WO 2003062057 A1
The invention is an enhanced security cockpit door. The invention provides anti-ballistic protection and intrusion resistance to protect the flight deck from a person or person(s) attempting to take command and control of the aircraft and/or harm to the flight crew. The invention incorporates an access control system that sends both an audible and visual alert to the flight deck when access is requested via the cabin-located access numeric keypad and has received the proper code. The invention provides an adequate time to between 30 and 60 seconds for hte flight crew to accept or deny the requested access. The invention thas been tested and will provide via the proprietary anti-ballistic composite core sheet sufficient ballistic protecton to withstand sey (6) shoots from a 44 mag or 9 mm firearm without penetration. The invention uses high strenght composite construction and proprietary adhesive bonding to provide an intrusion resistant structure that has been tersted to withstand multiple 300 joule impact loads. The invention incorporates a pressure equalization device that has been tested and proven to sense and react as required to provide reliable pressure equalization between compartments. The invention has been designed and tested as required to satisfy a 16 manhour installation time.
Claims (OCR text may contain errors)
(1) An intrusion resistant cockpit door compliant with FAA AC#25.795.1.
(2) An intrusion resistant cockpit door compliant with AC#25.795.1 and current FAA requirements for compartment pressure equalization.
(3) An intrusion resistant cockpit door compliant with AC#25.795.1 and current FAA requirements for emergency egress.
(4) A ballistic resistant door compliant with FAA AC#25.795.1.
(5) A ballistic resistant door compliant with FAA AC#25.795.1 and current FAA requirements for pressure equalization.
(6) A ballistic resistant door compliant with FAA AC#25.795.1 and current FAA requirements for emergency egress.
(7) A ballistic resistant door compliant with FAA AC#25.795.1 using a lightweight, nano-scale composite sheet (provisional patent application #60/327,684 filed on 6 October, 2001) (Anti-ballistic Sheet).
(8) A cockpit door compliant with FAA AC#25.795.1 that is also capable of withstanding ambient temperatures in excess of 300° with degradation of anti-ballistic characteristic.
(9) An enhanced security cockpit door compliant with FAA AC 25.795.1 and capable of being retrofitted to an aircraft within 16 manhours or less.
(10) A cockpit door with access, accept or deny controlled from cockpit pedestal switch by flight crew only.
Description (OCR text may contain errors)
ANTI-BALLISTIC , INTRUSION RESISTANT COCKPIT DOOR
I. TECHNICAL FIELD OF INVENTION
This invention relates to the field of enhanced aircraft security and more particularly anti-terrorist cockpit security issues.
DESCRIPTION OF RELATED ART
Cockpit doors, such as those currently provided by the aircraft manufacturers such as Boeing, Airbus, Canadair and various others are currently constructed of lightweight paper honeycomb materials. This construction provided the necessary frangibility required to satisfy instantaneous pressure equalization between the cockpit and cabin in the event of a decompression event, such as a bird strike to a cockpit window. Although this lightweight construction has performed its intended purpose as an easily-overcome barrier during a decompression event, this has also provided very little in the form of security to the aircraft flight deck and its crew.
As a result of increasing air rage incidents and more importantly the tragic events of September 11 , the immediate need for securing the flight deck has now been recognized and mandated by the F.A.A. and I.C.A.O. What is needed, therefore, is a cockpit door constructed of lightweight materials with sufficient strength to provide anti- ballistic protection up to NIJ Level Ilia (National Institute of Justice) and impact/intrusion resistance suitable to restrain a large human or accelerating drink cart. This impact energy has been determined to be 300 Joules and a suitably enhanced door will be capable of withstanding numerous blows to various pre-determined locations including those deemed to present a potential vulnerability.
Similarly, the anti-ballistic performance of the door will be sufficient to withstand numerous ballistic impacts at various locations and angles including gaps, seams and other areas of perceived vulnerability. In addition to and of equal importance to providing the enhanced anti-ballistic and intrusion resistances, the door has to provide for instantaneous pressure equalization. Instantaneous for the purpose of this requirement is defined as providing a method, or intrinsic design characteristic that allows for pressure equalization between the flight deck and cabin within 15 to 25 milliseconds. The inability to provide equalization between the flight deck and cabin compartments within this time span will result in excessive loading of surrounding structures such as floorboards, bulkheads, and monuments sufficient to exceed the design limits and result in a catastrophic structural failure.
π. BACKGROUND ART
Refer to Drawings attached.
III. DISCLOSURE OF INVENTION
The present invention relates to a lightweight cockpit door that has proven anti- ballistic performance and intrusion resistance in accordance with FAA AC# AC25.795-Z, which incorporates NIJ Level Ilia requirements.
The lightweight cockpit door is constructed with opposing laminated Nomex honeycomb panels of varying thickness and densities that encapsulates a proprietary high-performance, anti-ballistic composite layer (refer to provisional patent application 60/327,684 filed on October 6, 2001) (Anti-ballistic Sheet). This barrier has a weight of 0.9 pounds per ft2. The door is framed with a lightweight, high performance composite laminate frame that provides enhanced stiffness and ease of assembly.
The door has integral venting devices that have been thoroughly tested to satisfy the pressure equalization requirements necessary to avoid catastrophic structural failure of surrounding structures.
The door is also equipped with a mechanical pressure sensing latch that will sense a differential in cabin and cockpit compartment pressurization and release within 2 to 5 milliseconds. This device has the FAA required proven reliability of 10"9 and has over a decade of in-service performance in similar applications. The door panels and frames are joined using an adhesive bonding and fixtured until suitably cured. The gaps and seams are protected using a 1" overlay of anti- ballistic material supported at the gap by a composite laminate channel. The door(s) are attached and supported on one side by a continuous hinge that is attached using composite bonded inserts.
The door is locked using either an electromagnetic lock or electronic solenoid dead bolt. The method of lock control is via an integrated numeric keypad control panel on the cabin side and cockpit pedestal located override control.
A 30 to 60 second delay after the proper code has been entered during which an audible and visual alert will be provided to the flight crew, will allow sufficient time for the crew to either override the entry request or allow entry of the requestor.
A cockpit-side, removable emergency egress provision has been integrated into the design and can be located in the upper or lower door areas. Some aircraft have an observer seat in the flight deck aisle area and for these aircraft, it is necessary to located the egress panel in the upper area of the door as the observer seat would otherwise obstruct emergency egress through the lower door area.
IV. BRIEF DESCRIPTION OF DRAWINGS
A = Removable Anti-ballistic Emergency Egress Pillar
B = Electro-magnetic Remotely Activated Deadbolt Lock
C = Decompression Sensing/Release Latch
D = Vent Doors
E = Anti-ballistic Vent Panel
F = Anti-ballistic Core Material
G = Anti-ballistic Material Gap Overlay
V. BEST MODE FOR CARRYING OUT INVENTION
The best mode for carrying out this invention is to have a shop or facility that is equipped with specialized equipment necessary to fabricate and process advanced composite materials. It is further recommended that suitably trained personnel are employed of varying disciplines necessary to accomplish composite laminate lay-up, cutting, adhesive bonding, and blueprint reading. Once the above-referenced equipment and personnel are gathered, the detailed design and assembly drawings along with the process guidelines incorporate information sufficient for these personnel to fabricate and assemble the cockpit door assembly.
VI. INDUSTRIAL APPLICABILITY
This invention is specifically applicable to aircraft including but not limited to:
(1) Commercial Aircarriers
(2) Commercial Airfreight and Cargo Carriers
(3) Regional/Commuter Airlines
(4) Charter and Fractional Ownership Aircraft
(5) Private and Corporate Aircraft
(6) Military Transport Aircraft
(7) Any manned flying machines that are equipped with a separate cockpit and cabin area that could be possibly overtaken and used as a weapon.