The present invention relates to a parachute deploying apparatus, comprising: a) a manifold with which is releasably coupled a single vessel within which pressurized gas is generated; b) a gas generator which cooperates with said vessel; c) a plurality of hollow tubes which extend obliquely and upwardly from, and are in communication with, said manifold; and d) a plurality of projectiles, each of which formed with a rod that is receivable in a corresponding tube and to each of which is connected a cord that is also connected to a corresponding portion of an undeployed parachute, wherein the pressurized gas which is generated upon triggering of said gas generator is flowable through each of said tubes to propel said plurality of projectiles in different directions and to cause said parachute to become deployed.

The present invention relates to a parachute deploying apparatus, comprising: a) a manifold with which is releasably coupled a single vessel within which pressurized gas is generated; b) a gas generator which cooperates with said vessel; c) a plurality of hollow tubes which extend obliquely and upwardly from, and are in communication with, said manifold; and d) a plurality of projectiles, each of which formed with a rod that is receivable in a corresponding tube and to each of which is connected a cord that is also connected to a corresponding portion of an undeployed parachute, wherein the pressurized gas which is generated upon triggering of said gas generator is flowable through each of said tubes to propel said plurality of projectiles in different directions and to cause said parachute to become deployed.

An aerial vehicle safety apparatus includes a piston member, a cylinder that accommodates the piston member and is provided with a hole through which the piston member protrudes outward at time of operation, a push-up member that is pushed up in one direction by the piston member, an expandable object that is pushed up while being supported by the push-up member, a gas generator as a power source that moves the piston member in the cylinder, and a first member and a second member that serve as a cylindrical container that accommodates the piston member, the cylinder, the push-up member, the expandable object, and the gas generator. The expandable object is stored in the container so as to form a plurality of layers in a radial direction.

The present disclosure describes a signal relay node that is physically displaceable by a delivery system to move the signal relay node to a different location, to enable the signal relay node to overcome physical obstructions to signal propagation. A delivery system, such as a launching system, can launch the signal relay node encased within a housing unit, such as a projectile cap. Upon launch into the air, an additional aloft package may provide an aerostat, parachute, and/or a propeller and motor system to keep the signal relay node aloft in the air for a longer period of time.

The present disclosure describes a signal relay node that is physically displaceable by a delivery system to move the signal relay node to a different location, to enable the signal relay node to overcome physical obstructions to signal propagation. A delivery system, such as a launching system, can launch the signal relay node encased within a housing unit, such as a projectile cap. Upon launch into the air, an additional aloft package may provide an aerostat, parachute, and/or a propeller and motor system to keep the signal relay node aloft in the air for a longer period of time.

Movement of a disrupter cannon is arrested by a parachute. The parachute is coupled (e.g., tethered) to the disrupter cannon. Prior to firing the cannon, the parachute is held in a retainer. Movement of the disrupter cannon in response to firing pulls the parachute from the retainer. The parachute deploys and arrests the movement of the disrupter cannon. The retainer protects the parachute prior to firing the disrupter cannon. The retainer may hold the parachute during transport.

Movement of a disrupter cannon is arrested by a parachute. The parachute is coupled (e.g., tethered) to the disrupter cannon. Prior to firing the cannon, the parachute is held in a retainer. Movement of the disrupter cannon in response to firing pulls the parachute from the retainer. The parachute deploys and arrests the movement of the disrupter cannon. The retainer protects the parachute prior to firing the disrupter cannon. The retainer may hold the parachute during transport.

There is provided a safety apparatus including a push-up member in which an ejected object is hardly displaced even during transportation, and an aerial vehicle including the safety apparatus. A safety apparatus 100 includes a cylinder 14 that accommodates a piston member 10 and is provided with a bore 13 through which the piston member 10 protrudes to the outside (upward in FIG. 1) during operation, a push-up member 15 that is pushed up in one direction by the piston member 10, an ejected object 16 that is pushed up while being supported by the push-up member 15, a gas generator 17 as a power source that moves the piston member 10 in the cylinder 14, a container 18 that has a bottomed cylindrical shape and accommodates the piston member 10, the cylinder 14, the push-up member 15, the ejected object 16, and the gas generator 17, and a lid 21 that closes an opening end of the container 18. A movement preventing member 27 that prevents the ejected object 16 from moving in a circumferential direction of a bottomed cylindrical portion 19 is provided on an upper surface of a support 20 of the push-up member 15.

A drop zone marker includes a parachute, a first light module connected to the parachute by a first length of cord and a second light module connected to the first light module by a second length of the cord. A ballast is connected to the second light module by a third length of the cord is provided for pulling downwardly the drop zone marker. The parachute is configured to include an integral packing/deployment bag within which all components of the drop zone marker are contained up until deployment.

A drop zone marker includes a parachute, a first light module connected to the parachute by a first length of cord and a second light module connected to the first light module by a second length of the cord. A ballast is connected to the second light module by a third length of the cord is provided for pulling downwardly the drop zone marker. The parachute is configured to include an integral packing/deployment bag within which all components of the drop zone marker are contained up until deployment.