Aircraft cart retention system

1. An aircraft cart retention system, comprising:

a first aircraft cart retention device configured to actuate between a first deployed position and a first stowed position, the first aircraft cart retention device comprising:

at least one member coupled to a structure installed within an aircraft cabin; and

at least one latch coupled to the at least one member; and

a second aircraft cart retention device configured to actuate between a second deployed position and a second stowed position, the second aircraft cart retention device comprising:

at least an additional member coupled to the structure installed within the aircraft cabin; and

at least an additional latch coupled to the at least an additional member,

the first aircraft cart retention device and the second aircraft cart retention device configured to retain an aircraft cart in a position proximate to an exterior surface of the structure with at least two combined points of contact during non-taxi, takeoff, or landing (non-TTL) stages of flight when the first aircraft cart retention device is in the first deployed position and the second aircraft cart retention device is in the second deployed position,

the first aircraft cart retention device and the second aircraft cart retention device configured to allow the aircraft cart to be removed from the position proximate to the exterior surface of the structure when the first aircraft cart retention device is in the first stowed position and the second aircraft cart retention device is in the second stowed position,

the structure including a first cavity configured to receive the first aircraft cart retention device when the first aircraft cart retention device is in the first stowed position, the first aircraft cart retention device being configured to be at least partially inset within the first cavity when the first aircraft cart retention device is in the first stowed position,

the structure including a second cavity configured to receive the second aircraft cart retention device when the second aircraft cart retention device is in the second stowed position, the second aircraft cart retention device configured to be at least partially inset within the second cavity when the second aircraft cart retention device is in the second stowed position.

2. The aircraft cart retention system of claim 1 , the at least one member including a first linkage, a second linkage, and a first connecting linkage coupled to the first linkage and the second linkage; and

the at least an additional member including a third linkage, a fourth linkage, and a second connecting linkage coupled to the third linkage and the fourth linkage.

3. The aircraft cart retention system of claim 2 , the at least one latch including a first latch coupled proximate to a first joint coupling the first linkage and the first connecting linkage, and a second latch coupled proximate to a second joint coupling the second linkage and the first connecting linkage; and

the at least an additional latch including a third latch coupled proximate to a third joint coupling the third linkage and the second connecting linkage, and a fourth latch coupled proximate to a fourth joint coupling the fourth linkage and the second connecting linkage.

4. The aircraft cart retention system of claim 1 , the at least one member being configured to rotate about at least one axis through at least one hinge coupling the at least one member to the structure, the at least an additional member being configured to rotate about an at least an additional axis through at least an additional hinge coupling the at least an additional member to the structure.

5. The aircraft cart retention system of claim 4 , the at least one axis and the at least an additional axis being collinear.

6. The aircraft cart retention system of claim 1 , the at least one member comprising at least one shaft, the at least an additional member comprising at least an additional shaft.

7. The aircraft cart retention system of claim 6 , the at least one shaft being configured to extend outward from the structure when the first aircraft cart retention device is in the deployed position, the at least one shaft being configured to be inserted in the structure when the first aircraft cart retention device is in the deployed position,

the at least an additional shaft being configured to extend outward from the structure when the second aircraft cart retention device is in the deployed position, the at least an additional shaft being configured to be inserted in the structure when the second aircraft cart retention device is in the deployed position.

8. The aircraft cart retention system of claim 1 , further comprising:

a third aircraft cart retention device configured to actuate between a third deployed position and a third stowed position, comprising:

at least a third member coupled to the structure installed within the aircraft cabin; and

at least a third latch coupled to the at least a third member,

the first aircraft cart retention device and the third aircraft cart retention device configured to retain a second aircraft cart in a second position proximate to the exterior surface of the structure with at least two points of contact during the non-TTL stages of flight when the first aircraft cart retention device is in the first deployed position and the third aircraft cart retention device is in the third deployed position,

the first aircraft cart retention device and the third aircraft cart retention device configured to allow the aircraft cart to be removed from the second position proximate to the exterior surface of the structure when the first aircraft cart retention device is in the first stowed position and the third aircraft cart retention device is in the third stowed position,

the second aircraft cart being smaller than the first aircraft cart.

9. An aircraft cart retention system, comprising:

an aircraft cart retention device configured to actuate between a deployed position and a stowed position, comprising:

a first primary member coupled to a structure installed within an aircraft cabin;

a second primary member coupled to the structure installed within the aircraft cabin; and

at least one auxiliary member coupled to the first primary member and the second primary member,

the aircraft cart retention device configured to retain an aircraft cart in a position proximate to an exterior surface of the structure during non-taxi, takeoff, or landing (non-TTL) stages of flight when the aircraft cart retention device is in the deployed position,

the aircraft cart retention device configured to allow the aircraft cart to be removed from the position proximate to the exterior surface of the structure when the aircraft cart retention device is in the stowed position,

the structure including a cavity configured to receive the aircraft cart retention device when the aircraft cart retention device is in the stowed position, the aircraft cart retention device being configured to be at least partially inset within the cavity when the aircraft cart retention device is in the stowed position.

10. The aircraft cart retention system of claim 9 , at least one separator member being coupled to the structure installed within the aircraft cabin, the at least one separator member being configured to actuate between a second deployed position and a second stowed position,

the aircraft cart retention device and the at least one separator member being configured to retain a second aircraft cart in a second position proximate to the exterior surface of the structure during the non-TTL stages of flight when the aircraft cart retention device is in the first deployed position and the at least one separator member is in the second deployed position,

the aircraft cart retention device and the at least one separator member being configured to allow the aircraft cart to be removed from the second position proximate to the exterior surface of the structure when the aircraft cart retention device is in the first deployed position and the at least one separator member is in the second deployed position,

the second aircraft cart being smaller than the first aircraft cart.

11. The aircraft cart retention system of claim 9 , the at least one separator member being configured to independently actuate relative to the aircraft cart retention device.

12. The aircraft cart retention system of claim 9 , the at least one separator member being configured to couple to the at least one auxiliary member of the aircraft cart retention device.

13. The aircraft cart retention system of claim 9 , the structure including a second cavity configured to receive the at least one separator member when the at least one separator member is in a second stowed position, the aircraft cart retention device configured to be at least partially inset within the second cavity when a second aircraft cart retention device is in the second stowed position, the second cavity being connected with the cavity.