On-board emergency response system for a vehicle

Abstract

An on-board emergency response system for a vehicle include a drone being integrated with a vehicle to become separated only when the vehicle is in trouble or experiencing difficulties. Activation of the drone may be from inside the vehicle or remotely via a communication link. The drone is automatically ejected or activated when abnormal conditions inside or outside the vehicle are detected. The drone may provide a backup communication when needed. Once the drone is ejected from the plane, it then follows the vehicle from above at a predetermined distance. It also sends its location, video and images taken inside and outside the vehicle to the command center. If a disaster is inevitable, the drone then tracks the vehicle all the way to its destination. Since the vehicle's actual location is immediately known to the central command, the rescue team can take off in no time, skipping the search altogether.

Claims

1. An emergency response system for an airborne manned aerial vehicle (MAV), comprising; an unmanned aerial vehicle (UAV) having a physical connection and a wireless connection with the manned aerial vehicle, and also having a wireless communication connection to an air traffic control center; a manual and an automatic UAV launch trigger connected to a plurality of sensors enabled to detect an emergency situation in the MAV; wherein upon detection of the emergency situation by any one of an occupant of the MAV and the sensors, the manual launch trigger is configured to be initiated manually by the occupant and upon at least one of the sensors sensing the emergency situation, the automatic launch trigger is configured to be initiated automatically and once the UAV is launched it communicates at least location and flight conditions to the air traffic control center, wherein the UAV is automatically launched from the MAV when the sensors detect the emergency situations including a cockpit door tampering or breach, pilot error, and technical and mechanical failures of the MAV.

2. The system of claim 1, wherein the UAV would automatically be ejected from said airborne manned aerial vehicle (MAV) if the MAV is in an upside-down position or vice versa.

3. The system of claim 1, wherein the UAV would automatically be ejected from said flying airplane if a fire is detected within or on the MAV.

4. The system of claim 1, wherein the UAV establishes a three-way communication between the MAV, UAV and air traffic control center immediately after being ejected from the MAV.

5. The system of claim 1, wherein the UAV is configured to perform a plane's remote diagnostic after being separated from said flying plane.

6. The system of claim 1, wherein the UAV is equipped with a tracker system for the MAV enabling the UAV, after launch to track location of the MAV in air, land or water and communicate that location to the air traffic control center.

7. The system of claim 1, wherein the UAV is launched in an event the MAV becomes undetectable on a tracking or radar at the air traffic control center during flight.

8. The system of claim 1, wherein the emergency situation is remotely diagnosed by the air traffic control center for human error, and attempt a remote fix via the UAV.

9. The system of claim 1, wherein the UAV is separated from an immediate location of the MAV to rove above and track the MAV while sending the MAVs current location to the air traffic control center, enabling, by the air traffic control center access and retrieval of data, images, and video from inside and outside the MAV.

10. The system in claim 1, wherein the UAV tracks position and condition of the MAV until the MAV is landed.

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

(1) The drawings constitute a part of this specification and include exemplary embodiment to the invention, which may be embodied in various forms. It is to be understood that in some instances various aspects of the invention may be shown exaggerated or enlarged to facilitate an understanding of the invention.

(2) With the above and other related objects in view, the invention consists in the details of construction and combination of parts as will be more fully understood from the following description, when read in conjunction with the accompanying drawings in which:

(3) FIG. 1 illustrates a drone activation control system from an air vehicle according to one embodiment of the present invention.

(4) FIG. 2 illustrates a 3D view of a drone.

(5) FIG. 3 illustrates an air vehicle with a drone housing.

(6) FIG. 4 illustrates an air vehicle with an open drone housing showing the drone itself.

(7) FIG. 5 illustrates an air vehicle showing a drone being ejected from the air vehicle.

(8) FIG. 6 illustrates multiple positions where a drone can be automatically ejected from the air vehicle.

(9) FIG. 7 illustrates a 3-way communication between an air vehicle, a drone, and a command center.

(10) FIG. 8 illustrates a view of the air vehicle's cockpit.

(11) FIG. 9 illustrates a view of the air vehicle's passenger's area.

(12) FIG. 10 illustrates a drone roving over an air vehicle crashed on water.

(13) FIG. 11 illustrates a drone roving over an air vehicle crashed on land.

(14) FIG. 12 illustrates a drone providing lightning over a water crash site at night time.

(15) FIG. 13 illustrates a drone providing lightning over a land crash site at night time.

(16) FIG. 14 illustrates a view showing images sent from the drone to the control command center with radar indicating the exact location of the crash.

(17) FIG. 15 illustrates a view of the drone's solar power capability.

(18) FIG. 15A illustrates view detailing the drone's thin solar cells.

(19) FIG. 16 illustrates a view of the drone landing on water because of lack of power.

(20) FIG. 17 illustrates a view of the drone landing on land because of lack of power.

(21) FIG. 18 illustrates a view where the water's search and rescue team arrive at the scene.

(22) FIG. 19 illustrates a view where a reconnaissance airplane from the land's search rescue team arrives at the scene.

(23) FIG. 20 shows a crashed aircraft being retrieved from the water by a heavy lifting helicopter.

(24) FIG. 21 depicts the drone roving over a remote all-terrain vehicle.

(25) FIG. 22 depict a drone roving over a ship at sea.

DETAILED DESCRIPTION OF THE INVENTION

(26) The present invention now will be described more fully hereinafter with reference to the accompanying drawings, in which some, but not all embodiments of the invention are shown. Indeed, these inventions may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will satisfy applicable legal requirements. Like numbers refer to like elements throughout.

(27) The system of the present invention applies to any type of vehicle, such as an air vehicle, boat, ship, train, tractor trailer, bus or the like. The embodiments described below, however, are directed toward specific embodiments of a system to help locate and assist a distressed airplane. However, the methods and systems of the present invention apply equally to any other type of vehicle.

(28) The present invention will now be described by referencing the appended figures representing preferred embodiments. The embodiment of a system 10 for helping and locate a distressed vehicle includes at least one engagement element 12 and at least one processing element 14, as shown in the embodiments of FIG. 1. An engagement element 12 may be any type of element that initiates the launch of the location system of a vehicle, such as a drone. For example, an engagement element 12 may transmit a signal to the processing element 14 directing engagement of launching the drone. As such, the engagement element may be, but is not limited to, a button, switch, lever, or the like, or any other device capable of transmitting a command to the processing element 14, such as a keyboard, a voice signal receiver, a touch-screen, or a selection device such as a mouse in conjunction with a display. For instance, the location control system 10 may be activated automatically, as represented by box 16 of FIG. 1. In one embodiment, the engagement element 12 may be a sensor or the like that automatically transmits an engagement signal to the processing element 14 upon sensing a particular event. One such event can be the case where the air vehicle or aircraft is in an awkward or abnormal position during the flight as shown in FIG. 6. Such sensors may also be located anywhere in the vehicle 40 where a type of threat to the security of the vehicle or its passengers or other contents may be sensed. For instance, in an aircraft, an engagement sensor may be located proximate to the door of the cockpit, and the sensor may be programmed to transmit an engagement signal to the processing element when there is an attempt to forcibly open the door, such as repeated poundings on the door, and or when an aircraft is in an upside-down position or vice versa. In the case of a cockpit door, the sensor(s) may have a minimum force threshold, such that force applied to the door must exceed the threshold before the automatic drone launch system can be automatically activated. Therefore, at least most inadvertent applications of force on the door by people or objects will not cause the system to automatically engage. In addition to or instead of the automatic engagement element(s) 16, the system 10 may include manual engagement element(s) 18, such as buttons, switches or the like, that authorized personnel, such as the pilots of an aircraft may actuate if a threat is detected. Thus, one or more manual and/or automatic engagement elements may be located onboard vehicle 40, such as within and/or proximate the cockpit of an aircraft as represented by boxes 16 and 18 of FIG. 1.

(29) Furthermore, one or more locations outside vehicle 40, i.e., one or more remote international locations from the Coast Guard, the Air Force, or the Navy, on a global scale, but in communication with vehicle 40, as shown in FIG. 7, may include an engagement element, such that if a signal or other communication is received at the remote location that indicates a distress situation, or the security of vehicle 40 may be in jeopardy, the engagement element may activate or launch drone 14, as shown in FIG. 5, from the remote location, as represented by box 20 of FIG. 1 so as to help in correcting any errors if possible, or in determining the gravity of the situation onboard vehicle 40. Personnel and/or equipment at the remote location may monitor the aircraft and may be capable of detecting certain events using onboard Wi-Fi security cameras as represented by box 28, 30, and 32 of FIG. 1, and also depicted in FIGS. 8, and 9. If processing element (drone) 14 is activated because of a vehicle malfunctions such as engine failure, fire, and a catastrophe is therefore imminent, then the drone 14 should be automatically ejected from the air vehicle and be able to track vehicle 40 all the way to the end, using a predetermined distance above vehicle 40 as shown in FIG. 5.

(30) After drone 14 is launched from vehicle 40, images showing a glimpse of the condition of vehicle 40 from the inside out, including the cockpit, can be sent through the drone to the special unit team on the ground as shown in FIGS. 8 and 9.

(31) Since the drone is designed to follow vehicle 40 where ever it goes once launched, it might end up floating where ever vehicle 40 may be landing, above water or land. If above the water, drone 14 is also equipped with water sensor that would prevent it from chasing vehicle 40 deep under the ocean. Instead, it will keep tracking vehicle 40 from above at a predetermined distance from the water, as shown in FIG. 10, as the current continues to drag the plane deeper. If sensor's depth limit is reached and the search team is still not at the scene, drone 40 would stay still, where the depth limit was reached. If crash site is on land, drone 14 is equipped with heat and smoke sensors to keep itself far above the crash site as depicted in FIG. 11.

(32) Also, drone 14 has the capability to provide light to the crash sites from above, either on water or on land, using its onboard powerful flash light, as shown in FIGS. 12 and 13.

(33) Drone's 14 Wi-Fi cameras, as depicted in box 30 of FIG. 1, with night vision capability when needed, can transmit live video images to remote location 20 any time of the day, giving a glimpse of the state of vehicle 40 just moment after the crash, as shown in FIG. 14.

(34) Beside long-lasting batteries, drone 14 is also equipped with mini solar cell 42, power backup in the event more time is needed for the rescue team to arrive, providing that sunlight is available as shown in FIG. 15A. In the event drone's battery reaches its lowest preset level, it would automatically be switched to a backup solar power 42. The idea is to maintain sufficient power on board for communication purpose.

(35) In the event solar power 42 is unavailable, and the crash is on land, then drone's 14 onboard emergency parachute 110 would automatically be deployed. Drone 14 will then be programmed to land itself away from the crash site, as shown in FIG. 18. However, if the crash site is on water, drone's 14, built-in inflatable raft 100 would also automatically be deployed, so drone 14 might float over the water surface without the risk of being submerged, as illustrated In FIG. 16.

(36) Now since the crash site can be easily located, contrary to the conventional system, first response team can be at the scene quicker for a preliminary assessment, as shown in FIGS. 17 and 19.

(37) On the other hand, the search and rescue team have a better chance in saving some lives by being on the crash site sooner, as depicted in FIG. 20.