Abstract: An onboard rebreathing loop system resident on an aircraft for providing oxygen to aircraft personnel includes a ceramic oxygen generating system (COGS) module configured to receive an inlet air and output a high purity oxygen (O2) gas into a breathing loop and a carbon dioxide (CO2) scrubber module configured to receive exhaled air from the aircraft personnel and output a CO2-scrubbed air into the breathing loop. The high purity O2 gas and CO2-scrubbed air are mixed to form a mixed gas having a partial pressure of O2 suitable for breathing by the aircraft personnel. The onboard rebreathing loop system may further include an odor removal module, an air temperature and/or humidity control module to condition the mixed gas before breathing by the aircraft personnel, and a gas sensor module to confirm the partial pressure of O2 within the mixed gas before breathing by the aircraft personnel.

Abstract: A coalescing filter includes a housing, a top fitting and bottom fitting. The housing includes a sidewall defining a central chamber configured to receive a filter element therein. The top fitting is coupled to a top end of the housing and includes an inlet port configured to receive a moist source gas and direct the source gas into the filter element. The bottom fitting is coupled to a bottom end of the housing and includes an outlet orifice configured to discharge a dry product gas. The bottom fitting includes a pedestal configured to extend within the central chamber a spaced distance from the plurality of sidewalls. The pedestal is configured to seat the filter element thereon and further includes an outlet port in fluid communication with the outlet orifice.

Abstract: An onboard rebreathing loop system resident on an aircraft for providing oxygen to aircraft personnel includes a ceramic oxygen generating system (COGS) module configured to receive an inlet air and output a high purity oxygen (O2) gas into a breathing loop and a carbon dioxide (CO2) scrubber module configured to receive exhaled air from the aircraft personnel and output a CO2-scrubbed air into the breathing loop. The high purity O2 gas and CO2-scrubbed air are mixed to form a mixed gas having a partial pressure of O2 suitable for breathing by the aircraft personnel. The onboard rebreathing loop system may further include an odor removal module, an air temperature and/or humidity control module to condition the mixed gas before breathing by the aircraft personnel, and a gas sensor module to confirm the partial pressure of O2 within the mixed gas before breathing by the aircraft personnel.

Abstract: A coalescing filter includes a housing, a top fitting and bottom fitting. The housing includes a sidewall defining a central chamber configured to receive a filter element therein. The top fitting is coupled to a top end of the housing and includes an inlet port configured to receive a moist source gas and direct the source gas into the filter element. The bottom fitting is coupled to a bottom end of the housing and includes an outlet orifice configured to discharge a dry product gas. The bottom fitting includes a pedestal configured to extend within the central chamber a spaced distance from the plurality of sidewalls. The pedestal is configured to seat the filter element thereon and further includes an outlet port in fluid communication with the outlet orifice.

Abstract: A buckle release mechanism can be used to couple together various types of straps, webbing or belts. In one particular embodiment, the release mechanism forms part of a parachute canopy for a pilot's harness. The mechanism includes a housing with a locking mechanism. The locking mechanism employs two rotatable locking pins with associated cams and openings. An opening is formed within the housing for receiving a yoke. A striker plate with opposing lugs is formed at one end of the yoke. The lugs cooperate with the locking pins to either retain or eject the striker plate within the housing.

Abstract: A buckle release mechanism can be used to couple together various types of straps, webbing or belts. In one particular embodiment, the release mechanism forms part of a parachute canopy for a pilot's harness. The mechanism includes a housing with a locking mechanism. The locking mechanism employs two rotatable locking pins with associated cams and openings. An opening is formed within the housing for receiving a yoke. A striker plate with opposing lugs is formed at one end of the yoke. The lugs cooperate with the locking pins to either retain or eject the striker plate within the housing.

Abstract: A first aspect of the invention includes a multi-stage gas compressor having a central cam with a plurality of pistons operably connected to and radially extending from the central cam. The cam follower assemblies each include a roller element connected to a roller bracket which rides within and along a guide channel defines by facing grooves formed in housing end plates.

Abstract: A first aspect of the invention includes a multi-stage gas compressor having a central cam with a plurality of pistons operably connected to and radially extending from the central cam. The cam follower assemblies each include a roller element connected to a roller bracket which rides within and along a guide channel defines by facing grooves formed in housing end plates.

Abstract: An electronic controller (16) controls the operation of an electrochemical oxygen generating system (14) producing a desired gas. The product gas is fed to a storage unit (12) or a regulator (28) and pulsing valve (28) controlling the gas flow to a user. A two-stage system (180) combines a low pressure 100 and a high pressure (150) gas generating subsystems. The low pressure subsystem (100) uses IMAT's (106) to pump oxygen from ambient air to generate a low-pressure. The high pressure subsystem (150) uses IMAT's (160) to pump oxygen to high-pressure oxygen storage devices (194).