A61G1/06

Multi-purpose emergency services strap
09764930 · 2017-09-19 ·

A multi-purpose emergency services strap for facilitating lifting, transporting or carrying an individual has a strap body with a plurality of independent loops formed in the strap body. The independent loops include at least two adjacent, proximal leg loops formed in the strap body on either side of the midline, end loops on each end of the multi-purpose emergency services strap, and a plurality of adjacent handles formed in the strap body positioned distal to each of the at least two adjacent, leg loops and proximal to the end loops. The multi-purpose emergency services strap also includes a back strap and attachment loops that can be variously configured for many rescue and transport applications for humans and animals.

Mobile Apparatus With An Integrated Stretcher Apparatus For Patients
20210378889 · 2021-12-09 · ·

A mobile apparatus with an integrated stretcher apparatus for patients has a base having rotatably mounted wheels on a bottom side for moving the base on the ground, a frame which is fastened to a top side of the base and which is open at least on one side, and a stretcher apparatus having segments which are mounted pivotably relative to one another, wherein the segments are configured for folding the stretcher apparatus into a first form, in which all the segments adjoin one another in a plane, and for folding said stretcher apparatus into a second form, in which the stretcher apparatus is packed down, and wherein the stretcher apparatus and the frame are configured to be complementary to one another such that the stretcher apparatus in the second form can be completely introduced into the frame.

Mobile Apparatus With An Integrated Stretcher Apparatus For Patients
20210378889 · 2021-12-09 · ·

A mobile apparatus with an integrated stretcher apparatus for patients has a base having rotatably mounted wheels on a bottom side for moving the base on the ground, a frame which is fastened to a top side of the base and which is open at least on one side, and a stretcher apparatus having segments which are mounted pivotably relative to one another, wherein the segments are configured for folding the stretcher apparatus into a first form, in which all the segments adjoin one another in a plane, and for folding said stretcher apparatus into a second form, in which the stretcher apparatus is packed down, and wherein the stretcher apparatus and the frame are configured to be complementary to one another such that the stretcher apparatus in the second form can be completely introduced into the frame.

ON-BOARD POWER AND REMOTE POWER FOR SUSPENDED LOAD CONTROL APPARATUSES, SYSTEMS, AND METHODS

Load control apparatuses, systems and methods to control a location, orientation, or rotation of a suspended load by imparting thrust with thrusters. The load control apparatuses, systems and method comprise an on-board power supply, a remote power supply, and a power control module. The power control module may distribute a pulse power to the thrusters from the on-board power supply and or from a combination of the on-board power supply and the remote power supply, may manage power between the on-board power supply and the remote power supply, and may to recharge the on-board power supply with the remote power supply.

Patient support apparatus with hydraulic oscillation dampening

A patient transport apparatus with a base, a litter comprising a support surface, and a lift mechanism to facilitate arranging the litter at different heights relative to the base between a plurality of lift configurations including a fully-retracted configuration and a fully-extended configuration. The lift mechanism includes an actuator including a cylinder, fluid reservoir, and a pump driven by a motor to direct hydraulic fluid from the fluid reservoir to the cylinder. A sensor outputs a signal indicative of a magnitude of pressure in the cylinder. A user interface with an input control is provided. A controller determines a target parameter for the motor and, in response to user engagement with the input control, drives the motor at the target parameter to effect movement of the litter relative to the base at a predetermined rate irrespective of a weight of a patient supported on the litter.

Ambulance cot and loading and unloading system

An ambulance cot loading and unloading system for an emergency vehicle includes a base for mounting in the emergency vehicle and an arm mounted for linear movement along the base, wherein the arm configured to support a cot while the cot is being loaded into or unloaded from the emergency vehicle. The ambulance cot loading and unloading system further includes an indicator mounted relative to the arm and a control system, which is in communication with the indicator and configured to generate a status indication of the cot loading and unloading system at the indicator.

Ambulance cot and loading and unloading system

An ambulance cot loading and unloading system for an emergency vehicle includes a base for mounting in the emergency vehicle and an arm mounted for linear movement along the base, wherein the arm configured to support a cot while the cot is being loaded into or unloaded from the emergency vehicle. The ambulance cot loading and unloading system further includes an indicator mounted relative to the arm and a control system, which is in communication with the indicator and configured to generate a status indication of the cot loading and unloading system at the indicator.

AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING-VTOL
20210362855 · 2021-11-25 ·

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.

AIRCRAFT WITH VERTICAL TAKE-OFF AND LANDING-VTOL
20210362855 · 2021-11-25 ·

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.

LITTER PLATFORM SUPPORT AND POSITIONING SYSTEM

The present disclosure includes litter platform support and positioning systems described generally comprising at least one lift column mounted to an interior floor in an emergency vehicle or structure. The lift column is connected to at least one support assembly, the at least one support assembly adapted to receive and position a litter assembly. In some implementations, the support assembly is connected to the lift column and adapted to independently adjust the litter assembly vertically, laterally, longitudinally, and rotate 360°. The litter platform support and positioning system further includes at least one individual motor associated with each lift column which is operatively connected to a drive screw to independently adjust and control the location of each support assembly to individually position a corresponding litter platform assembly.