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Title:
SECURITY COCKPIT DOOR; INTEGRALLY VENTED, PRESSURE EQUALIZED
Document Type and Number:
WIPO Patent Application WO/2003/089300
Kind Code:
A1
Abstract:
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 of between 30 and 60 seconds for the flight crew to accept or deny the requested access. The invention has been tested and will provide via the proprietary anti-ballistic composite core sheet sufficient ballistic protection to withstand six (6) shoots from a 44 mag or 9 mm firearm without penetration. The invention uses high strength composite construction and proprietary adhesive bonding to provide an intrusion resistant structure that has been tested to withstand multiple 300 joule impact loads. The invention incorporates a unique, integral vent system that provides continuous, uninterrupted pressure equalization between compartments with no need for pressure differential sensors, latches or any type of mechanical device. The invention has been designed and tested as required to satisfy a 16 manhour installation time.

Inventors:
Squires, Stephen B. (5901 Pine Valley, Flower Mound, TX, 76022, US)
Application Number:
PCT/US2002/012054
Publication Date:
October 30, 2003
Filing Date:
April 15, 2002
Export Citation:
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Assignee:
USDR AEROSPACE LTD. (7175 Research Rd, Mansfield, TX, 76063, US)
Squires, Stephen B. (5901 Pine Valley, Flower Mound, TX, 76022, US)
International Classes:
B64C1/14; B64D45/00; (IPC1-7): B64D45/00; B64C1/14
Foreign References:
US3704845A1972-12-05
US5085017A1992-02-04
US4033247A1977-07-05
US32768401P2001-10-06
Attorney, Agent or Firm:
Wells, Gaddy (7175 Research Rd, Mansfield, TX, 76063, US)
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Claims:
CLAIMS
1. (1) An intrusion and ballistic resistant cockpit door compliant with AC#25. 795.1 that provides continuous, uninterrupted pressure equalization through an integral vent system without sensors or latches. (2) An intrusion resistant cockpit door compliant with FAA AC#25. 795.1. (3) An intrusion resistant cockpit door compliant with AC#25. 795.1 and current FAA requirements for compartment pressure equalization. (4) An intrusion resistant cockpit door compliant with AC#25. 795.1 and current FAA requirements for emergency egress. (5) A ballistic resistant door compliant with FAA AC#25. 795.1. (6) A ballistic resistant door compliant with FAA AC#25. 795.1 and current FAA requirements for pressure equalization. (7) A ballistic resistant door compliant with FAA AC#25. 795.1 and current FAA requirements for emergency egress. (8) A ballistic resistant door compliant with FAA AC#25. 795.1 using a lightweight, nanoscale composite sheet (provisional patent application #60/327, 684 filed on 6 October, 2001) (Antiballistic Sheet). (9) 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 antiballistic characteristic. (10) 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. (11) A cockpit door with access, accept or deny controlled from cockpit pedestal switch by flight crew only.
Description:
SECURITY COCKPIT DOOR ; INTEGRALLY VENTED, PRESSURE EQUALIZED 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 Illa (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 importallçe, ViU"Iy"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 results 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.

II. BACKGROUND ART Refer to Drawings attached.

III. DISCLOSURE OF INVENTION Summary 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 Illa 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 architecture that have been thoroughly tested to satisfy the pressure equalization requirements necessary to avoid catastrophic structural failure of surrounding structures.

This unique proprietary integral vent architecture provides for continuous pressure equalization between compartments while also providing ballistic and intrusion protection.

The door panels and frames äre JUe U Ubllly 1n adhesive bonding and fixtured until suitably cured. The gaps and seams are protected using a 1"wide 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 = Ballistic Sheet Core Material B = Remotely Activated Locking Mechanism C = Integral, offset, anti-ballistic, continuous pressure equalization vent feature D = Electronic, spring-loaded solenoid dead bolt latch 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.

Vl. INDUSTRIAL APPLICABILI i r 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.