Abstract: In one version there is provided a shaft locking assembly for use in an apparatus, to provide motion control and unwanted movement elimination of the apparatus. The shaft locking assembly includes a locking device with a locking shaft having a castellated ring element with castellations. The shaft locking assembly includes a drive shaft and a rotating element disposed around the drive shaft. The shaft locking assembly includes a retaining structure assembly having a side portion with projection members corresponding to the castellations. The shaft locking assembly is in a locked position when the castellations are engaged and interlocked with the projection members, and the shaft locking assembly is in an unlocked position when a shaft engagement device is engaged with the drive shaft and the locking shaft, and actuates the locking shaft, so that the castellations are disengaged and unlocked from the projection members, and rotates the drive shaft.

Abstract: In one version there is provided a shaft locking assembly for use in an apparatus, to provide motion control and unwanted movement elimination of the apparatus. The shaft locking assembly includes a locking device with a locking shaft having a castellated ring element with castellations. The shaft locking assembly includes a drive shaft and a rotating element disposed around the drive shaft. The shaft locking assembly includes a retaining structure assembly having a side portion with projection members corresponding to the castellations. The shaft locking assembly is in a locked position when the castellations are engaged and interlocked with the projection members, and the shaft locking assembly is in an unlocked position when a shaft engagement device is engaged with the drive shaft and the locking shaft, and actuates the locking shaft, so that the castellations are disengaged and unlocked from the projection members, and rotates the drive shaft.

Abstract: An apparatus to protect exposed structures on an aircraft which includes a core; a securing mechanism coupled to the core; and an outer coating applied to the core to encapsulate the core and facilitate the attachment of the securing mechanism. A thermal protection layer may be applied to the apparatus for high temperature applications.

Abstract: A exposed edge protection device molded from an elastomer or a combination of elastomers of varying durometers formed together to match the outer mold line of an exposed edge. The device may include encapsulated flexible magnets providing for a durable monolithic device produced cost-effectively in a single-step process.

Abstract: An apparatus to protect exposed structures on an aircraft which includes a core; a securing mechanism coupled to the core; and an outer coating applied to the core to encapsulate the core and facilitate the attachment of the securing mechanism. A thermal protection layer may be applied to the apparatus for high temperature applications.