PHARE POUR ATTERRISSEUR D'AERONEF
20230216182 · 2023-07-06
Inventors
Cpc classification
H01Q1/22
ELECTRICITY
H01Q9/0407
ELECTRICITY
B64D47/02
PERFORMING OPERATIONS; TRANSPORTING
H01Q1/42
ELECTRICITY
H01Q1/28
ELECTRICITY
International classification
H01Q1/28
ELECTRICITY
Abstract
A light for mounting on an aircraft is fitted with a light source, an antenna for establishing radio communication between the aircraft and a ramp agent, or airport equipment, or an airport vehicle, and connection means for connecting a signal cable for linking the antenna to radio communication means of the aircraft.
Claims
1. A method of providing an aircraft with radio communication means for communicating with ramp agents, or with airport equipment, or with an airport vehicle, the method comprising; replacing an existing light of the aircraft by a replacement light including an antenna for establishing radio communication between the aircraft and a ramp agent, or airport equipment, or an airport vehicle, together with connection means for connecting a signal cable to enable the antenna to be linked to radio communication means of the aircraft; and arranging a signal cable between the light and the radio communication means of the aircraft.
2. The method according to claim 1, wherein the replacement light comprises: a light source; a cover; and a protective glass closing the cover and cooperating with the cover to define a cavity containing the light source, wherein the antenna is arranged inside the cover in the cavity.
3. The method according to claim 1, wherein the antenna of the replacement light is a flat antenna.
4. The method according to claim 1, wherein the replacement light includes modulator/demodulator means connected directly to the antenna.
5. An aircraft, comprising: radio communication means for communicating between the aircraft and a ramp agent, or airport equipment, or an airport vehicle; a light including an antenna for establishing radio communication between the aircraft and a ramp agent, or airport equipment, or an airport vehicle, together with connection means for connecting a signal cable for linking the antenna to the radio communication means of the aircraft; and a signal cable arranged between the light and the radio communication means of the aircraft.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0009] [
[0010] [
[0011] [
[0012] [
DETAILED DESCRIPTION OF THE INVENTION
[0013] With reference to
[0014] As can be seen in
[0015] As can be seen in
[0016] The invention seeks to facilitate communication between the crew of the aircraft 1 and a ramp agent 100 by establishing radio communication.
[0017] For this purpose, and in accordance with the invention, an antenna, specifically a flat “patch” type antenna 9, is arranged in the light 3 by being placed inside the cover 6, on its inside face, and thus in the same cavity as the light source 8, and it is arranged to radiate and receive mainly towards the front of the aircraft through the protective glass 7. The antenna 9 is thus protected from the weather and from impacts. The light 3 includes a connector 11 for connecting the antenna 9 to the radio communication means of the aircraft by means of a signal cable 10 that comes down along the undercarriage, in parallel with the power cable 5 for the light source 8.
[0018] The antenna 9 serves to establish radio communication with a transceiver carried by the ramp agent 100 (e.g. by being included in a headset), thus enabling the agent to communicate with the crew on board the aircraft. By way of example, the radio communication may take place using freely available frequencies for short-range use of Wi-Fi, DECT, ..., type, or indeed using any other radio communication protocol. For this purpose, the signal cable 10 conveys an RF signal between the antenna 9 and the radio communication means of the aircraft. The signal cable 10 is preferably shielded in order to avoid any interfering radiation.
[0019] In a variant shown in
[0020] The invention is particularly adapted for retrofitting existing aircraft. Specifically, in order to provide radio connections between ground crew and the aircraft, or indeed data communication between the aircraft and airport equipment or an airport vehicle, it suffices to replace an existing light of the aircraft with a light of the invention that is attached to the same support as the existing light, and then to run a signal cable from the radio communication means of the aircraft to the light. This retrofit can be done without any structural modification to the fuselage or to the landing gear and it therefore does not require any structural re-certification. Advantageously, a light of the invention is provided with the same interfaces as existing lights.
[0021] The invention is not limited to the above description, but on the contrary covers any variant coming within the ambit defined by the claims. In particular, although above, the light source of the light is a bulb, the light source could be of any other kind, such as for example one or more light-emitting diodes (LEDs).
[0022] Although above, the invention is used to provide radio communication between the aircraft and a ramp agent, the invention could be used to provide data communication for airport operations between the aircraft and airport equipment or an airport vehicle.
[0023] Although above, the light of the invention is preferably arranged on the nose undercarriage of the aircraft, it could equally well be arranged on a different undercarriage, on the door of a well into which the undercarriage is retracted in flight, or indeed on the structure of the fuselage or of the wings.
[0024] Although above, the antenna is of the patch type, which can be incorporated very easily in a light, the antenna could be of any other type.
[0025] Although above, the antenna is incorporated in the cavity defined by the cover and the protective glass, the invention applies equally to other types of light without a protective glass and in which the light source is directly exposed to the weather.
[0026] Above, in order to facilitate understanding the invention, the signal cable 10 is shown as being physically separate from the power cable 5, with both cables extending along the undercarriage via separate paths; however, the signal cable 10 could naturally be combined with the power cable 5 in a common cable harness going down along the undercarriage, the signal cable 10 and the power cable 5 then possibly sharing a common connector for connection to the light of the invention.