US1384659A - ii ii i - Google Patents
ii ii i Download PDFInfo
- Publication number
- US1384659A US1384659A US1384659DA US1384659A US 1384659 A US1384659 A US 1384659A US 1384659D A US1384659D A US 1384659DA US 1384659 A US1384659 A US 1384659A
- Authority
- US
- United States
- Prior art keywords
- light
- source
- searchlight
- intensity
- horizon
- 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
Links
- 230000003287 optical Effects 0.000 description 16
- 239000000203 mixture Substances 0.000 description 4
- 239000012141 concentrate Substances 0.000 description 2
- 238000005286 illumination Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000006011 modification reaction Methods 0.000 description 2
- 239000011800 void material Substances 0.000 description 2
Images
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
- F21V5/00—Refractors for light sources
Definitions
- the searchlight forming-the subject of this invention complies in all respects with the above conditions.
- the invention is characterized by the provision, in connection with a searchlight, of an aperture or window by means of which it is possible to illuminate from the horizon to the zenith of the Searchlight in a continuous manner and with a single source of light.
- Figure 1 is a vertical section of a sea-rchlight constructed according to the invention.
- Fig. 2 is a front view of the optical panel ofthe searchlight.
- Fig. 3 shows a modification and
- Fig. 4 is a curve showing the ranges of the beam of lightof-the Searchlight.
- the Searchlight- consists essentially of an optical panel 1, composed of dioptric and catadioptric' elements.
- 2 designates a source of light, in this case anincandescent mantle, but any other source of light could be employed.
- table 3 supporting the optical system carries a crown wheel 4 meshing with the pinion 5 of a motor.
- the prismatic elements are arranged so as to concentrate the luminous rays emitted by the source of light 2 into a very intense beam limited, on the one hand, by the line AB which is horizontal, and on the other hand by the line CD, which forms withtthe certainal a certain angle a which is determined by practical considerations.
- the light source is at the focus of the optical panel 1, and in the center of the portion of the panel situated above the horizontal plane PF passing through the light source, i ig. 2, the prisms are supported by a double standard M having an interval or 'gap E which forms an aperture or window in which there are no prisms. If reference is had to Fig.- 1, it will be seen that the rays emitted by the source of light pass through this interval and give illumination from the horizontal up to the vertical line passing through the axis of the Searchlight.
- the interval E is dimensioned in such a manner that the pencil of light formed by the direct light emitted by the source is of horizontal amplitude equal to that of the pencil formed by the prisms and retains the same character in the whole vertical plane.
- the horizontal amplitude of the pencil given by the prisms being very small, the interval E is very small and, consequently, the small quantity of prisms removed from the panel only inapprc-ciably diminishes the intensity of the beam or pencil.
- the total beam obtained stretches therefore in a vertical plane from the horizon to the vertical passing through the axis of the searchlight, and this without interruption of continuity.
- the shaded zone included in the angle a corresponds to the intensity of the beam of light given out by the optical panel 1.
- the shaded zone included in the angle (5 corresponds to the intensity of the beam of light emitted directly by the source.
- Figs. 1 and 2 gives a simple flash. It is obvious that it would be posslble to construct searchlights having a plurality of regular panels or grouped around the source of light and thus to have either simple flashes or groups of flashes.
- a searchlight composed of reflectors alone or of reflectors and lenses, as shown in Fig. 3.
- a window which allows the light emitted by the source placed at the focus to escape directly, as in the device shown in Figs. 1 and .2.
- a signal light for use in aerial navigation comprising in combination a source of light, an optical system for projecting the beam from said source, said optical system having a narrow central aperture extending from a horizontal plane passing through the light source to the zenith.
- a signal light for use in aerial navigaments said standard having an aperture de-- void of optical elements extending from the horizon to the zenith.
- a signal light for use in aerial naviga tion comprising in combination a source of l ght, means for pro ect1ng the beam from said source substantially horizontally, a central narrow window being provided extending from the horizon-to the zenith for the passage of a portion of the light emitted by I said source.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Illuminated Signs And Luminous Advertising (AREA)
Description
H. L. M. J. BENARD.
AERIAL SIGNAL LIGHT.
APPLICATION FILED MAY 23. 919.
Patented July 12, 1921.
3 SHEETS-SHEET I.
' I In'wnEz! Ebnrz' Z. (M Jfi H. L. M. I. BENARD.
AERIAL SIGNAL LIGHT. v APPLICATION FILED MAY 23, 1919.
3 SHEETS SHEET 2- Fig. 2
' fnzwizir E6077; LMJjenard.
(9 anuumv I 41212 31 12631 Patented July 12, 1921.
3 SHEETS-SHEET 3- UNITED STATES HENRI LUG-LIEN MARIE JOSEPH BENARD, OF PARIS, FRANCE.
AERIAL SIGNAL-LIGHT.
Specification of Letters Patent. Patented July 12, 1921,
Application filed May 23, 1919. Serial No. 299,104.
T 0 all whom it may concern:
Be it known that I, HENRI LUGLIEN MARIE JosnrH Biiimmi, a citizen of the Republic of should be able to illuminate in a continuous manner, from the horizon to the zenith of the search-light. It is notnecessary that the intensity of the beam shall be equal in all parts of the vertical plane. Rationally speaking the beam of light should have its maximum intensity in the horizontal direction and this intensity should gradually decrease from the horizon to a point above the Searchlight in which latter region it need only have suiiicient intensity to enable the light to be visible at the greatest altitude which can be obtained by aircraft. As this altitude does not, in practice, exceed 4000 meters a very low intensity is suflicient for the light to be visible, the more so since at high elevations visibility is very good owing to the purity of the air.
The searchlight forming-the subject of this invention complies in all respects with the above conditions.
In principle the invention is characterized by the provision, in connection with a searchlight, of an aperture or window by means of which it is possible to illuminate from the horizon to the zenith of the Searchlight in a continuous manner and with a single source of light.
In the accompanying drawing, Figure 1 is a vertical section of a sea-rchlight constructed according to the invention. Fig. 2 isa front view of the optical panel ofthe searchlight. Fig. 3 shows a modification and Fig. 4 is a curve showing the ranges of the beam of lightof-the Searchlight.
Referring to'Fig. l, the Searchlight-consists essentially of an optical panel 1, composed of dioptric and catadioptric' elements. 2 designates a source of light, in this case anincandescent mantle, but any other source of light could be employed. table 3 supporting the optical system carries a crown wheel 4 meshing with the pinion 5 of a motor.
The prismatic elements are arranged so as to concentrate the luminous rays emitted by the source of light 2 into a very intense beam limited, on the one hand, by the line AB which is horizontal, and on the other hand by the line CD, which forms withtthe orizontal a certain angle a which is determined by practical considerations.
The light source is at the focus of the optical panel 1, and in the center of the portion of the panel situated above the horizontal plane PF passing through the light source, i ig. 2, the prisms are supported by a double standard M having an interval or 'gap E which forms an aperture or window in which there are no prisms. If reference is had to Fig.- 1, it will be seen that the rays emitted by the source of light pass through this interval and give illumination from the horizontal up to the vertical line passing through the axis of the Searchlight.
The interval E is dimensioned in such a manner that the pencil of light formed by the direct light emitted by the source is of horizontal amplitude equal to that of the pencil formed by the prisms and retains the same character in the whole vertical plane.
It should be noted that the horizontal amplitude of the pencil given by the prisms being very small, the interval E is very small and, consequently, the small quantity of prisms removed from the panel only inapprc-ciably diminishes the intensity of the beam or pencil.
The total beam obtained stretches therefore in a vertical plane from the horizon to the vertical passing through the axis of the searchlight, and this without interruption of continuity.
If the curves of the ranges of the beam were traced, one would obtain, for the whole beam, the curve represented in Fig. 4 in which 2 represents the searchlight. The shaded zone included in the angle a corresponds to the intensity of the beam of light given out by the optical panel 1. The shaded zone included in the angle (5 corresponds to the intensity of the beam of light emitted directly by the source.
It will therefore be seen that, taking by way of example an altitude of 4000 meters to which an aeroplane can rise, this altitude being indicated by athe lowest point of the beam, the aviator will always be within the beam of light, subject of course to the condition that he is not situated at a distance from the Searchlight which is superior to the horizontal range of this latter.
The apparatus shown in Figs. 1 and 2 gives a simple flash. It is obvious that it would be posslble to construct searchlights having a plurality of regular panels or grouped around the source of light and thus to have either simple flashes or groups of flashes. i
It would also be possible to construct a searchlight composed of reflectors alone or of reflectors and lenses, as shown in Fig. 3. In the upper portion of each reflector A and in the upper half of each lens L is formed a window which allows the light emitted by the source placed at the focus to escape directly, as in the device shown in Figs. 1 and .2.
Claims: 5
1. A signal light for use in aerial navigation, comprising in combination a source of light, an optical system for projecting the beam from said source, said optical system having a narrow central aperture extending from a horizontal plane passing through the light source to the zenith.
2. A signal light for use in aerial navigaments, said standard having an aperture de-- void of optical elements extending from the horizon to the zenith.
4. A signal light for use in aerial naviga tion comprising in combination a source of l ght, means for pro ect1ng the beam from said source substantially horizontally, a central narrow window being provided extending from the horizon-to the zenith for the passage of a portion of the light emitted by I said source.
HENRI LUGLIENMARIE JOSEPH BENARD
Publications (1)
Publication Number | Publication Date |
---|---|
US1384659A true US1384659A (en) | 1921-07-12 |
Family
ID=3399281
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US1384659D Expired - Lifetime US1384659A (en) | ii ii i |
Country Status (1)
Country | Link |
---|---|
US (1) | US1384659A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2586375A (en) * | 1947-07-31 | 1952-02-19 | Westinghouse Electric Corp | Rotating beacon having duplicate lamp systems one of which is automatically energized upon failure of the other |
US2989727A (en) * | 1955-11-10 | 1961-06-20 | Edgerton Germeschausen & Grier | Illumination landing method and system |
US20030193807A1 (en) * | 2002-04-16 | 2003-10-16 | Alexander Rizkin | LED-based elevated omnidirectional airfield light |
US6679621B2 (en) * | 2002-06-24 | 2004-01-20 | Lumileds Lighting U.S., Llc | Side emitting LED and lens |
US20080061310A1 (en) * | 2006-09-07 | 2008-03-13 | Hong Kong Applied Science and Technology Research Institute Company Limited | Light emitting diode device, and manufacture and use thereof |
US20110148270A1 (en) * | 2009-12-21 | 2011-06-23 | Malek Bhairi | Spherical light output LED lens and heat sink stem system |
US20120294014A1 (en) * | 2004-10-28 | 2012-11-22 | Harwood Ronald P | Housing for intelligent lights |
-
0
- US US1384659D patent/US1384659A/en not_active Expired - Lifetime
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2586375A (en) * | 1947-07-31 | 1952-02-19 | Westinghouse Electric Corp | Rotating beacon having duplicate lamp systems one of which is automatically energized upon failure of the other |
US2989727A (en) * | 1955-11-10 | 1961-06-20 | Edgerton Germeschausen & Grier | Illumination landing method and system |
US20030193807A1 (en) * | 2002-04-16 | 2003-10-16 | Alexander Rizkin | LED-based elevated omnidirectional airfield light |
US6932496B2 (en) * | 2002-04-16 | 2005-08-23 | Farlight Llc | LED-based elevated omnidirectional airfield light |
US6679621B2 (en) * | 2002-06-24 | 2004-01-20 | Lumileds Lighting U.S., Llc | Side emitting LED and lens |
US20120294014A1 (en) * | 2004-10-28 | 2012-11-22 | Harwood Ronald P | Housing for intelligent lights |
US8960967B2 (en) * | 2004-10-28 | 2015-02-24 | Ronald P. Harwood | Housing for intelligent lights |
US20080061310A1 (en) * | 2006-09-07 | 2008-03-13 | Hong Kong Applied Science and Technology Research Institute Company Limited | Light emitting diode device, and manufacture and use thereof |
US7800122B2 (en) | 2006-09-07 | 2010-09-21 | Hong Kong Applied Science And Technology Research Institute Co., Ltd. | Light emitting diode device, and manufacture and use thereof |
US20110148270A1 (en) * | 2009-12-21 | 2011-06-23 | Malek Bhairi | Spherical light output LED lens and heat sink stem system |
US8330342B2 (en) | 2009-12-21 | 2012-12-11 | Malek Bhairi | Spherical light output LED lens and heat sink stem system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1384659A (en) | ii ii i | |
US2338901A (en) | Vehicle lamp | |
US1734834A (en) | Light projector | |
US2481054A (en) | Light projector | |
US1357034A (en) | Electric-light fixture | |
US1337880A (en) | benard | |
US2313838A (en) | Mirror illumination | |
US1598106A (en) | Automobile headlight | |
US1413379A (en) | Aerial sickktal light | |
US2147679A (en) | Illuminating system | |
US2605384A (en) | Aircraft position lamp for projecting a full circle high intensity light spread | |
US3387124A (en) | Illuminating floodlight | |
US1039476A (en) | Aerial illuminating mechanism. | |
US1618055A (en) | Device for artificial illumination | |
US1955602A (en) | Light projector | |
US2588154A (en) | High-intensity lighting unit | |
US2114232A (en) | Searchlight | |
US1955603A (en) | Light projector | |
US2360768A (en) | Gun sight | |
US1817827A (en) | Lighting plant for air-port landing places | |
US1682387A (en) | Headlight | |
US1389180A (en) | Illumination-light | |
US288242A (en) | Lbb kelly | |
US1815831A (en) | Light projector | |
US1594742A (en) | Lamp |