A canopy fragilization system for use in an aircraft ejection system may comprise: a sharp breaker disposed on a first side of an ejection seat, the sharp breaker configured to act as a primary breaker of a canopy of an aircraft; a blunt breaker disposed on a second side of the ejection seat, the blunt breaker configured to act as a secondary breaker of the canopy of the aircraft; and a deployable overhead protection assembly comprising a first tertiary breaker and a second tertiary breaker.

Aspects of this disclosure relate to a removable fuselage expansion window assembly, comprising: a window panel; an outer window frame; a window bracket configured to secure the window panel to the outer window frame; an inner window frame with an indented rim that is aligned with the window bracket; and a latch assembly located below the indented rim of the inner window frame between the outer window frame and the inner window frame. The latch assembly includes one or more retainers to hold a bottom portion of the removable fuselage expansion window assembly within a rectangular frame formed by vertical and horizontal beams in an outer wall of an aircraft, wherein the latch assembly includes a lever that releases the removable fuselage expansion window assembly by disengaging the one or more retainers from the rectangular frame when the lever is pulled.

Aspects of this disclosure relate to a removable fuselage expansion window assembly, comprising: a window panel; an outer window frame; a window bracket configured to secure the window panel to the outer window frame; an inner window frame with an indented rim that is aligned with the window bracket; and a latch assembly located below the indented rim of the inner window frame between the outer window frame and the inner window frame. The latch assembly includes one or more retainers to hold a bottom portion of the removable fuselage expansion window assembly within a rectangular frame formed by vertical and horizontal beams in an outer wall of an aircraft, wherein the latch assembly includes a lever that releases the removable fuselage expansion window assembly by disengaging the one or more retainers from the rectangular frame when the lever is pulled.

A pyrotechnic egress system for a structure may comprise an explosive cord, an outer sheath disposed about the explosive cord, and a stress concentrator coupled to the outer sheath. The stress concentrator may comprise a triangular cross section. The stress concentrator may include a standoff structure.

Ejection system for a vehicle emergency exit ejection system for a vehicle emergency exit, the emergency exit extending along a base surface and being designed to cooperate in a mounted position with a receiving frame of the vehicle, the ejection system including a retaining element and a locking mechanism designed to cooperate with the retaining element in a locking configuration in which a movable part of the locking mechanism prevents a relative movement of the retaining element and the locking mechanism in a direction of ejection of the emergency exit which is transversal to the base surface, the movable part being configured to be moved in a closing plane that extends transversally to the base surface and an ejection configuration in which the locking mechanism is capable of moving in the direction of ejection relative to the retaining element.

Ejection system for a vehicle emergency exit ejection system for a vehicle emergency exit, the emergency exit extending along a base surface and being designed to cooperate in a mounted position with a receiving frame of the vehicle, the ejection system including a retaining element and a locking mechanism designed to cooperate with the retaining element in a locking configuration in which a movable part of the locking mechanism prevents a relative movement of the retaining element and the locking mechanism in a direction of ejection of the emergency exit which is transversal to the base surface, the movable part being configured to be moved in a closing plane that extends transversally to the base surface and an ejection configuration in which the locking mechanism is capable of moving in the direction of ejection relative to the retaining element.

A system for initiating a canopy release signal for a canopy of an aircraft includes a first striker secured to the canopy, and a first initiator assembly secured to a fuselage of the aircraft. The first initiator assembly has a protrusion. The first striker is configured to be rotated against the protrusion of the first initiator assembly. The canopy release signal is output in response to the first striker rotating against the protrusion of the first initiator assembly.

A system for initiating a canopy release signal for a canopy of an aircraft includes a first striker secured to the canopy, and a first initiator assembly secured to a fuselage of the aircraft. The first initiator assembly has a protrusion. The first striker is configured to be rotated against the protrusion of the first initiator assembly. The canopy release signal is output in response to the first striker rotating against the protrusion of the first initiator assembly.

A canopy fragilization system for use in an aircraft ejection system may comprise: a sharp breaker disposed on a first side of an ejection seat, the sharp breaker configured to act as a primary breaker of a canopy of an aircraft; a blunt breaker disposed on a second side of the ejection seat, the blunt breaker configured to act as a secondary breaker of the canopy of the aircraft; and a deployable overhead protection assembly comprising a first tertiary breaker and a second tertiary breaker.

A canopy fragilization system for use in an aircraft ejection system may comprise: a sharp breaker disposed on a first side of an ejection seat, the sharp breaker configured to act as a primary breaker of a canopy of an aircraft; a blunt breaker disposed on a second side of the ejection seat, the blunt breaker configured to act as a secondary breaker of the canopy of the aircraft; and a deployable overhead protection assembly comprising a first tertiary breaker and a second tertiary breaker.