Aircraft and exterior speaker systems for aircraft

Patent metadata

Field	Value
Publication number	US-9834320-B2
Application number	US-201514697895-A
Country	US
Kind code	B2
Filing date	Apr 28, 2015
Priority date	Apr 28, 2015
Publication date	Dec 5, 2017
Grant date	Dec 5, 2017

Abstract

Aircraft, aircraft exterior speaker systems, and methods of projecting sound waves from an exterior of an aircraft are provided. An aircraft includes an outer skin membrane, a vibration actuator, and a controller. The outer skin membrane has an exterior surface that defines an exterior boundary of the aircraft. The vibration actuator is coupled for common vibration with the outer skin membrane. The controller is operatively coupled with the vibration actuator and is configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface. The controller is further configured to transmit the command to the vibration actuator. The vibration actuator is configured to vibrate in response to receiving the command.

First claim

What is claimed is:

1. An aircraft, comprising:
an outer skin membrane having an exterior surface that defines an exterior boundary of the aircraft;
a wing having a wingtip;
a vibration actuator coupled for common vibration with the outer skin membrane; and
a controller operatively coupled with the vibration actuator and configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface and further configured to transmit the command to the vibration actuator, the vibration actuator being configured to vibrate in response to receiving the command, wherein the controller is further configured to generate the command based on proximity of the wingtip to an object for providing a tug driver with towing warnings.

2. The aircraft of claim 1 , wherein the outer skin membrane forms at least part of an engine cowl, a wing-to-body fairing, a horizontal stabilizer, a wing of the aircraft, or combinations thereof.

3. The aircraft of claim 1 , wherein the outer skin membrane has an interior surface, and wherein the vibration actuator is fastened to the interior surface of the outer skin membrane.

4. The aircraft of claim 1 , wherein the vibration actuator is an electromagnetic driver or a piezo electric actuator.

5. The aircraft of claim 1 , wherein the controller is further configured to generate the commands based on maintenance instructions to be conveyed to ground crew during maintenance operations.

6. The aircraft of claim 1 , wherein the vibration actuator is coupled to the outer skin membrane at an engine cowling, and wherein the controller is further configured to generate the commands based on active noise cancelation of noise generated by a jet engine of the aircraft.

7. An aircraft, comprising:
an outer skin membrane having an exterior surface that defines an exterior boundary of the aircraft, wherein the outer skin membrane is a composite material formed from a honeycomb structure;
a vibration actuator coupled for common vibration with the outer skin membrane, wherein the vibration actuator is embedded in a cell or cells of the honeycomb structure; and
a controller operatively coupled with the vibration actuator and configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface and further configured to transmit the command to the vibration actuator, the vibration actuator being configured to vibrate in response to receiving the command.

8. An aircraft, comprising:
an outer skin membrane having an exterior surface that defines an exterior boundary of the aircraft;
a vibration actuator coupled for common vibration with the outer skin membrane; and
a controller operatively coupled with the vibration actuator and configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface and further configured to transmit the command to the vibration actuator, the vibration actuator being configured to vibrate in response to receiving the command, wherein the controller comprises a component of a security system, and wherein the controller is further configured to generate the command based on a threat detected by the security system.

9. An aircraft, comprising:
an outer skin membrane having an exterior surface that defines an exterior boundary of the aircraft;
a vibration actuator coupled for common vibration with the outer skin membrane;
a controller operatively coupled with the vibration actuator and configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface and further configured to transmit the command to the vibration actuator, the vibration actuator being configured to vibrate in response to receiving the command; and
a remote communication device operatively coupled with a remotely located device operated by a remotely located user, and
wherein the controller is further configured to generate the command based on input from the remote communication device to facilitate communication between the remotely located user and people located near the aircraft.

10. An aircraft, comprising:
an outer skin membrane having an exterior surface that defines an exterior boundary of the aircraft;
a vibration actuator coupled for common vibration with the outer skin membrane; and
a controller operatively coupled with the vibration actuator and configured to generate a command for the vibration actuator based on audible content to be projected from the exterior surface and further configured to transmit the command to the vibration actuator, the vibration actuator being configured to vibrate in response to receiving the command, wherein the controller is further configured as a cabin management system that detects a power state of devices and systems on the aircraft, and wherein the controller is further configured to generate the commands to announce which of the devices and systems are in an “on” power state in response to detecting an occupant exiting the aircraft.

11. The aircraft of claim 10 , further comprising a pilot headset microphone operatively coupled with the controller, and wherein the controller is further configured to receive signals from the pilot headset microphone and to generate the command based on the signals received from the pilot headset microphone.

Assignees

• Gulfstream Aerospace Corp

Inventors

• Lucas Michael
• Brinley Michael
• Lynch Kristopher

Classifications

• B64D47/02 Primary

  Arrangements or adaptations of signal or lighting devices · CPC title

• B64D2045/0095

  Devices specially adapted to avoid bird strike · CPC title

• B64D45/00

  Aircraft indicators or protectors not otherwise provided for · CPC title

• G10K2210/1281

  Aircraft, e.g. spacecraft, airplane or helicopter · CPC title

• H04R7/045

  using the distributed mode principle, i.e. whereby the acoustic radiation is emanated from uniformly distributed free bending wave vibration induced in a stiff panel and not from pistonic motion · CPC title