HYBRID HEADLIGHT FOR AIRCRAFT

Abstract

This beam shaper for an aircraft headlight comprises a light input surface (3) and a light output surface (6), the output surface comprises prism-shaped areas so as to deflect a light beam transmitted between the light input surface and output surface by guiding the beam in two directions (D1, D2) which are oblique relative to an optical axis (A) of the beam shaper.

Claims

1. A beam shaper for an aircraft headlight, comprising a light input surface (3) and a light output surface (6), characterized in that the output surface comprises prism-shaped areas so as to deflect a light beam transmitted between the light input surface and output surface by guiding the beam in two directions (D1, D2) which are oblique relative to an optical axis (A) of the beam shaper.

2. The beam shaper of claim 1, wherein the output surface comprises a set of prisms (9) with triangular bases, extending in a parallel way and forming internal surfaces (10, 11) for reflection of the light beams.

3. The beam shaper of claim 2, wherein each of the prisms comprises two prismatic faces delimiting between them a beam deflection angle of between 45° and 55°, or preferably equal to 52°.

4. The beam shaper of claim 2, wherein the prisms (9) are separated by a distance of between 2 and 10 mm, preferably 5 mm.

5. The beam shaper of claim 1, comprising a body (2) having three lobes for shaping light beams emitted from three respective light sources, these lobes having a common output surface (6).

6. The beam shaper of claim 5, wherein the body comprises a set of fixing and centring stems (4, 5) extending from the input surface and a set of housings (7) for receiving a light-emitting diode.

7. An aircraft headlight comprising a set of light sources having light-emitting diodes and a set of beam shapers for shaping the light beam emitted by the light sources, characterized in that said set of beam shapers comprises beam shapers (1) according to claim 1.

8. The aircraft headlight of claim 7, comprising a first set of beam shapers (C2) delivering parallel beams of shaped light at their output and a second set of beam shapers (C1) for orientating the light, the first and second sets of beam shapers being mounted in respective areas of the headlight and being activated on the basis of flight and/or taxiing phases of the aircraft.

9. The aircraft headlight of claim 8, further comprising an outer lens (13) having a striated area (14), extending so as to face the orientating beam shapers and serving to spread the RTO beam, on the light output surface side.

Description

DESCRIPTION OF THE DRAWINGS

[0023] Other objects, characteristics and advantages of the invention will be apparent from a perusal of the following description, provided solely by way of non-limiting example with reference to the attached drawings, in which:

[0024] FIGS. 1 and 2 are, respectively, perspective views and top views of a beam shaper of an aircraft headlight according to the invention;

[0025] FIGS. 3 and 4 are side views of the beam shaper of FIGS. 2 and 3 in two different orientations;

[0026] FIGS. 5a and 5b, on the one hand, and FIGS. 6a and 6b, on the other hand, illustrate the principle of forming an RTO beam, and show the spreading of the beam in an oblique direction orientated towards the left and the right respectively;

[0027] FIG. 7 is a perspective view of a headlight having a beam shaper according to the invention;

[0028] FIG. 8 shows an outer lens mounted to face the light output surface of the beam shapers; and

[0029] FIG. 9 shows the light beams obtained by means of a headlight according to FIG. 7.

DETAILED DESCRIPTION

[0030] Reference will be made in the first place to FIGS. 1 to 4, which show the general architecture of a beam shaper according to the invention, designated by the general reference numeral 1.

[0031] This beam shaper is designed to be mounted in a headlight for external illumination of an aircraft, to provide the runway illumination functions of the taxi and runway turn-off type.

[0032] As may be seen, the beam shaper in this case has a structure with three lobes, L1, L2, L3, which respectively shape light beams emitted from light-emitting diodes (not shown).

[0033] The beam shaper 1 has a body 2 made in one piece by moulding from a plastic material, advantageously polycarbonate, and has a rear face 3 by means of which the beam shaper is mounted on a circuit bearing LEDs, using fixing and centring stems 4 and 5, and an opposed front face 6 delimiting a common light output surface for the set of lobes L1, L2 and L3.

[0034] As may be seen, the rear face 3 of each lobe L1, L2 and L3 has a housing 7 in which a light-emitting diode is housed. The peripheral surface and the base surface of the housing thus form a surface for the input of light into the beam shaper which shapes the light beams delivered by the diodes, and which transmits the light, in the form of parallel beams of shaped light, to the output surface of the beam shaper formed by the front face 6.

[0035] As may be seen, the front face 6 of the beam shaper has a set of parallel striations such as those marked 8, thereby forming a set of prisms 9 with triangular bases which extend in a direction of the beam shaper perpendicular to a direction of spreading of a beam.

[0036] Each prism 9 has two faces 10 and 11, which form between them a prismatic angle selected on the basis of the deflection or orientation of the beam to be produced.

[0037] In this respect, the prismatic faces 10 and 11 may be made to form an angle of between 45° and 55°. Preferably, a prismatic angle of 52° is used, so as to provide peak intensity in an oblique direction relative to the geometric axis of the beam shaper.

[0038] With reference to FIGS. 5a and 5b, on the one hand, and 6a and 6b, on the other hand, it may be seen that the prismatic faces 10 and 11 may be used to guide the beams in an oblique direction D relative to the geometric axis A of the beam shaper and to orientate the beam, respectively, to the left (FIGS. 5a and 5b) and to the right (FIGS. 6a and 6b).

[0039] It should be noted that, preferably, the prisms are spaced apart by a distance of between 2 and 10 mm. However, it has been found that a distance of 5 mm between the prisms provides sufficient spread and light output.

[0040] FIGS. 7 and 8 show a hybrid headlight 12 for aircraft which can provide the runway illumination functions of the taxi and RTO types.

[0041] As may be seen, this headlight comprises a set of light sources, each comprising a light-emitting diode associated with a beam shaper for shaping the beam emitted by the diode.

[0042] The hybrid headlight comprises beam shapers C1 for orientating the light, as described above with reference to FIGS. 1 to 4, and beam shapers C2 capable of shaping the light beam emitted from light-emitting diodes in the form of parallel beams, in respective areas of the headlight. An outer lens 13 comprising a striated area 14 is positioned facing the light output surfaces of the diodes in such a way that the striated area 14 is positioned facing the orientation beam shapers C1. The striated area 14 of this outer lens 13 serves to spread the two beams F2 and F3 of the RTO function.

[0043] As shown in FIG. 9, because of this arrangement, the headlight is capable of providing a first beam F1, using the diodes associated with the beam shapers C2, and spread beams F2 and F3, using the diodes associated with the spreading beam shapers C1.

[0044] It is possible to activate the different areas of the headlight simultaneously to obtain all three beams F1, F2 and F3, or to activate areas selectively to obtain a taxi illumination function (beam F1) or an RTO illumination function (beams F2 and F3).

[0045] A hybrid headlight according to the invention may, for example, be produced by using 6 triple light spreading beam shapers C1, each associated with 3 LEDs, and a set of 6 triple beam shapers C2, each of which is also associated with 3 light-emitting diodes, and may therefore comprise 36 light-emitting diodes, all within conventional overall dimensions.

[0046] In this respect, it should be noted that the size of the headlights is usually denoted by the PAR number, which denotes the diameter of the headlight in eighths of an inch. Thus the PAR 36 size corresponds to a diameter of 4½ inches, that is to say 114 mm, PAR 46 corresponds to a diameter of 5¾ inches, that is to say 5 145 mm, and PAR 64 corresponds to a diameter of 8 inches, that is to say 203 mm.

[0047] A hybrid headlight according to the invention may advantageously be produced in a PAR 64 size, and may therefore have overall dimensions corresponding to a conventional take-off light and thus replace, with reduced weight and overall dimensions, three headlights on the nose leg, namely one taxi light and two right and left runway turn-off lights.

[0048] While illustrative embodiments have been illustrated and described, it will be appreciated that various changes can be made therein without departing from the spirit and scope of the invention.