Abstract: A cloud security control platform and method enforces security controls across multiple cloud environments, services and disparate teams while providing a frictionless “Permissions on Demand” mechanism for approvals and exceptions. In contrast to the prior art, security is evaluated on a permission by permission basis, with the default being that all permissions are denied and then only given to a particular identity on an as-needed basis. This approach reduces the security risks associated with the vast capabilities available in Public Cloud environments and permits an organization that uses the platform to grant access, approve exceptions and delegate approvals with the appropriate compliance.

Abstract: One embodiment is an aircraft including a fuselage; a wing connected to the fuselage; first and second booms connected to the wing on opposite sides of the fuselage; first and second forward propulsion systems attached to forward ends of the first and second booms; first and second aft propulsion systems fixedly attached proximate aft ends of the first and second booms; first and second wing-mounted propulsion systems connected to outboard ends of wings; and first and second wing tips fixedly connected to outboard sides of the first and second wing-mounted propulsion systems; wherein the first and second wing-mounted propulsion systems and the first and second wing tips are collectively tiltable between a first position when the aircraft is in a hover mode and a second position when the aircraft is in a cruise mode.

Abstract: A rotor system includes a rotor assembly and a duct system. The rotor assembly includes rotor blades extending from a mast axis and configured to rotate about the mast axis. The duct assembly includes a moveable duct portion and a stationary duct portion. In a first duct configuration, the moveable duct portion surrounds a first portion of the rotor assembly, the stationary duct portion surrounds a second portion of the rotor assembly, and the moveable duct portion and the stationary duct portion enclose the rotor assembly. In a second duct configuration, the stationary duct portion surrounds the second portion of the rotor assembly, and the moveable duct portion is moved away from the first portion of the rotor assembly, such that the rotor assembly is not enclosed.

Abstract: One embodiment is an aircraft including a fuselage; a wing connected to the fuselage; first and second booms connected to the wing on opposite sides of the fuselage; first and second forward propulsion systems attached to forward ends of the first and second booms; first and second aft propulsion systems fixedly attached proximate aft ends of the first and second booms; and first and second wing-mounted propulsion systems connected to outboard ends of wings; wherein the first and second wing-mounted propulsion systems are tiltable between a first position when the aircraft is in a hover mode and a second position when the aircraft is in a cruise mode.

Abstract: One embodiment is an aircraft including a fuselage; a wing connected to the fuselage; first and second booms connected to the wing on opposite sides of the fuselage; first and second forward propulsion systems attached to forward ends of the first and second booms; first and second aft propulsion systems fixedly attached proximate aft ends of the first and second booms; first and second wing-mounted propulsion systems connected to outboard ends of wings; and first and second wing tips fixedly connected to outboard sides of the first and second wing-mounted propulsion systems; wherein the first and second wing-mounted propulsion systems and the first and second wing tips are collectively tiltable between a first position when the aircraft is in a hover mode and a second position when the aircraft is in a cruise mode.

Abstract: A proprotor system for a ducted aircraft convertible between a vertical takeoff and landing flight mode and a forward flight mode includes a plurality of proprotor blades and a duct surrounding the proprotor blades. The duct includes an adaptive geometry device movable into various positions including a hover position and a cruise position. One or more actuators coupled to the adaptive geometry device are configured to move the adaptive geometry device between the hover position and the cruise position based on the flight mode of the ducted aircraft, thereby improving flight performance of the ducted aircraft.

Abstract: A rotor system includes a rotor assembly and a duct system. The rotor assembly includes rotor blades extending from a mast axis and configured to rotate about the mast axis. The duct assembly includes a moveable duct portion and a stationary duct portion. In a first duct configuration, the moveable duct portion surrounds a first portion of the rotor assembly, the stationary duct portion surrounds a second portion of the rotor assembly, and the moveable duct portion and the stationary duct portion enclose the rotor assembly. In a second duct configuration, the stationary duct portion surrounds the second portion of the rotor assembly, and the moveable duct portion is moved away from the first portion of the rotor assembly, such that the rotor assembly is not enclosed.

Abstract: A panel construction suitable for automotive parts comprises (a) a first composite fiber mat layer (b) adjacent to and covering a face of the fiber mat, a thermoplastic polymer film and optionally (c) adjacent to and covering the thermoplastic film, a second composite fiber mat layer, where the fiber mats comprise non-woven fibers or fabrics and a cured acrylic resin binder. The thermoplastic film is preferably a thermoplastic polyurethane film. The construction preferably contains no adhesive layer between components (a), (b) and (c).

Abstract: A panel construction suitable for automotive parts comprises (a) a first composite fiber mat layer (b) adjacent to and covering a face of the fiber mat, a thermoplastic polymer film and optionally (c) adjacent to and covering the thermoplastic film, a second composite fiber mat layer, where the fiber mats comprise non-woven fibers or fabrics and a cured acrylic resin binder. The thermoplastic film is preferably a thermoplastic polyurethane film. The construction preferably contains no adhesive layer between components (a), (b) and (c).

Abstract: Responding to an account reactivation request includes receiving an account reactivation request from a former subscriber having a deactivated account and automatically accessing stored account information related to the deactivated account based on the account reactivation request. The stored account information is compared with a reactivation standard to produce a comparison result. Based on the comparison result a response to the reactivation request is provided. The receiving, accessing, comparing, and responding may be performed by a computer without interaction between the former subscriber and a service representative.

Abstract: Responding to an account reactivation request includes receiving an account reactivation request from a former subscriber having a deactivated account and automatically accessing stored account information related to the deactivated account based on the account reactivation request. The stored account information is compared with a reactivation standard to produce a comparison result. Based on the comparison result a response to the reactivation request is provided. The receiving, accessing, comparing, and responding may be performed by a computer without interaction between the former subscriber and a service representative.

Abstract: An electronic medical record module receives data concerning patient medical visits resulting from occupational health or safety incidents processes the data based on pre-defined OSHA logic to automatically identify one or more patient medical visits that are OSHA-recordable, and outputs a plurality of different reports including patient medical visits that are OSHA-recordable. An incident investigation module electronically dispatches an investigator to investigate occupational health or safety incidents, and receives data concerning the investigations including corrective actions to avoid reoccurrence. A data analysis module filters received data at one or more filter levels (e.g. worker characteristics, injury/illness codes, work assignment, time period, etc.) and generates a plurality of reports based on the filtered data.

Abstract: Responding to an account reactivation request includes receiving an account reactivation request from a former subscriber having a deactivated account and automatically accessing stored account information related to the deactivated account based on the account reactivation request. The stored account information is compared with a reactivation standard to produce a comparison result. Based on the comparison result a response to the reactivation request is provided. The receiving, accessing, comparing, and responding may be performed by a computer without interaction between the former subscriber and a service representative.