Distress beacon integrated in the vertical tailplane of an aircraft

Patent metadata

Field	Value
Publication number	US-9958530-B2
Application number	US-201414534390-A
Country	US
Kind code	B2
Filing date	Nov 6, 2014
Priority date	Nov 12, 2013
Publication date	May 1, 2018
Grant date	May 1, 2018

Abstract

The vertical tailplane of the aircraft is equipped with a distress beacon. The floatability of the vertical tailplane is taken advantage of in order to keep the distress beacon on the surface of the water in the case of an accident caused by a forced landing on the sea.

First claim

The invention claimed is:

1. A vertical tailplane of an aircraft, comprising:
a distress beacon being generally cylindrical in shape with a generally circular cross-section and a generally cylindrical exterior side-surface,
a fixing device that is water-soluble, wherein said fixing device forms a clamping collar that engagees the generally cylindrical exterior side-surface of the distress beacon,
a housing for receiving the distress beacon and the fixing device within said housing, said housing is closed by a radome forming an aerodynamic surface transparent to the waves likely to the transmitted by the beacon,
said housing being hermetically sealed and maintained at a predefined internal pressure;
wherein the distress beacon comprises a battery and a heating unit provided for maintaining the battery at a temperature higher than a reference temperature;
wherein the radome forms a leading edge of the vertical tailplane.

2. The vertical tailplane as claimed in claim 1 , wherein the distress beacon comprises a float.

3. The vertical tailplane as claimed in claim 1 , wherein the internal pressure is higher than 1 bar.

4. The vertical tailplane as claimed in claim 1 , wherein said distress beacon is held in its housing by water-soluble fixing devices.

5. The vertical tailplane as claimed in claim 1 , wherein the distress beacon is arranged inside the radome in the leading edge of the vertical tailplane.

6. The vertical tailplane as claimed in any one of the preceding claims, wherein said radome is equipped with one or more privileged fracture zones.

7. An aircraft comprising a vertical tailplane, the tailplane comprising:
a distress beacon being generally cylindrical in shape with a generally circular cross-section and a generally cylindrical exterior side-surface,
a fixing device that is water-soluble, wherein said fixing device forms a clampling collar that engages the generally cylindrical exterior side-surface of the distress beacon,
a housing for receiving the distress beacon and the fixing device within said housing, said housing is closed by a radome forming an aerodynamic surface transparent to the waves likely to the transmitted by the beacon,
said housing being hermetically sealed and maintained at a predefined internal pressure;
wherein the distress beacon comprises a battery and a heating unit provided for maintaining the battery at a temperature higher than a reference temperature;
wherein the radome forms a leading edge of the vertical tailplane.

8. An aircraft comprising a vertical tailplane, the tailplane comprising:
a distress beacon being generally cylindrical in shape with a generally circular cross-section and a generally cylindrical exterior side-surface,
a fixing device that is water-soluble, wherein said fixing device forms a clamping collar that engages the generally cylindrical exterior side-surface of the distress beacon,
a housing for receiving the distress beacon and the fixing device within said housing, said housing is closed by a radome forming an aerodynamic surface transparent to the waves likely to the transmitted by the beacon,
said housing being hermetically sealed and maintained at a predefined internal pressure;
wherein the distress beacon comprises a battery and a heating unit provided for maintaining the battery at a temperature higher than a reference temperature;
wherein the radome forms a leading edge of the vertical tailplane;
wherein the radome is equipped with one or more privileged fracture zones such that a portion of the leading edge of the vertical tailplane is fracturably removable.

Assignees

• Airbus Operations Sas
• Airbus Operations Sas

Inventors

• Colin Michel

Classifications

• B64D25/20 Primary

  Releasing of crash-position indicators · CPC title

• G01S19/17

  Emergency applications · CPC title

• B64D2045/0065

  Black boxes, devices automatically broadcasting distress signals · CPC title

• G01S5/0231 Primary

  Emergency, distress or locator beacons · CPC title