Ejection device for a flight data recorder

Patent metadata

Field	Value
Publication number	US-9387937-B2
Application number	US-201113805270-A
Country	US
Kind code	B2
Filing date	Jun 16, 2011
Priority date	Jun 19, 2010
Publication date	Jul 12, 2016
Grant date	Jul 12, 2016

Abstract

An ejection device for a flight data recorder includes an ejection spindle, which can be detachably connected to the flight data recorder by means of a bayonet coupling. The bayonet coupling can be released by means of force application by the ejection spindle, a disengaging device, which has a compression-resistant housing and into which the ejection spindle can be screwed, and a gas pressure generator, a valve, which is located within the disengaging device and which permits a flow connection between the outlet of the gas pressure generator and the ejection spindle when the ejection spindle is screwed in and which disables the flow connection between the outlet of the gas pressure generator and the ejection spindle when the ejection spindle is unscrewed.

First claim

The invention claimed is:

1. An ejection device for a flight data recorder, the ejection device comprising:
an ejection spindle comprising an ejection rod, the ejection rod movably received within a central cavity of the ejection spindle, the ejection rod having a recess in an outer surface thereof and a movable locking element engaging the outer surface and movable between a locking position and an unlocking position, wherein in the unlocking position the movable locking element is received within the recess;
a bayonet connection, wherein the ejection spindle is configured to be releasably connected to the flight data recorder via the bayonet connection through engagement of the bayonet connection with the movable locking element when the movable locking element is in the locking position, wherein the bayonet connection is configured to be released upon movement of the ejection rod such that the movable locking element moves into the recess of the ejection rod and thereby disengages from the bayonet fastening;
a disengagement device having a gas pressure generator and a pressure-resistant housing, wherein the ejection spindle is screwable into the disengagement device; and
a moveable valve arranged inside the disengagement device, the valve being configured to assume a first operating position when the ejection spindle is screwed into the disengagement device and to assume a second operating position when the ejection spindle is not screwed into the disengagement device, wherein the moveable valve is spring biased towards the second operating position,
wherein the first operating position permits a flow connection between an outlet of the gas pressure generator and the ejection spindle, and
wherein the second operating position prevents the flow connection between the outlet of the gas pressure generator and the ejection spindle;
wherein, when the valve is in the first operating position, the ejection rod of the ejection spindle is movable by gas pressure upon actuation of the gas pressure generator to move the locking element from the locked position and the unlocked position.

2. The ejection device as claimed in claim 1 , wherein the valve is configured to be prestressed by the ejection spindle being screwed into the disengagement device.

Assignees

• Grewe Reinhold
• Feierabend Stefan
• Airbus Defence & Space Gmbh

Inventors

• Grewe Reinhold
• Feierabend Stefan

Classifications

• B64D2045/0065

  Black boxes, devices automatically broadcasting distress signals · CPC title

• B64D25/20

  Releasing of crash-position indicators · CPC title

• Y10T403/592

  Ball detent · CPC title

• Y10T403/22

  with fluid pressure responsive component · CPC title

• Y10T403/7007

  Bayonet joint · CPC title