Aircraft with wireless provision of power

Patent metadata

Field	Value
Publication number	US-12132330-B2
Application number	US-202117912338-A
Country	US
Kind code	B2
Filing date	Jan 27, 2021
Priority date	Mar 18, 2020
Publication date	Oct 29, 2024
Grant date	Oct 29, 2024

Abstract

An aircraft has a first antenna arrangement, a payload and a processing unit. The first antenna arrangement is designed to wirelessly receive electromagnetic signals. The processing unit is coupled to the first antenna arrangement, on the one hand, and to the payload, on the other hand. The processing unit is designed to modulate an electromagnetic signal received by the first antenna arrangement and thereby to generate a first modulated signal and to forward it to the payload. The payload is designed to use the first modulated signal as working signal. A radiofrequency power signal on an uplink is thus remodulated into a payload working signal, such that the payload working signal is able to be used directly by the payload without rectification into a DC voltage.

First claim

The invention claimed is:

1. An aircraft comprising:
a first antenna arrangement configured to wirelessly receive electromagnetic signals;
a payload;
a processing unit coupled to the first antenna arrangement and to the payload;
wherein the processing unit is configured to modulate an electromagnetic signal received by the first antenna arrangement and thereby to generate a first modulated signal and to forward the first modulated signal to the payload;
wherein the payload is configured to use the first modulated signal as working signal,
wherein the electromagnetic signal is configured to transmit power for the payload wirelessly from a remote station to the aircraft;
wherein the processing unit is configured to convert the electromagnetic signal into an AC signal without any conversion into a DC signal and without buffer storage of an energy of the electromagnetic signal in an energy storage unit; and
wherein the processing unit is configured to use the electromagnetic signal to directly make available a required radio frequency power for the payload and, following the modulation of the electromagnetic signal, to route the first modulated signal to the payload and use the first modulated signal as the working signal.

2. The aircraft as claimed in claim 1 ,
wherein the payload is a second antenna arrangement configured to use the first modulated signal as payload transmission signal; or
wherein the payload is a communication installation configured to use the first modulated signal as carrier signal of a wireless communication connection; or
wherein the payload is an intelligence installation configured to use the first modulated signal as transmitter signal; or
wherein the payload is a data processing unit configured to use the first modulated signal as voltage and current supply.

3. The aircraft as claimed in claim 1 ,
wherein the processing unit has a first modulator;
wherein the first modulator is configured to downmodulate the received electromagnetic signal to a lower frequency to generate the first modulated signal.

4. The aircraft as claimed in claim 3 ,
wherein the first modulator is configured to apply a coherent modulation to generate the first modulated signal.

5. The aircraft as claimed in claim 1 ,
wherein the processing unit is configured to convert a portion of the received electromagnetic signal into a DC signal and to use the DC signal as energy supply for components of the aircraft.

6. The aircraft as claimed in claim 1 ,
wherein the processing unit has a second modulator;
wherein the second modulator is configured to modulate an output signal from the payload to a higher or lower frequency and thereby to generate a second modulated signal.

7. The aircraft as claimed in claim 6 ,
wherein the processing unit has a data compressor configured to process the second modulated signal.

8. The aircraft as claimed in claim 6 , further comprising:
an emission unit and a reception unit;
wherein the emission unit is configured to send the working signal as payload transmission signal;
wherein the reception unit is configured to receive a payload reception signal;
wherein the processing unit is configured to transmit the payload reception signal to the first antenna arrangement to allow transmission to a remote station by way of the electromagnetic signal to be sent.

9. A system comprising an aircraft and a ground unit;
wherein the aircraft is an aircraft as claimed in claim 1 ;
wherein the ground unit is arranged outside the aircraft;
wherein the ground unit is configured to wirelessly transmit an electromagnetic signal to the aircraft via an uplink and to receive signals from the aircraft via a downlink.

10. The system as claimed in claim 9 ,
wherein the ground unit is arranged on the Earth's surface.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Daniel Christian

Classifications

• H02J2105/32

  for aircrafts · CPC title

• H02J50/502 Primary

  the energy repeater being integrated together with the emitter or the receiver · CPC title

• H02J50/20 Primary

  using microwaves or radio frequency waves · CPC title

• H04B5/79

  for data transfer in combination with power transfer · CPC title

• B64D2221/00

  Electric power distribution systems onboard aircraft · CPC title