Aircraft lighting device having optical element magnetically coupled to LED circuit board
10989382 · 2021-04-27
Assignee
Inventors
- Anil Kumar Jha (Lippstadt, DE)
- Andre Hessling-von Heimendahl (Koblenz, DE)
- Elmar Schrewe (Anroechte, DE)
Cpc classification
F21V5/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21V17/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21W2107/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D47/04
PERFORMING OPERATIONS; TRANSPORTING
B64D2011/0053
PERFORMING OPERATIONS; TRANSPORTING
F21Y2115/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21V7/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/29
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/192
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/143
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/321
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D47/02
PERFORMING OPERATIONS; TRANSPORTING
F21W2106/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D11/00
PERFORMING OPERATIONS; TRANSPORTING
H05K2201/10121
ELECTRICITY
B60Q3/44
PERFORMING OPERATIONS; TRANSPORTING
F21S41/39
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/153
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D2203/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
F21V17/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D47/04
PERFORMING OPERATIONS; TRANSPORTING
F21S41/29
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H05K3/00
ELECTRICITY
B64D11/00
PERFORMING OPERATIONS; TRANSPORTING
F21S41/143
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B60Q3/44
PERFORMING OPERATIONS; TRANSPORTING
F21S41/19
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/39
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S41/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An aircraft lighting device includes a circuit board; an LED soldered to the circuit board; an optical element supported by the circuit board and positioned for re-directing at least part of the light emitted by the LED; a magnetic coupling between the circuit board and the optical element; and at least one surface mounted device included in the optical element, such surface mounted device including a pin soldered to the circuit board.
Claims
1. Lighting device, comprising: a circuit board; an LED, soldered to the circuit board; an optical element, supported by the circuit board and positioned for re-directing at least part of the light in operation emitted by the LED; and a magnetic coupling between the circuit board and the optical element, wherein the optical element comprises at least one surface mounted device pin, soldered to the circuit board.
2. The lighting device according to claim 1, wherein the optical element is one of a reflector or a lens.
3. The lighting device according to claim 1, wherein the magnetic coupling comprises one of: a permanent magnet at the optical element and a ferromagnetic element at the circuit board; a ferromagnetic element at the optical element and a permanent magnet at the circuit board; or a first permanent magnet at the optical element and a second permanent magnet at the circuit board.
4. An aircraft comprising at least one lighting device in accordance with claim 1.
5. The lighting device according to claim 1, wherein the lighting device is an interior aircraft light.
6. The lighting device according to claim 5, wherein the interior aircraft light is a personal reading light.
7. The lighting device according to claim 1, wherein the lighting device is an exterior aircraft light.
8. The lighting device according to claim 7, wherein the exterior aircraft light is an aircraft headlight.
9. The lighting device according to claim 7, wherein the exterior aircraft light is one of a helicopter search light, an aircraft taxi light, an aircraft take-off light, an aircraft landing light, an aircraft runway turn-off light, and a multi-purpose aircraft headlight having at least two functionalities of an aircraft taxi light, an aircraft take-off light, an aircraft landing light, and an aircraft runway turn-off light.
10. Lighting device, comprising: a circuit board; an LED, soldered to the circuit board; an optical element, supported by the circuit board and positioned for re-directing at least part of the light in operation emitted by the LED; and a magnetic coupling between the circuit board and the optical element, wherein the lighting device has one of the following features: the lighting device further comprises at least one positioning LED, soldered to the circuit board and extending from the circuit board, wherein the optical element has at least one recess, with each of the at least one positioning LED being arranged in an associated one of the at least one recess; or the optical element comprises at least one protrusion and the circuit board comprises at least one drilled hole, with each of the at least one protrusion being arranged in an associated one of the at least one drilled hole; or the optical element comprises a self-aligning hinge mechanism arranged around the LED.
11. The lighting device according to claim 10, wherein the optical element is one of a reflector or a lens.
12. The lighting device according to claim 10, wherein the magnetic coupling comprises one of: a permanent magnet at the optical element and a ferromagnetic element at the circuit board; a ferromagnetic element at the optical element and a permanent magnet at the circuit board; or a first permanent magnet at the optical element and a second permanent magnet at the circuit board.
13. An aircraft comprising at least one lighting device in accordance with claim 10.
14. The lighting device according to claim 10, wherein the lighting device is an interior aircraft light.
15. The lighting device according to claim 14, wherein the interior aircraft light is a personal reading light.
16. The lighting device according to claim 10, wherein the lighting device is an exterior aircraft light.
17. The lighting device according to claim 16, wherein the exterior aircraft light is an aircraft headlight.
18. The lighting device according to claim 16, wherein the exterior aircraft light is one of a helicopter search light, an aircraft taxi light, an aircraft take-off light, an aircraft landing light, an aircraft runway turn-off light, and a multi-purpose aircraft headlight having at least two functionalities of an aircraft taxi light, an aircraft take-off light, an aircraft landing light, and an aircraft runway turn-off light.
19. A method for manufacturing a lighting device, comprising: soldering an LED to a circuit board; positioning an optical element on the circuit board for re-directing at least part of the light in operation emitted by the LED; and attaching the optical element to the circuit board via a magnetic coupling between the optical element and the circuit board, wherein the positioning of the optical element on the circuit board comprises one of: soldering the optical element to the circuit board via at least one surface mounted device pin; or soldering at least one positioning LED to the circuit board, and inserting the at least one positioning LED into at least one corresponding recess in the optical element; or drilling at least one hole into the circuit board, with the drilling of the at least one hole into the circuit board in particular taking place after the soldering of the LED to the circuit board, and inserting at least one protrusion of the optical element into the at least one hole in the circuit board; or aligning the optical element with the LED via a hinge mechanism in the optical element.
Description
BRIEF DESCRIPTION OF THE FIGURES
(1) Further exemplary embodiments of the invention will be described with respect to the accompanying drawings, wherein:
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
DETAILED DESCRIPTION
(11)
(12) The lighting device 2 of
(13) The lighting device 2 further comprises three magnetic couplings 10 between the reflector 8 and the circuit board 4. In the top view of
(14) The reflector 8 comprises two surface mounted device pins (SMD pins) 20, which are soldered to the circuit board 4. In the top view of
(15) As stated above,
(16) Each of the magnetic couplings 10 comprises a first permanent magnet 12 and a second permanent magnet 14. The first permanent magnets 12 are provided at the reflector 8. In particular, the first permanent magnets 12 are provided in corresponding recesses 13 of the reflector 8. The reflector 8 may have cylindrical protrusions on its lower side, i.e. on the side opposite the reflective surface, with channels within those cylindrical protrusions forming the recesses 13 for receiving the first permanent magnets 12. In the exemplary embodiment of
(17) The second permanent magnets 14 are provided at the circuit board 4. In particular, the second permanent magnets 14 are press-fit into corresponding holes in the circuit board 4. In the exemplary embodiment of
(18) The first permanent magnets 12 and the second permanent magnets 14 are of opposite polarities. In this way, an attractive force exists between the first permanent magnet 12 and the second permanent 14 of each magnetic coupling scene. The attractive forces of the magnetic couplings 10 combine to provide a firm attachment between the reflector 8 and the circuit board 4. In the exemplary embodiment of
(19) In the exemplary embodiment of
(20)
(21) As stated above, the reflector 8 comprises two SMD pins 20. The SMD pins 20 are provided on the side of the reflector 8 facing the circuit board 4. The SMD pins 20 are soldered to the circuit board 4. The SMD pins 20 provide for a fixed positioning of the reflector 8 with respect to the circuit board 4. While the magnetic couplings 10, as described above, prevent the reflector 8 from disengaging from the circuit board 4 in the z-direction of the circuit board 4. The SMD pins 20 prevent for a shifting of the reflector 8 along the circuit board 4. The position of the reflector 8 with respect to the circuit board 4 is fixed, which in turn also fixes the relative position between the LED 6 and the reflector 8.
(22) During manufacture of the lighting device 2, the LED 6 is soldered to the circuit board 4 and the SMD pins 20 are soldered to the circuit board 4. In particular, the LED 6 and the SMD pins 20 may be soldered to the circuit board 4 in the same manufacturing step. In this way, the LED 6 and the SMD pins 20 may swim or shift in the same or substantially the same manner, while the solder is still liquid. This in turn will ensure that a very accurate relative positioning between the reflector 8 and the LED 6 is maintained.
(23)
(24) The lighting device 202 of
(25) The positioning between the reflector 208 and the circuit board 204 of the lighting device 202 of
(26) The reflector 208 has two recesses 24 for receiving the two positioning LEDs 22. The two recesses 24 are channels within cylindrical protrusions extending from the side of the reflector 208 facing the circuit board 204. The lateral extensions of the recesses 24 substantially correspond to the lateral extensions of the positioning LEDs 22. In the exemplary embodiment of
(27) During manufacture of the lighting device 202, the LED 6 and the positioning LEDs 22 are soldered to the circuit board 204. In particular, the LED 6 and the positioning LEDs 22 may be soldered to the circuit board 204 in the same manufacturing step. In this way, the positions of the LED 6 and of the positioning LEDs 22 may be affected in the same or substantially the same manner, when swimming or shifting while the solder is still liquid. Accordingly, a very accurate relative positioning between the LED 6 and the reflector 208 may be achieved.
(28)
(29) The lighting device 302 of
(30) The positioning of the reflector 308 with respect to the circuit board 4 is different in the lighting device 302 of
(31) The protrusions 26 are provided around a lower end of the reflector 308, i.e. around a region of the reflector 308 where the reflective surface comes close to the circuit board 304. However, it is pointed that the protrusions 26 may also be arranged at different portions of the reflector 8. In the assembled state, the protrusions 26 are received by the corresponding drilled holes 28 in the circuit board 304. In this way, the positioning between the reflector 308 and the circuit board 304 is fixed. This in turn means that the relative positioning between the reflector 308 and the LED 6 is also fixed.
(32) During manufacture, the LED 6 may be soldered to the circuit board 304 in a particular manufacturing step. In a subsequent manufacturing step, the drilled holes 28 may be drilled into the circuit board 4, taking the position of the LED 6 as a reference. In a further manufacturing step, the reflector 308 may be positioned with respect to the circuit board 304 by inserting the protrusions 26 into the drilled holes 28. In this way, an accurate relative positioning between the LED 6 and the reflector 308 may be achieved. With the drilled holes 28 being created after the soldering of the LED 6 to the circuit board 304, the relative positioning between the LED 6 and the reflector 308 may be made independent from the LED 6 swimming or shifting on the circuit board 304 during soldering. At the same time as inserting the protrusions 26 into the drilled holes 28, the magnetic attachment between the reflector 308 and the circuit board 304 via the magnetic couplings 10 is effected.
(33)
(34) The lighting device 402 of
(35) The positioning between the reflector 208 and the circuit board of the lighting device 202 of
(36) During the manufacture of the lighting device 402, the reflector 408 is pressed down onto the circuit board. During this procedure, the LED 6 is positioned in the opening between the four hinges 30. The engagement between the reflector 408 and the circuit board pushes the hinges 30 upwards. As a consequence, the hinges 30 tighten around the LED 6 and, thus, self-align the reflector 408 with the LED 6. The closed position of the hinges 30 with respect to the LED 6 is illustrated in the top view of
(37) As described above,
(38)
(39) As stated above, a magnetic coupling 510 is provided between the lens 9 and the circuit board 4. In particular, a first permanent magnet 12 is press-fit into the lens 9, and a second permanent magnet 14 is press-fit into the circuit board 514. Further, the lens 9 comprises a protrusion 526, which is received by a drilled hole 28 in the circuit board 514. The lens 9 is firmly attached and accurately positioned with respect to the circuit board 4 and, thus, with respect to the LED 6. Multiple magnetic couplings 10 and multiple protrusions/drilled holes may be present.
(40)
(41)
(42) The lighting device 602 of
(43) In the exemplary embodiment of
(44) The light outputs of the structural units may re-inforce each other. As a result, the lighting device 2 has a very bright light output towards the observer in the viewing direction of
(45)
(46)
(47)
(48) On the side depicted to the left in
(49) Six electrical switches 130 are provided to the right side of the personal reading lights 902, a pair of two switches 130 next to each of the personal reading lights 902. One of the switches 130 of each pair may be configured for switching the adjacent personal reading light 902, while the second switch of each pair may be configured for triggering a signal for calling cabin service personnel.
(50) A row of three adjacent gaspers 122 arranged in the lateral direction is provided next to the switches 130. The overhead passenger service unit 120 further comprises a loudspeaker 126, a display panel 128, and a covered cavity 124 for housing at least one oxygen mask (not shown).
(51) While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.