Monitor stop device
A monitor stop system is disclosed. The system may include a top-tilting monitor. The system may also include a monitor shroud including a tab configured to prevent the monitor from actuating to the deployed position during an HIC event. The system may further include one or more monitor stop devices. Each monitor stop device may include a spring-loaded pin assembly and a housing configured to surround at least a portion of the spring-loaded assembly. The tab may be configured to translate towards an interior surface of the seatback bezel and may be configured to cause the pin to translate through one or more monitor stop openings of the seatback bezel. Upon the pin translating, the pin may be configured to capture at least a portion of the top-tilting monitor to prevent the top-tilting monitor from actuating to the deployed position during the HIC event.
1. An aircraft seat, the aircraft seat comprising:
a seatback including a seatback bezel, the seatback bezel including one or more monitor stop openings;
an in-flight entertainment device coupled to a surface of the seatback bezel, the in-flight entertainment device including a top-tilting monitor configured to actuate about a top axis of the top-tilting monitor between at least a stowed position and a deployed position, the in-flight entertainment device including a monitor shroud configured to couple the top-tilting monitor to the seatback, the monitor shroud including a tab configured to prevent the top-tilting monitor from actuating to the deployed position during a head injury criterion (HIC) event; and
one or more monitor stop devices, each monitor stop device comprising:
a spring-loaded pin assembly including a compressible spring and a pin, the compressible spring configured to compress along a horizontal axis of a shaft of the pin; and
a housing configured to surround at least a portion of the spring-loaded assembly, the housing configured to couple the spring-loaded pin assembly to a portion of the seatback bezel;
the tab of the monitor shroud configured to translate towards an interior surface of the seatback bezel when a force is applied to the top-tilting monitor during the HIC event,
upon the tab of the monitor shroud translating towards the interior surface of the seatback bezel, the compressible spring configured to cause the pin to translate through the one or more monitor stop openings,
upon the pin translating through the one or more monitor stop openings, the pin configured to capture at least a portion of the top-tilting monitor to prevent the top-tilting monitor from actuating to the deployed position during the HIC event.
2. The aircraft seat of claim 1 , wherein the spring-loaded pin assembly further comprises at least one of:
one or more retaining clips, one or more washers, one or more bushings, or one or more rivets.
3. The aircraft seat of claim 1 , wherein the housing is configured to couple the spring-loaded pin assembly to the portion of the seatback bezel at a central axis of the top-tilting monitor.
4. The aircraft seat of claim 1 , wherein the housing includes one or more pin openings configured to receive at least a portion of the shaft of the pin, the pin configured to translate through the one or more pin openings of the housing,
upon the tab of the monitor shroud translating towards the interior surface of the seatback bezel, the compressible spring configured to cause the pin to translate through the one or more pin openings in the housing.
5. The aircraft seat of claim 1 , wherein the housing is formed of sheet metal.
6. The aircraft seat of claim 1 , wherein the housing is formed of plastic.
7. A monitor stop system, the monitor stop system comprising:
a top-tilting monitor configured to actuate about a top axis of the top-tilting monitor between at least a stowed position and a deployed position;
a monitor shroud including a tab configured to prevent the top-tilting monitor from actuating to the deployed position during a head injury criterion (HIC) event; and
one or more monitor stop devices, each monitor stop device comprising:
a spring-loaded pin assembly including a compressible spring and a pin, the compressible spring configured to compress along a horizontal axis of a shaft of the pin; and
a housing configured to surround at least a portion of the spring-loaded assembly, the housing configured to couple the spring-loaded pin assembly to a portion of a seatback bezel of a seat;
the tab of the monitor shroud configured to translate towards an interior surface of the seatback bezel when a force is applied to the top-tilting monitor during the HIC event,
upon the tab of the monitor shroud translating towards the interior surface of the seatback bezel, the compressible spring configured to cause the pin to translate through one or more monitor stop openings of the seatback bezel,
upon the pin translating through the one or more monitor stop openings, the pin configured to capture at least a portion of the top-tilting monitor to prevent the top-tilting monitor from actuating to the deployed position during the HIC event.
8. The system of claim 7 , wherein the seat includes an aircraft seat.
9. The system of claim 8 , wherein the aircraft seat comprises:
an aircraft seatback including the seatback bezel, the seatback bezel including the one or more monitor stop openings.
10. The system of claim 7 , wherein the spring-loaded pin assembly further comprises at least one of:
one or more retaining clips, one or more washers, one or more bushings, or one or more rivets.
11. The system of claim 7 , wherein the housing is configured to couple the spring-loaded pin assembly to the portion of the seatback bezel at a central axis of the top-tilting monitor.
12. The system of claim 7 , wherein the housing includes one or more pin openings configured to receive at least a portion of the shaft of the pin, the pin configured to translate through the one or more pin openings of the housing,
upon the tab of the monitor shroud translating towards the interior surface of the seatback bezel, the compressible spring configured to cause the pin to translate through the one or more pin openings in the housing.
13. The system of claim 7 , wherein the housing is formed of sheet metal.
14. The system of claim 7 , wherein the housing is formed of plastic.