This application is the U.S. national phase of International Application No. PCT/IB2007/053438 filed on Jul. 10, 2007, the entire contents of which are incorporated herein by reference.
The invention relates to the field of stowage box for breathing mask.
To ensure the safety of the passengers and crewmembers in case of a depressurization accident or the occurrence of smoke in the aircraft, aviation regulations require on board all airliners a safety oxygen supply circuit able to supply each passenger and crewmember with an oxygen flow rate function of the cabin altitude. Such oxygen is delivered to the crewmember or passenger, also known as end user, through a breathing mask.
After a depressurization accident or upon the occurrence of smoke in the aircraft, the crewmembers must don their protective mask upon their face as quickly as possible. Indeed, the lack of oxygen at high altitude (hypoxia) or the toxic fumes can alter the crewmembers' abilities to proceed with any emergency measures that will ensure the safety of the passengers and the aircraft.
A protective mask is generally stored in a box called a stowage box located next to the crewmember's position. Generally, the stowage box comprises a frame forming a receptacle for the mask, itself having an open face of rectangular shape for inserting and extracting the mask, and at least two doors closing the open face of the frame, at least in part. The mask is extracted through the face that is closed by two doors that retain and/or protect the mask, each opening and closing about a respective hinge, the two hinges of the doors operating about two parallel hinge axes. The box is installed on the right or left of the seat of the pilot, the open face being generally the top side of the box. The stowage box comprises a pneumatic assembly able to close the feed of breathing gas of the breathing mask when the breathing mask is installed in the stowage box. The objective of the pneumatic assembly is to reduce or suppress the consumption of breathing gas when the mask is not in use. Therefore, the pneumatic assembly is connected to one of the doors of the box such that the feed of breathing gas is closed when the doors are closed and is open when the doors are open.
For instance, patent application US 2004/0144384 discloses such a box.
Problem with such a box is the occupied space in small aircraft. The known boxes are well suited for large aircraft, typically able to transport 100 passengers and more, in which the pilot cabin is large enough.
However, in small passenger aircrafts, typically able to transport between 10 and 80 passengers, the pilot cabin is crowded by all the equipments used to control the aircraft. And there is no space available around the seats of the pilots to install a stowage box as known in the prior art.
It would be advantageous to achieve a stowage box that can be installed inside a cabin of a small passenger aircraft but with the same functionality and safety as the box of the prior art, i.e. to allow the feed of breathable gas only when the mask is in use but always when the mask is in use.
To better address one or more concerns, in a first aspect of the invention, a stowage box for a breathing mask comprises:
And the pneumatic assembly is adapted to close the feed of breathing gas when the mask is inserted into the frame and to open the feed of breathing gas when the mask is extracted from the frame.
The box is advantageously controlling the feed of breathable gas through the position of the mask and not though the position of a door as in the prior art. Therefore the space occupied by the box is less than the space occupied by a prior art box as no space is used by the doors.
In particular embodiments:
These and other aspects of the invention will be apparent from and elucidated with reference to the embodiment described hereafter where:
In reference to
On the side 13, a mortise 17 leads into the open face. A groove 18 is formed on the side 13, at the entry of the mortise 17. The groove 18 is linear and substantially vertical.
A pneumatic assembly 19 is fixed at an end of the mortise 17 opposite to the open face 15.
The pneumatic assembly 19 comprises a button 21, a first tube 23 coming from a breathing gas generator (not represented) and a second tube 25 connected to the breathing mask. So the breathing mask is fed in breathable gas from the breathing gas generator through the pneumatic assembly 19.
The pneumatic assembly 19 further comprises,
The button 21 is the proximal end of a sliding valve 29 having a substantially cylindrical form. The valve 29 slides into a tube 31 running on from the base of the U of the duct 27. The valve 29 comprises two O-rings 33, 35, one roughly in the middle of the valve 29 and one at the distal end of the valve 29, opposite of the button 21. The sliding valve 29 comprises also a collar 37.
The tube 31 is screwed into a larger cylinder 39 leading into the duct 27.
The side 13 and the mortise 17 are adapted,
As shown in
The operation of the stowage box 1 is the following.
The pilot maintains the breathing mask 43 by means of the two parts 49, 51 that the pilot pinches with the thumb and at least the forefinger. The movable part 49 is in an inwards position. When the breathing mask 43 is inserted into the stowage box 1, the rigid part 41 slides along the side 13 and the mortise 17 guides the stand-outs 45 so that the breathing mask 43 is in position inside the stowage box 1. The stand-outs 45 having a L-shape, the border of the mortise 17 is inserted between the bottom of the rigid part 41 and the feet of the stand-outs 45. When the breathing mask is in stowage position, the pilot releases the movable part 49 so that the lug 53 is inserted into the groove 18 so that the breathing mask 43 is maintained in the stowage position by the stand-outs 45 and the lug 53.
In stowage position, the rigid part 41 pushes the button 21 and, therefore, the valve 29 in a close position where the duct 27 is hermetically obstructed by the end of the valve and the O-ring 35.
When the pilot needs the breathing mask 43, he pinches the movable part 49 as explained here above to move it inwards and disengage the lug 53 from the groove 18. Then, the pilot can extract the breathing mask 43 from the stowage box, releasing at the same time the valve 29. The breathing gas arrives into the duct 27 through the tube 23 at a pressure of at least 3 bars. Therefore the difference of pressure between the breathable gas and the cabin pressure is such that the valve 29 is pushed by the breathable gas and slides to an open position,
The collar 37 limits the movement of the valve 29 by butting against the tube 31 in the open position, and by butting against a shoulder of the duct in the close position.
While the invention has been illustrated and described in details in the drawings and foregoing description, such illustration and description are to be considered illustrative or exemplary and not restrictive; the invention is not limited to the disclosed embodiment.
For instance, different means may be used to maintain the breathing mask in stowage position such as a strap crossing the open face and fixed by a hook and loop fastener.
The groove 18 and its counterpart 53 are described on the right-hand side of the box. However, they may be positioned on the left-hand side or doubled on each side of the mask/box.
In another embodiment, the duct may have an L-shape with the tube 23 running on from the valve 29.
Though the description of the embodiment is done for a stowage box having an open face on a vertical side, the man skilled in the art understands that the described stowage box may be positioned differently, for instance with the open face on the top side of the stowage box.
Other variations to the disclosed embodiments can be understood and effected by those skilled on the art in practicing the claimed invention, from a study of the drawings, the disclosure and the appended claims. In the claims, the word “comprising” does not exclude other elements and the indefinite article “a” or “an” does not exclude a plurality.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/IB2007/053438 | 7/10/2007 | WO | 00 | 6/22/2010 |
Publishing Document | Publishing Date | Country | Kind |
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WO2009/007794 | 1/15/2009 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
3073301 | Hay et al. | Jan 1963 | A |
4002167 | Rambosek | Jan 1977 | A |
4561544 | Reeve | Dec 1985 | A |
4625721 | Levine et al. | Dec 1986 | A |
4735002 | Rath | Apr 1988 | A |
4915106 | Aulgur et al. | Apr 1990 | A |
5036846 | Aulger et al. | Aug 1991 | A |
5954052 | McDonald et al. | Sep 1999 | A |
6026590 | Picozza et al. | Feb 2000 | A |
6470887 | Martinez | Oct 2002 | B1 |
6755194 | Taieb | Jun 2004 | B2 |
6923183 | Martinez et al. | Aug 2005 | B2 |
6994086 | Martinez et al. | Feb 2006 | B1 |
7047972 | Ging et al. | May 2006 | B2 |
20040144384 | Martinez | Jul 2004 | A1 |
20120325216 | Bruckert | Dec 2012 | A1 |
Number | Date | Country |
---|---|---|
1433502 | Jun 2004 | EP |
WO02100487 | Dec 2002 | WO |
2011089463 | Jul 2011 | WO |
Entry |
---|
International Search Report in International Application No. PCT/IB2007/053438. |
International Search Report dated Oct. 19, 2010 in Application No. PCT/IB2010/000607. |
Number | Date | Country | |
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20100288281 A1 | Nov 2010 | US |