摘要:
The invention relates to a respiratory protection hood which comprises a sealed flexible shell (2) including a pressurised oxygen vessel (3) provided with a calibrated output opening (7) leading into the inside space of the flexible shell (2) and a device for trapping at least one portion of the carbon dioxide exhaled by the user, comprising a cartridge (4) for adsorbing carbon dioxide with a radial structure comprising a tubular body extending in a longitudinal direction (A) and covering a volume (8) of material which absorbs carbon dioxide, said structure of the cartridge (4) comprising a perforated tube (9) arranged around the volume (8) of absorbent material and extending in the longitudinal direction (A) to allow the transit of air to be purified radially in the volume (8) of absorbent material, at least one portion of the perforated tube (9) being arranged around the volume of absorbent material in direct communication with the inside space of the hood (2).
摘要:
An emergency oxygen supply system for aircraft comprising a source (2) of compressed oxygen, means (3) for releasing oxygen from the source (2) in case of a drop in air pressure, at least one oxygen mask (4), a respective mechanical breath-actuated valve (14) for releasing a pulse of oxygen into the or each mask (4) and a pressure reducer (15) for releasing oxygen from the source into an intermediate reservoir (5) upstream of the mechanical breath-actuated pulse valve (14).
摘要:
Hood comprising a flexible envelope (2) and a reservoir (3) of oxygen comprising a calibrated outlet orifice (4) that leads into the internal volume of the envelope (2), the outlet orifice (4) being closed off by a removable stopper (5), characterized in that the reservoir (3) of pressurized oxygen comprises two independent storage compartments (6, 7), a first compartment (6) of which communicates with the outlet orifice (4) and a second compartment (7) of which is isolated from the outlet orifice (4) via a sealed partition provided with a member (8, 9, 10) for opening the partition, the opening member (8, 9) being switchable between a first configuration which prevents fluidic communication between the second compartment (7) and the outlet orifice (4) and a second configuration that allows fluidic communication between the second compartment (7) and the outlet orifice (4), the opening member (8, 9, 10) being sensitive to the pressure difference between the second compartment (7) and the first compartment (6) and being configured to automatically switch from the first to the second configuration when the pressure difference between the second compartment (7) and the first compartment (6) is less than a given threshold.
摘要:
Respiratory protection hood comprising a flexible envelope (2) and a reservoir (3) of pressurized oxygen comprising an outlet orifice (3) that leads into the internal volume of the envelope (2), the outlet orifice (4) being closed off by a removable stopper (5), characterized in that the reservoir (3) of oxygen comprises, upstream of the orifice (4), a passage (6) for the pressurized gas and a needle (7) that is able to move in a given direction (A) of displacement in said passage (6), the needle (7) being subjected to two opposite forces in the direction (A) of displacement, said forces being respectively generated on the one hand by the pressure of the gas in the reservoir (3) and on the other hand by a return member (8), the needle (7) having a section with a defined profile that is variable in the direction (A) of displacement in order to modify the degree of closure of the passage depending on the position of said needle relative to the passage (6) so as to regulate the flow rate of gas allowed to escape via the passage (6) towards the orifice (4) as a function of time and the pressure of gas in the reservoir (3).
摘要:
According to the invention, passengers are supplied with a first fraction of oxygen-enriched air from independent supply means, in particular high-pressure cylinders (16), during a descent phase in which the aircraft descends from a normal cruising altitude to an intermediary diversion altitude. Moreover, compressed air is taken from the aircraft's own compressed air source in order to produce (in 2) a second fraction of said oxygen-enriched air, which is delivered to the passengers at least during a stabilised flight phase of the aircraft at an altitude close to the diversion altitude, above 5,500 metres.