Illumination device for illuminating the vertical tail plane of an aircraft and aircraft with exterior illumination on its vertical tail plane

Abstract

A device for illuminating a vertical tail plane of an aircraft, comprising a matrix of LEDs or lasers, a laser diode with a diffractive optical element, an electronic board with a microcontroller, a power supply unit and a housing enclosing one or more of the matrix of LEDs, the laser diode, the electronic board and the power supply unit. The LEDs or lasers and the laser diode are individually and electronically controlled by the microcontroller, in such a way that the LEDs or lasers can be individually dimmed to create a dynamic illumination pattern on the side surfaces of the vertical tail plane. The illumination pattern is transmitted by the microcontroller. The laser diode with the diffractive optical element can create a fixed figure on the side surfaces of the vertical tail plane. An aircraft is provided with exterior illumination on its vertical tail plane, comprising such illumination devices.

Claims

1. An illumination device for illuminating a vertical tail plane of an aircraft, comprising: a matrix of LEDs or lasers, a laser diode with a diffractive optical element, an electronic board with a microcontroller, a power supply unit, and a housing that encloses one or more of the matrix of LEDs, the laser diode, the electronic board and the power supply unit, wherein the LEDs or lasers and the laser diode are individually and electronically controlled by the microcontroller, such that the LEDs or lasers can be individually dimmed to create a dynamic illumination pattern on opposing side surfaces of the vertical tail plane, the illumination pattern being transmitted by the microcontroller, and the laser diode with the diffractive optical element is configured to create a fixed figure on the opposing side surfaces of the vertical tail plane, wherein the opposing side surfaces of the vertical tail plane comprise areas with reflecting paint to which the illumination device points.

2. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the LEDs or lasers are of different colors to create dynamic color illumination patterns.

3. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the housing comprises an upper cover made of plastic or glass.

4. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein each LED or laser has an associated lens.

5. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein each LED or laser has an associated mirror.

6. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, additionally comprising a heat sink under the electronic board to dissipate heat.

7. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the laser diode is monochromatic.

8. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the diffractive optical element is customizable and interchangeable throughout a life of the product.

9. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the power supply unit is enclosed by the housing.

10. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the power supply unit is not enclosed by the housing.

11. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein the microcontroller is configured to cause each LED or laser to dim independently according to a predefined pattern sequenced in a loop.

12. An aircraft with exterior illumination on its vertical tail plane, comprising an aircraft fuselage, the vertical tail plane and two horizontal tail planes projecting from the aircraft fuselage, each horizontal tail plane comprising an illumination device according to claim 1 connected to an electrical supply system of the aircraft and oriented to provide light onto a respective closest side surface of the vertical tail plane, the vertical tail plane having a text or logo applied on it, wherein the side surfaces of the vertical tail plane comprise areas with a reflecting paint to which the illumination device on a horizontal tail plane points.

13. The aircraft with exterior illumination on its vertical tail plane, according to claim 12, wherein an illumination effect coupled with the reflecting paint highlights specific points or areas of the text or logo on the vertical tail plane more when illuminated.

14. The aircraft with exterior illumination on its vertical tail plane, according to claim 12, wherein the orientation of the illumination devices with respect to the vertical tail plane is adjustable.

15. The illumination device for illuminating the vertical tail plane of an aircraft, according to claim 1, wherein an illumination effect coupled with the reflecting paint highlights specific points or areas of the text or logo on the vertical tail plane more when illuminated.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) For a more complete understanding of the present invention, it will be described below in greater detail, making reference to the attached drawings, in which:

(2) FIG. 1 is a side view of a conventional aircraft, showing a horizontal tail plane and the vertical tail plane, and an illumination device projecting an illumination pattern on one side surface of the vertical tail plane.

(3) FIG. 2 is a sketch of illumination pattern examples on one side surface of the vertical tail plane.

(4) FIG. 3 is a representation of an illumination device of the invention including the laser diode.

(5) FIG. 4 is a schematic representation of the illumination device of FIG. 3.

(6) FIGS. 5 and 6 show arrangements for the matrix of LEDs of the illumination device of the invention.

(7) FIG. 7 is a proposed architecture for the electronic control.

(8) FIG. 8 shows the laser diode and a detail of the laser diode projection principle.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(9) FIG. 1 shows a side view of a conventional aircraft 2 comprising, among other elements, an aircraft fuselage 12 from which a vertical tail plane 9 and two horizontal tail planes 10 project.

(10) The vertical tail plane 9 has a text or logo painted on it.

(11) Each horizontal tail plane 10 comprises the illumination device 1 shown in FIGS. 3 and 4, connected to the electrical supply system of the aircraft 2 and oriented to provide light onto the respective closest side surface of the vertical tail plane 9. According to one embodiment, the orientation of the illumination devices 1 with respect to the vertical tail plane 9 is adjustable.

(12) FIG. 2 is simplified model of one side surface of a vertical tail plane 9, on which the different steps of an illuminated pattern provided by the LEDs 3 is shown as an example: on this FIG. 2 views of illumination for successive steps of time appear, showing the intensity of luminous flux.

(13) The illumination device 1 shown in FIGS. 3 and 4 comprises:

(14) a matrix of LEDs 3 each with its individual optical cluster,

(15) a laser diode 4 with its diffractive optical element 5,

(16) an electronic board 6 with a microcontroller 16,

(17) a power supply unit, and

(18) a housing 8 that encloses fully or partially the above-mentioned elements,

(19) such that the LEDs 3 and the laser diode 4 are individually and electronically controlled by the microcontroller 16, in such a way that the LEDs 3 can be individually dimmed to create a dynamic illumination pattern 14 on the side surfaces of the vertical tail plane 9, the illumination pattern 14 being transmitted by the microcontroller 16. The laser diode 4 combined with a diffractive optical element 5 allows the projection of a fixed figure on the vertical tail plane 9, that is superimposed on the logo. This illuminated form, text or image can be defined depending on the client need and in esthetic coherency with the logo of the Airline. The diffractive optical element 5 can be customizable and interchangeable throughout the life of the product.

(20) The LEDs 3 can be of different colors to create color illumination patterns 14.

(21) The laser diode 4 can be monochromatic and controlled by the power supply unit.

(22) The housing 8 can enclose the matrix of LEDs 3, the laser diode 4 and the electronic board 6 and may comprise an upper cover 11 made of plastic or glass (see FIG. 4). The electronic board 6 can also be in a separated part, along with the power supply unit, according to the installation constraints of the light.

(23) The power supply is not represented in the figures, and can be managed separately or in an integrated manner in the illuminating device 1, depending on installation constraints on the aircraft 2. The impact of the choice of integrated or separated power supply unit is on the dimensioning of the heat dissipation sinks 13.

(24) Each LED 3 may have an associated lens and/or mirror, as optical elements. FIG. 3 shows a proposal with mirrors in the matrix of LEDs 3.

(25) Each illumination device 1 additionally may comprise a heat sink 13 under the electronic board 6 to dissipate the heat in the illumination device 1 (see FIG. 4).

(26) The matrix of LEDs 3 can have many configurations, depending on the surface to be illuminated and on installation constraints. As non-limiting examples, matrixes of x*y LEDs 3 can be used. For instance, the matrix of LEDs 3 can be formed by 24 LEDs 3; it may be an arrangement formed by 4 columns and 6 rows (as shown in FIG. 6) or by 3 columns and 8 rows (as shown in FIG. 5), or other configurations are also possible. Other shapes (such as circular ones) are also possible.

(27) As previously indicated, the LEDs 3 are controlled electronically, each one separately, and their power is adapted in a dynamic way to create a waving illumination effect: while some LEDs 3 are illuminated to their maximum, others are dimmed within the matrix of LEDs 3; each LED 3 illuminating a part of the logo area on the vertical tail plane 9, which allows the creation of a pattern on the surface.

(28) The invention allows this dynamic illumination, not only in white light, but also in different colors, in order to have broader possibilities. This illumination effect can also be coupled with the application of a reflecting paint to highlight specific points or areas of the logo on the vertical tail plane 9 even more when illuminated.

(29) The embedded electronic board 6 uses a microcontroller 16 which transmits the wanted illumination pattern to each LED 3. The definition of the pattern is made through a format that is easily customizable, using a matrix in a txt file defining the expected values of illumination of each LED 3 for different steps, that is then interpreted by the software of the microcontroller 16 and repeated in a loop.

(30) This allows to provide a service to the airline companies, which can define the pattern that best suits them.

(31) FIG. 8 shows the laser diode, the diffractive optical element 5, a focusing lens 15, and a detail of the laser diode projection principle.

(32) It is also to be taken into account that lasers can be used instead of LEDs 3 in the illumination device 1 of the invention, thus having a matrix of lasers instead of a matrix of LEDs 3.

(33) Although the present invention has been fully described in connection with preferred embodiments, it is evident that modifications may be introduced within the scope thereof, not considering this as limited by these embodiments, but by the contents of the following claims.

(34) While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.