Disclosed are systems, apparatuses, and methods for and related to dynamic control of torque and or lateral thrust applied to a load suspended load on a suspension cable to thereby achieve a target orientation or position or to otherwise move through use of a hyperparameter, wherein the hyperparameter comprises a normalized moment of inertia, wherein the hyperparameter comprises a ratio of a force command to a thruster and an angular acceleration.

A stretcher loading assembly including a support member operatively attachable to an aircraft floor, an elongate rail member attached to the support member, an elongate traverse beam movably attached to the rail member, and a trolley assembly movably attached to the traverse beam, the trolley assembly including lifting means movable between a lowered position and a raised position, the lifting means adapted to support a stretcher in the raised position, wherein the support member is at least twice as wide as the rail member.

A soft transfer case for biological and chemical material is provided. The transfer case includes a film-laminated, woven textile exterior layer as a pouch resembling an open cylinder. The cylinder is capable of being clamped at each end of the cylinder. A pouch shaped and single open end elastomeric bladder capable of containing biological and chemical material can be contained by the exterior layer. The bladder requires only one seam which is used to permanently seal the open end with the material contained therein. Upon pressurization of the bladder, the exterior layer expands and a restraining force is generated between the textile layer and the clamps.

The invention refers to a VTOL aircraft of the type that uses certain aerodynamic phenomena to increase the lifting force and to reduce the thrust/weight ratio. An aircraft 1 uses a propulsion system 2 consisting of four thrust producing elements, two in front 3 and two in rear 4. Each front thrust producing element 3 contains at least one front rotor 5 operated by at least one front electric motor, fixed on a fuselage 10. Each rear thrust producing element 4 contains at least one rear rotor 7 driven by at least a rear electric motor 8, fixed on the fuselage 10. On the fuselage 10 is attached symmetrically a front wing 12. On the fuselage 10 is attached symmetrically a rear wing 13. The wing 12 and 13 are used also in static conditions respectively in take-off and landing.

Disclosed are a thruster positioning mechanism and a securement mechanism for use in relation to a suspended load control apparatus or system to control a load suspended by a cable from a carrier.

A passenger seat arrangement for installation in an aircraft comprises at least one seating unit comprising a backrest element and a seat element pivotable relative to the backrest element between a resting position and a position of use. The passenger seat arrangement also has a support frame which bears against the at least one seating unit and which is able to be connected in a load-bearing manner to a structure of the aircraft. The support frame has at least one mechanical interface which, in each case, is assigned to a seating unit and is designed to fasten different mutually exchangeable modular units in a releasable and load-transmitting manner to the support frame.

A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.

An enclosed patient suite may include a plurality of suite walls, a patient bed positioned in a patient area defined within the plurality of suite walls, a plurality of medical systems with at least some of the plurality of medical systems mounted to the plurality of suite walls, a plurality of support members coupled to the plurality of suite walls, a plurality of wheels with a particular wheel of the plurality of wheels coupled to a corresponding support member of the plurality of support members, a rail brake configured to engage a floor-mounted rail in a floor of at least one of a cargo hold or a cabin of an aircraft, and a controller coupled to the plurality of medical systems and configured to receive data from and transmit data to the plurality of medical systems. The enclosed patient suite may be dimensioned to fit within the aircraft.

An automated pilotless air ambulance system. The system includes an air vehicle (AV) having a fuselage coupled to a stretcher for carrying a patient. The system is configured to fly the patient from a point of injury to a medical treatment facility. The system also has a plurality of air lift motors for vertically lifting the air vehicle. The system further includes a plurality of air-lift motors coupled to the fuselage forming a low profile. The air lift motors are centralized motors or de-centralized motors for vertically lifting the AV. The system also has an automated life support and monitoring patient suite having a plurality of life support and monitoring devices, including medical supplies. The system additionally has a bidirectional datalink coupled to the air vehicle for executing various functions such as communicating with a patient's or a first responder's mobile device.

A method for providing medical services to a patient, including: receiving a medical service request associated with a patient location; selecting an aircraft, located at an initial location, from a plurality of aircraft based on the patient location and the initial location; determining a flight plan for flying the aircraft to a region containing the patient location; at a sensor of the aircraft, sampling a first set of flight data; at a processor of the aircraft, autonomously controlling the aircraft to fly based on the flight plan and the set of flight data; selecting a landing location within the region; and landing the aircraft at the landing location, including: sampling a set of landing location data; determining a safety status of the landing location based on the set of landing location data; outputting a landing warning observable at the landing location; at the sensor, sampling a second set of flight data; and in response to determining the safety status and outputting the landing warning, autonomously controlling the aircraft to land at the landing location based on the second set of flight data.