US 5,118,053 AGranted

Pressure equalization systems

AssigneeThe Boeing Company

InventorsAshok K. Singh, Scott E. Coburn

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Abstract

A system for preventing the sudden depressurization of a compartment in an aircraft from causing structural damage or damage to other critical aircraft components. The system includes a pivotable closure. Normally, this closure is latched across a passage between a pressurized compartment such as a passenger cabin and a dump such as the space between the cabin wall and the outer skin of the aircraft. In the event that pressure is suddenly lost in a second pressurized compartment such as a cargo hold beneath the floor of the passenger compartment, a pressure differential is created across a flap-type latch actuator carried by the closure. This rotates the actuator, disengaging an actuator-associated latch element from a fixedly mounted keeper and thereby allowing the closure to be swung to an open position by outrushing air. This makes the entire area of the passage to the dump available for the outflow of air. As a consequence, the pressure between the two compartments is rapidly equalized, keeping the floor of the passenger compartment from collapsing and preventing damage to critical aircraft components routed beneath the floor or through the aircraft body such as control cables, electrical leads, and hydraulic lines.

Claims7

Dependent claims

The combination of an aircraft body having:

a first pressurizable compartment, a second pressurizable compartment, wall means between said first and second compartments, and dump means to which air can flow from the first of said compartments with means automatically operable coincident with a sudden decrease of the pressure in the second compartment to increase the area of a flow path between said first compartment and said dump means and thereby allow the pressure between the first and second compartments to equalize with sufficient rapidity to prevent the differential in pressure between the first and second compartments from exerting on said wall means a force of a high enough magnitude to collapse or otherwise damage said wall means or components of the aircraft in the proximity of said wall means, there being a passage between said first compartment and said dump means, a closure means spanning said passage, means so mounting said closure means for pivotable movement about one edge thereof relative to said aircraft body that air can flow from said first compartment to said dump means at a high rate when said closure means is pivoted to an open position, an opening through said closure means for accommodating the flow of return heating and/or conditioning air from said first compartment to said dump means at a lower rate in the absence of the decompression of the second compartment, and means for conducting air from said opening to said dump means at said lower rate comprising a duct having an inner, return air discharge end and an outer, return air inlet end, the outer end of said duct being fixed to said closure means in surrounding relationship to the opening through the closure means and said flow accommodating means also including an apertured grill which spans and is fixed to said duct at the inner, discharge end thereof.

The combination of an aircraft body having a first pressurizable compartment, a second pressurizable compartment, wall means between said first and second compartments, and a dump means to which air can flow from the first of said compartments with means automatically operable coincident with a sudden decrease of the pressure in the second compartment to increase the area of the flow path between said first compartment and said dump means and thereby allow the pressure between the first and second compartments to equalize with sufficient rapidity to prevent the differential in pressure between the first and second compartments from collapsing or otherwise damaging said wall means or components of the aircraft in the proximity of said wall means, there being a passage between said dump means and the means for increasing the area of the flow path between the first compartment and the dump means comprising:

a closure means spanning said passage, means mounting said closure means or pivotable movement about one edge thereof relative to said aircraft body, a latch means having one component fixed relative to said aircraft body and a second component which is fixed to said closure means at an edge thereof opposite said one edge and is so engageable with said first component that said sudden decrease in pressure will create a pressure differential between the first and dump means of sufficient magnitude to disengage said second latch component from the first latch component and a rotation of said closure means about said mounting means to an open position in which essentially the full area of said passage is available for the pressure equalizing flow of air form said first compartment to said dump means, there being an opening through said closure means and the combination also including means for accommodating the flow of air from said second compartment into said dump means at a lower rate that comprises a duct having an inner, return air discharge end and an outer, return air inlet end, the outer end of said duct being fixed to said closure means in surrounding relationship to the opening through the closure means and said means for accommodating the flow of air through the closure means at the lower rate also including an apertured grill which spans and is fixed to said duct at the inner, discharge end thereof.

a closure means spanning said passage, means mounting said closure means for pivotable movement about one edge thereof relative to said aircraft body, a latch means having one component fixed relative to said aircraft body and a second component which is fixed to said closure means at an edge thereof opposite said one edge and is so engageable with said first component that said sudden decrease in pressure will create a pressure differential between the first compartment and the dump means of sufficient magnitude to disengage said second latch component from the first latch component and effect a rotation of said closure means about said mounting means to an open position in which essentially the full area of said passage is available for the pressure equalizing flow of air form said first compartment to said dump means, said latch means including an elongated, non-hinged, flap-type actuator and mounting means pivotably fixing said actuator to said closure means for pivotable movement about a second axis located at said opposite edge of the closure means and said first latch component being carried by said actuator, whereby a sudden decompression of said second compartment as aforesaid will so create a pressure differential across said actuator as to rotate the actuator about said second axis and disengage said first latch component form said second latch component and allow said closure means to be rotatably displaced to said open position by the pressure differential-generated force as aforesaid.

The combination of an aircraft body having a first pressurizable compartment, a second pressurizable compartment, wall means between said first and second compartments, and dump means to which air can flow from the first of said compartments with means automatically operable coincident with a sudden decrease of the pressure in the second compartment to increase the area of the flow path between said first compartment and said dump means and thereby allow the pressure between the first and second compartments to rapidly equalize and prevent the collapse of or damage to said wall means or components of the aircraft in the proximity of said wall means, there being a duct providing a flow passage between said first compartment and said dump means with a return air inlet at the duct end nearest the first compartment and a return air outlet at the opposite duct end and the automatically operable means including a closure means spanning said passage, means mounting said closure means for pivotable movement about one edge thereof relative to said aircraft body, and a latch means having one component fixed relative to said aircraft body and a second component which is fixed to said closure means at an edge thereof opposite said one edge and is so engageable with said first component that said sudden decrease in pressure will create a pressure differential between the first compartment and the dump means of sufficient magnitude to disengage said second latch component from the first latch component and enable a rotation of said closure means about said mounting means to an open position in which essentially the full area of said passage is available for the pressure equalizing flow of air from said first compartment to said dump means and said combination further comprising means in said closure means through which conditioning or heating air can be discharged when said closure means is in the closed position and an apertured grill which spans and is fixed to the opposite end of said duct and controls the flow of air from the first compartment through the passage to said dump means.

Dependencies are inferred from the claim text.