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58 results about "Emergency procedure" patented technology

An emergency procedure is a plan of actions to be conducted in a certain order or manner, in response to a specific class of reasonably foreseeable emergency, a situation that poses an immediate risk to health, life, property, or the environment. Where a range of emergencies are reasonably foreseeable, an emergency plan may be drawn up to manage each threat. Most emergencies require urgent intervention to prevent a worsening of the situation, although in some situations, mitigation may not be possible and agencies may only be able to offer palliative care for the aftermath. The emergency plan should allow for these possibilities.

Temporarily installed aircraft observer door plug, chair, sonotube ejection and control system

The system and apparatus of the present invention is generally comprised of a non-dedicated, temporarily installed, aircraft observer bubble door, chair, sonotube ejection system, mission electronics LRU rack and workstation assembly which are affixed to the Air Deployment System (ADS) rails, cargo tie down “D” rings, seat belt restraint ring bolt sockets, and litter bar of a host aircraft, thereby precluding the requirement for dedicated airframe modifications. One embodiment of the present invention also utilizes a multi-axis, articulated, foldable chair temporarily installed in conjunction with a segmented or one piece pressurized observer bubble door plug and door retraction system. The door plug assembly is designed to accommodate the simultaneous use of a sonotube stores launch system, a missile defense system, and an observer bubble window. The door plug also accommodates fitment around the envelope of a special mission strut which extends through the interior to the exterior of the host aircraft beneath the door plug's lower periphery. The door plug is also moveably mounted within a temporary retraction rail system which interfaces mechanically to the permanent door retraction rails and the aircraft floor or ADS rail system. When the host aircraft is not equipped with an ADS rail system, the retract rails, chair stanchion, mission electronics racks, and workstation assemblies are mounted to an adaptive floor plate (AFP) which can be modified to interface with various cargo floor “D” rings, or other cargo tie down mechanisms and bolt patterns such that several types of dissimilar aircraft can utilize the subject apparatus either with or without ADS rails installed. Once installed the subject apparatus can be stowed outboard of the fuselage cargo transit envelope to permit use of the ADS rail system in-flight, without affecting normal air drop operations, crew egress, the flight performance envelope, or emergency procedures of the host aircraft.
Owner:1281329 ALBERTA

Emergency patient emergency rescue system based on mobile monitoring car

The invention discloses an emergency patient emergency rescue system based on a mobile monitoring car. The mobile monitoring car is connected with a community user medical device and a hospital information system through a wireless network, obtains sign information of monitored users and related information of hospitals in real time, and monitors the health states of the users; the mobile monitoring car instantly enter the emergency rescue state when the users send out distress call information or when the medical device for monitoring the users automatically gives an alarm, so that the patients are automatically positioned and tracked in real time; the mobile monitoring car obtains information of the patients through electronic medical records, comprehensively evaluates all collaboration hospitals for the patients who need to be admitted to hospitals, sends the patients to different hospitals to be treated, orders operations and sends all the information of the patients to the hospitals, so that medical workers can make rescue preparation in advance. Doctors and experts in the hospitals can know illness states of the patients and participate in emergency work as early as possible, so that emergency procedures are optimized, and the therapeutic effect is improved.
Owner:SOUTHEAST UNIV

Improvements to body area networks

A method of declaring an emergency condition in a wireless sensor network, the wireless sensor network comprising a plurality of devices (10, 11, 12) including sensors (11) arranged for monitoring at least one living body or other entity, the method comprising steps of: sensing a value of parameter related to the living body by one of the sensors (11); wirelessly transmitting information by said sensor to another device (10) in the network; determining existence or non-existence of an emergency condition affecting said living body by using said sensed value or said transmitted information; and declaring existence or non-existence of the emergency condition to at least one other device (e.g. 10) in the network. The determining step may be carried out in any of the sensor (11), a coordinator (10) of the wireless sensor network, or a central monitor (12) in communication with the coordinator. The declaring step may be performed by setting a frame control field of a frame-based wireless sensor network to a value predefined as denoting an emergency frame. An acknowledgement frame may be used by the recipient to acknowledge receipt of the emergency declaration, after which an emergency procedure is followed. The emergency procedure can involve, for example, increasing the bandwidth allocated to the sensor so as to ensure reliability of subsequent information from the sensor. The method may be applied, for example, to monitoring of patients in a hospital using MBANs operating in accordance with IEEE 802.15.6.
Owner:FUJITSU LTD

Aircraft based non-dedicated special mission pod mounting apparatus

The system and apparatus of the present invention is generally comprised of a non-dedicated, temporarily installed, airborne special mission payload mounting system which is mechanically interfaced to the Air Deployment System (ADS) rails of a host cargo aircraft. Where a host aircraft does not possess ADS rails, an Adaptive ADS rail section typical of those used by the host aircraft, is installed to the existing cargo floor “D” rings using adjustable cam locks familiar to those skilled in the art of aircraft cargo restraint systems. Where the host aircraft does not have the required cargo “D” rings installed they are then temporarily installed within the “D” ring bolt sockets to enable the aircraft to accommodate mounting of the Adaptive ADS rail section plate. Once the ADS rail section and plate are installed, an Adaptive Mounting Plate (AMP) is placed over the ADS rail section and restrained in position by using multiple bolts, and the cargo “D” rings integral to the ADS rail securing the AMP in position using adjustable cam locks hooked through the ADS rail “D” rings thereby precluding the requirement for a load transfer (torque) pallet, or dedicated airframe modifications. Once the AMP is secured, an articulated or fixed position strut can be attached to it through the opened side doorway without removing the original door. Once the fixed position or articulated strut is bolted to the AMP, a one piece or segmented two piece pressurized door plug indented along its lower periphery to accommodate the protruding form factor of the fixed position or articulated strut is installed within the vacant doorway above the strut providing an airtight seal and thereby permitting pressurization of the aircraft. In-flight dynamic loads exerted upon the various mission payload pods are transferred through the strut to the interior ADS rail by the AMP and to various cargo “D” rings located on the aircraft floor by a plurality of removable Load Transfer Braces (LTB) hinged to the inboard side of the AMP which in turn transfers said dynamic loads to a Floor Loads Plate (FLP) secured to multiple cargo tie down “D” rings on the floor of the host aircraft by means of adjustable cam locks. Said removable load transfer braces being able to rapidly disconnect from the adjustable cam locks, “D” rings, and FLP for stowage in the vertical position, outboard of the cargo transit envelop as to permit in flight air drop operations. In flight, the articulated strut assembly can be extended below the fuselage to achieve a 360 degree unobstructed field of view (FOV) for a given payload, or retracted into the fuselage to change sensor payloads or re-load jettisonable stores. The preferred embodiment of the present invention can be installed or removed in minutes, does not interfere with crew egress, the aircraft flight performance envelope, or emergency procedures of the host aircraft while installed and further possesses redundant primary drive retraction systems along with a manual retraction system, and payload jettisoning system to preclude any danger in landing the aircraft should there be a problem retracting the various mission payloads.
Owner:1281329 ALBERTA
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