Pyrotechnic latch actuator responsive to a decompression detection system and method

1. A system for monitoring a pressure change within at least one compartment of an aircraft and operating a pyrotechnic device associated with a door latch, comprising:

a door latch structured and arranged in an aircraft door that comprises a pyrotechnic actuator and a latch bolt;

the pyrotechnic actuator configured to move and unlock the latch bolt when the pyrotechnic actuator is actuated;

a pressure sensor configured to provide a pressure signal corresponding to a pressure within a compartment of an aircraft;

a controller responsive to the pressure signal corresponding to the pressure within a compartment of an aircraft from the pressure sensor;

the controller further configured to determine a decompression event based on the pressure signal corresponding to the pressure within a compartment of an aircraft from the pressure sensor;

an output driver configured to generate an output driver signal to actuate the pyrotechnic actuator when the controller determines the decompression event based on the pressure signal corresponding to the pressure within the compartment of the aircraft from the pressure sensor;

an electromechanical device configured to receive power and electromechanically move the latch bolt from a locked position to an unlocked position; and

the electromechanical device configured to receive power and electromechanically move the latch bolt from an unlocked position to a locked position,

wherein the pyrotechnic device is configured to move the electromechanical device and the latch bolt when the pyrotechnic device is actuated.

2. The system of claim 1 , further comprising:

a flange that is connected to the latch bolt and configured to move the latch bolt in response to the pyrotechnic actuator being actuated.

3. The system of claim 1 , further comprising:

a latch housing configured to house at least the latch bolt; and

a pressure chamber located within the latch housing, the pressure chamber operatively connected to the pyrotechnic actuator.

4. The system of claim 1 , further comprising:

a spring configured to be moved in response to the pyrotechnic actuator being actuated and the latch bolt being moved by an actuation of the pyrotechnic actuator; and

the spring further configured to return the latch bolt to a normal operating position after implementation of the pyrotechnic actuator.

5. The system of claim 1 , further comprising:

a housing configured to support the pyrotechnic actuator; and

the housing configured to contact a flange that is connected to the latch bolt and configured to move the latch bolt in response to the pyrotechnic actuator being actuated.

6. The system of claim 1 , further comprising:

a latch housing configured to house at least the latch bolt;

a pressure chamber located within the latch housing, the pressure chamber operatively connected to the pyrotechnic actuator;

a spring configured to be moved in response to the pyrotechnic actuator being actuated and the latch bolt being moved by an actuation of the pyrotechnic actuator; and

the spring further configured to return the latch bolt to a normal operating position after implementation of the pyrotechnic actuator.

7. The system of claim 1 , wherein

the controller being configured to band pass filter the pressure signal and generate a filtered pressure signal;

the controller being configured to determine a change in the filtered pressure signal and generate a pressure change output signal corresponding to a change in pressure; and

the controller being configured to determine whether the pressure change output signal meets a predetermined threshold and generate a threshold output signal indicating that a decompression event has occurred if the pressure change output signal meets the predetermined threshold.

8. A process for monitoring a pressure change within at least one compartment of an aircraft and operating a pyrotechnic device associated with a door latch, comprising:

arranging a door latch in an aircraft door that comprises a pyrotechnic actuator and a latch bolt;

configuring the pyrotechnic actuator to move and unlock the latch bolt when the pyrotechnic actuator is actuated;

generating a pressure signal corresponding to a pressure within a compartment of an aircraft with a pressure sensor;

receiving the pressure signal corresponding to the pressure within a compartment of an aircraft from the pressure sensor with a controller;

determining with the controller a decompression event based on the pressure signal corresponding to the pressure within a compartment of an aircraft from the pressure sensor;

generating a driver signal with an output driver to actuate the pyrotechnic actuator when the controller determines the decompression event based on the pressure signal corresponding to the pressure within the compartment of the aircraft from the pressure sensor;

configuring an electromechanical device to receive power and electromechanically move the latch bolt from a locked position to an unlocked position; and

configuring the electromechanical device to receive power and electromechanically move the latch bolt from an unlocked position to a locked position; and

configuring the pyrotechnic device to move the electromechanical device and the latch bolt when the pyrotechnic device is actuated.

9. The process of claim 8 , further comprising:

configuring a flange to be connected to the latch bolt and to move the latch bolt in response to the pyrotechnic actuator being actuated.

10. The process of claim 8 , further comprising:

configuring a latch housing to house at least the latch bolt; and

configuring a pressure chamber to be located within the latch housing, the pressure chamber operatively connected to the pyrotechnic actuator.

11. The process of claim 8 , further comprising:

configuring a spring to be moved in response to the pyrotechnic actuator being actuated and the latch bolt being moved by an actuation of the pyrotechnic actuator; and

configuring the spring to return the latch bolt to a normal operating position after implementation of the pyrotechnic actuator.

12. The process of claim 8 , further comprising:

configuring a housing to support the pyrotechnic actuator; and

configuring the housing to contact a flange that is connected to the latch bolt and configured to move the latch bolt in response to the pyrotechnic actuator being actuated.

13. The process of claim 8 , further comprising:

configuring a latch housing to house at least the latch bolt;

configuring a pressure chamber to be located within the latch housing, the pressure chamber operatively connected to the pyrotechnic actuator;

configuring a spring to be moved in response to the pyrotechnic actuator being actuated and the latch bolt being moved by an actuation of the pyrotechnic actuator; and

configuring the spring to return the latch bolt to a normal operating position after implementation of the pyrotechnic actuator.

14. The process of claim 8 , wherein

band pass filtering the pressure signal and generating a filtered pressure signal;

determining a change in the filtered pressure signal and generating a pressure change output signal corresponding to a change in pressure; and

determining whether the pressure change output signal meets a predetermined threshold and generating a threshold output signal indicating that a decompression event has occurred if the pressure change output signal meets the predetermined threshold.