:
FIGURE 1 is a cross-sectional view of the device;
FIGURE 2 is a front elevation.
With reference to the drawings, the numeral 2 designates an electroluminescent panel, applied on a protective bottom 3 housed within a recess 4 of an annular support 5 provided with holes 6 for fastening the assembly on a wall or a pivotable support not illustarated because already known.
Above the electroluminescent panel 2 is mounted a cylindrical screen of an opaque material having a predetermined thickness, and provided with a plurality of axial bores designated by the numerical 7, extending throughout the thickness of the screen. As shown in FIGURE 2, the screen is ideally divided into concentric annular zones, in which the bores 7 have a diameter of a decreasing value from the periphery toward the center, where the bores are closer and have the smallest value. About the perforated screen is provided a transparent rim 9 covering an outer annular zone of the panel 2 so that said zone is visible from any direction substantially in front of the device. The transparent rim 9 is fastened 3,356,923 Patented Jan. 30, 1968 by jaws 8 provided with bolts to the support 5. In the front surface of the screen, a protective transparent covering may be provided, the purpose of which is to prevent the entrance of dust or other foreign materials into the bores 7.
As shown in FIGURE 1, the zone of the electroluminescent panel 2 in which the larger bores are provided, is visible within a range having an angular amplitude of about 9, while the concentric zones have a progressively smaller range of visibility up to the bores of the central zone which is visible through an angular amplitude of about 1.
The use of the device is as follows:
The device is mounted in proximity to the landing strip, with the central axis oriented according to the desired direction. When the pilot is approaching the landing strip, if the flight direction exceeds 9 of incidence to the landing direction, the pilot sees only the outer annular band of the electroluminescent panel, that is the zone covered by the transparent rim 9. If the sight forms an angle smaller than 9, the pilot perceives the annular zone in which the larger bores are provided. Then he shall so maneuver as to discern the whole electroluminescent panel, insofar only under these conditions one has virtually the coincidence of the flight direction with the landing direction.
Obviously, it is understood that the device disclosed is suitable for use also in other fields having the same requirements. In the drawings the system is shaped as a disk, being however, obvious that it may take any shape and size, in connection to the specific modes of use, the luminous panel may be also illuminated as well, by means of a conventional luminous source.
The present invention has been described in a preferred embodiment thereof, it being however understood that changes and modifications may be made therein without departing from the scope and the spirit of the invention.
What is claimed is:
1. A differentiated-visibility luminous indicator device, comprising, in combination, an electroluminescent panel arranged perpendicularly to a predetermined direction, and an opaque screen, having a corresponding shape and a predetermined thickness, superimposed on said panel and provided with a plurality of axial bores, parallel to said direction, and of a diameter decreasing from the periphery toward the center of the screen, so that the complete visibility of said panel is obtained only when the observer is aligned with said direction, with an approximation which is given by the ratio of the diameter of the central bores to their length.
2. A device according to claim 1 wherein a circumferential band of said panel is positioned outwardly to the screen and is protected by a transparent element, so that said circumferential band is visible from substantially any position in front of the device.
3. A device according to claim 1, wherein said panel is shaped 'as a disk, and said screen is ideally divided into concentric annular zones, every one of which has a plurality of bores of a constant diameter.
4. A device according to claim 1, wherein said electroluminescent panel is mounted on a support, and said screen is protected in the fore part by a protective transparent layer.
References Cited UNITED STATES PATENTS 1,255,755 2/1918 Ioh-anson 24046.51 3,277,455 10/1966 Viret et al. 340382 JOHN W. CALDWELL, Primary Examiner.
ALVIN H. WARING, Examiner.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT1347164 | 1964-06-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3366923A true US3366923A (en) | 1968-01-30 |
Family
ID=11144463
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US464363A Expired - Lifetime US3366923A (en) | 1964-06-22 | 1965-06-16 | Vehicle direction indicating luminous indicator |
Country Status (2)
Country | Link |
---|---|
US (1) | US3366923A (en) |
GB (1) | GB1078787A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3633157A (en) * | 1970-02-16 | 1972-01-04 | Us Navy | Helicopter visual-positioning aid |
US3771123A (en) * | 1971-03-04 | 1973-11-06 | A Lanes | Optical flashing light simulator and alerting device |
JPS5346908A (en) * | 1976-10-06 | 1978-04-27 | Ciba Geigy Ag | Novel compound as additive for lubricant and lubricating composition containing same |
US5291195A (en) * | 1990-02-20 | 1994-03-01 | H. Koch & Sons Co. | Target light for docking |
US20080121760A1 (en) * | 2006-11-29 | 2008-05-29 | Lundgren Mark A | Docking device |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE7600840L (en) * | 1976-01-27 | 1977-06-13 | Magnus Rutger Forss | DIRECTION DEVICE |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1255755A (en) * | 1917-07-25 | 1918-02-05 | Emil G Johanson | Lens-screen. |
US3277455A (en) * | 1964-02-06 | 1966-10-04 | Bendix Corp | Ambient light control on electroluminescent segments |
-
1965
- 1965-06-16 US US464363A patent/US3366923A/en not_active Expired - Lifetime
- 1965-06-21 GB GB26094/65A patent/GB1078787A/en not_active Expired
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1255755A (en) * | 1917-07-25 | 1918-02-05 | Emil G Johanson | Lens-screen. |
US3277455A (en) * | 1964-02-06 | 1966-10-04 | Bendix Corp | Ambient light control on electroluminescent segments |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3633157A (en) * | 1970-02-16 | 1972-01-04 | Us Navy | Helicopter visual-positioning aid |
US3771123A (en) * | 1971-03-04 | 1973-11-06 | A Lanes | Optical flashing light simulator and alerting device |
JPS5346908A (en) * | 1976-10-06 | 1978-04-27 | Ciba Geigy Ag | Novel compound as additive for lubricant and lubricating composition containing same |
US5291195A (en) * | 1990-02-20 | 1994-03-01 | H. Koch & Sons Co. | Target light for docking |
US20080121760A1 (en) * | 2006-11-29 | 2008-05-29 | Lundgren Mark A | Docking device |
US7607616B2 (en) * | 2006-11-29 | 2009-10-27 | The Boeing Company | Docking device |
Also Published As
Publication number | Publication date |
---|---|
GB1078787A (en) | 1967-08-09 |
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