| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | Aircraft floor to fuselage attachment | US11683228 | 2007-03-07 | US07721992B2 | 2010-05-25 | Robert D. Keeler, Jr.; Albert L. Neal |
| A floor to fuselage attachment structure incorporates a truss having an upper angled attachment engaging the floor proximate an edge and extending at an angle upward from the floor edge to attach to the fuselage. Additionally, the truss includes a lower angled attachment engaging the floor proximate the edge and extending at an angle downward to attach to the fuselage. The upper and lower angled attachments support the floor with the edge spaced from the fuselage and further have a plurality of apertures for providing airflow between a first volume above the floor and a second volume below the floor. | ||||||
| 102 | Method and apparatus for extending flight crew's time of useful consciousness after decompression | US11244535 | 2005-10-06 | US07624732B2 | 2009-12-01 | Bradley J. Mitchell; Trevor M. Laib |
| Systems and methods are provided for regulating the pressure within an aircraft flight crew area during and/or after a decompression event. For example, an aircraft may include a flight crew area, at least one pressure sensor for detecting the pressure of the atmosphere within the flight crew area, and at least one regulated decompression panel that is operatively associated with the pressure sensor, for regulating the pressure within the flight crew area during and/or after a decompression event. | ||||||
| 103 | Operation mechanism for activating a deceleration device | US11715840 | 2007-03-08 | US07571877B2 | 2009-08-11 | Clive French; Nick Chignell-Stapleton |
| An operation mechanism adapted for activating a deceleration device for decelerating an opening movement of a door. The operation mechanism features a first mode of operation and an second operation mode. In the first mode of operation the operation mechanism allows free rotation of the door, when the operation mechanism is loaded by an impulse of the door below a predetermined threshold value. In the second mode of operation when the operation mechanism is loaded by an impulse of the door above the predetermined threshold value the operation mechanism decelerates free rotation of the door by connecting the door to the deceleration device which will then decelerate the acceleration of the door. | ||||||
| 104 | Decompression Device With Adjustable Release Pressure | US12334856 | 2008-12-15 | US20090159748A1 | 2009-06-25 | Thomas Treimer; Ingo Hildebrand; Hubert Stutzle |
| The invention relates to a decompression element for pressure equalisation in a cabin of an aircraft, with a decompression element frame (4), a flap (2) and a hinge element or at least one bearing element (6′) for fitting the flap to the decompression element frame (4). The hinge element or the bearing element (6′) can be produced from a plastics material. A decompression device for decompressing a cabin area comprises a decompression device frame (17), a first opening (19) which enables a flow to take place between a line (16) of an air-conditioning system of the aircraft and the interior space of the decompression device. A second opening (14) of the decompression device enables a flow to take place between the cabin area and the interior space of the decompression device. The decompression element with the flap (2) is disposed at a third opening. | ||||||
| 105 | Reduced Door Opening Force and Enhanced Security Flight Deck Door Mechanism | US11923238 | 2007-10-24 | US20080135684A1 | 2008-06-12 | James J. Kunda; Shannon J. Kupfer; Michael E. Renzelmann |
| An aircraft door mechanism includes a solenoid connected to a support assembly. The solenoid displaces the latch pin between a solenoid energized and a solenoid de-energized position. A catch assembly rotatably connected to the support assembly is positioned to engage a 3½ degree or less taper portion of the latch pin in the solenoid energized position. When the latch pin moves to the solenoid de-energized position, a latch bolt supported by the door rotates the catch assembly. The latch bolt includes a distal bulbous end which multiplies the force applied to the door to rotate the catch assembly. If the latch pin is extended, a substantially greater force is required to force the latch pin to the solenoid de-energized position owing to the reduced taper of the latch pin. Authorized door entry is therefore easier and unauthorized door entry is made more difficult. | ||||||
| 106 | Pressure sensing dead bolt | US10491977 | 2002-10-04 | US07255376B2 | 2007-08-14 | John D Pratt; Timothy S. Rozema |
| An apparatus, system and method including a latching device for displaceably retaining a panel relative to a frame. The latching device includes at least a bolt which is carried on the latching device and is operatively associated with the panel to prevent disengagement of the panel. The latching device includes at least one pressure responsive device operatively coupled to the bolt to retain the bolt in a desired position and release the bolt when a predetermined pressure differential occurs relative to two, generally opposite, sides of the panel or when a pressure decrease occurs on one side of the panel. | ||||||
| 107 | Device for warning of differential pressure during the opening of a pressurized closing device pertaining to an opening in the fuselage of an aeroplane | US10526424 | 2003-09-01 | US07207524B2 | 2007-04-24 | Carsten Puschmann; Wolfgang Lessat; Jens Hasse |
| An apparatus warns of differential pressure during the opening of a pressure-loaded door that closes an opening in an aircraft fuselage. An air guide passage extends from the side with higher pressure to the side with lower pressure. The air guide passage is closeable by a valve that is controllable with a control lever operatively Connected to a door opening mechanism. When there is a differential pressure between the two sides, upon opening of the valve the apparatus produces an acoustic signal as a differential pressure indication that is independent of a supply system and serves as a warning signal for the operator of the aircraft door. | ||||||
| 108 | Flight deck security pocket door system | US11026889 | 2004-12-30 | US20060145007A1 | 2006-07-06 | David Melberg; Jonathan Barrows |
| A security pocket door traverses within a security bulkhead wall that defines a pocket, within which the pocket door traverses, and a through passage to permit people, carts and luggage to pass. The pocket door has an upper door track mechanism and a lower door track mechanism that engages a corresponding upper and lower track mechanism of the bulkhead and floor, respectively. The bulkhead door locks with at least one solenoid with a locking pin that engages a hole in a tab of the pocket door. The locking pin creates a magnetic field with a magnet located in the tab to send a signal to the flight deck in order to indicate a closed and locked or an unlocked pocket door condition. When the pocket door is in its closed position, the door perimeter overlaps the bulkhead on at least three sides of the door and also overlaps with the floor. | ||||||
| 109 | Insulating baffle for a floor shear truss | US10807087 | 2004-03-23 | US07007892B2 | 2006-03-07 | Gregory A. Tubbs |
| An insulation baffle for a mobile platform. The baffle is secured to a structure separating different lobes of the mobile platform. The baffle includes a main body portion and at least one blow out portion. A perimeter of the blow out portion is defined by at least one recess. The recess also forms a web portion that connects the blow out portion with the main body portion. A depth of the recess is predetermined such that the web portion formed by the recess will sever when a pressure differential between the different lobes exceeds a predetermined threshold. When the web portion severs at least a section of the blow out portion separates from the main body portion to air to pass between the lobes so that the pressure differential is reduced to approximately zero. | ||||||
| 110 | Device for warning of differential pressure during the opening of a pressurized closing device pertaining to an opening in the fuselage of an aeroplane | US10526424 | 2003-09-01 | US20060006285A1 | 2006-01-12 | Carsten Puschmann; Wolfgang Lessat; Jens Hasse |
| In an apparatus for warning of differential pressure during the opening of a pressure-loaded closure device (1) of an opening in the aircraft fuselage by means of an opening mechanism (4; 100; 105), the invention exists in that an air guide passage is provided from the side with higher pressure (passenger cabin P) to the side with lower pressure (outside environment A). The air guide passage is closeable by a valve (5; 209), whereby it is controllable with a control lever (4; 208) placed in operative connection with the door opening mechanism, and produces an acoustic signal upon opening of the valve (5; 209) and an existing differential pressure. With such a warning apparatus, a differential pressure indication independent of a supply system is provided and serves as a warning signal for the operator of an aircraft door. Thereby, the differential pressure indication is directly coupled to the action of the operator. Moreover, false alarms are excluded and the warning apparatus achieves a very high reliability. | ||||||
| 111 | Door reinforcement system | US10385928 | 2003-03-11 | US06938376B2 | 2005-09-06 | Magdy Morssi Youssef |
| A door reinforcement system comprises two pairs of assemblies, each assembly having subassemblies on the inside and the outside of the door. The inside subassemblies include a plate with a channel for housing a sliding bolt, and may include three subassemblies with two bolts, each of which spans a subassembly attached to the wall structure and a subassembly attached to the door. By providing the at least two pairs of assemblies, a better reinforment is obtained by reinforcing against the torque that would be present with a single dead bolt. | ||||||
| 112 | Apparatus for controlling the ingress and egress to and from an operator's compartment | US10358408 | 2003-02-04 | US06925756B2 | 2005-08-09 | Bernd Roessner; Wilfried Sprenger |
| The ingress to and egress from an access restricted compartment, such as the cockpit in an aircraft, is controlled by a revolving gate (1) rotatably mounted in a stationary gate frame (2). The revolving gate (1) has a single gate opening (11) and is rotatable about its central longitudinal axis through predetermined or preselected angular sectors to bring the gate opening (11) either into alignment with any one opening (21) of at least two frame openings (21) at a time, to provide ingress or egress, or to cause said single gate opening (11) to face a wall (2A) of said stationary gate frame (2) or a closed door (51) in said stationary gate frame (2) to close the gate (1). In the closed position of the gate (1) escape from the gate (1) is prevented by locking the gate in its closed position by at least one arresting bolt that is electrically controllable. The atmosphere in the revolving gate (1) is also controllable for incapacitating any unauthorized intruder. | ||||||
| 113 | Pressure responsive blowout latch | US10939659 | 2004-09-13 | US20050116100A1 | 2005-06-02 | John Pratt; Timothy Rozema; Frank Jackson; William Bourne; Manuel Hernandez |
| An apparatus, system and method including a latching device for displaceably retaining a panel relative to a frame. The latching device includes at least a bolt which is carried on the latching device and is operatively associated with the panel to prevent disengagement of the panel. The latching device includes at least one pressure responsive device operatively coupled to the bolt to retain the bolt in a desired position and release the bolt when a predetermined pressure differential occurs relative to two, generally opposite, sides of the panel or when a pressure decrease occurs on one side of the panel. | ||||||
| 114 | Pressure responsive blowout latch with reservoir | US10462144 | 2003-06-16 | US06866227B2 | 2005-03-15 | John D. Pratt; Timothy S. Rozema |
| A method and apparatus for maintaining a panel in a closed position and releasing a panel upon application of changes resulting from a pressure change in an area adjoining the panel. The apparatus includes a latch mechanism attached to a structure having a bolt for engaging corresponding panel. The latch mechanism may be retained on the corresponding panel with the bolt engaging the structure. A pressure responsive device is provided to detect a change in pressure on one side of the panel and facilitating release of the bolt in response to a pressure change of a predetermined range or force. The latch mechanism and pressure responsive device vent to or communicate with only one side of the panel. A reservoir on one side of the panel communicates with a pressure responsive chamber of the pressure responsive device. The reservoir is generally on the same side of the panel to provide a pressure volume which is generally isolated from ambient pressure, such as during a decompression event. The method includes a method of maintaining a latch mechanism in a closed position subject to a pressure change, including sensing the pressure change on only one side of the panel. | ||||||
| 115 | Integrated cockpit door lock and access system | US10255916 | 2002-09-26 | US06830217B2 | 2004-12-14 | Sami Movsesian; Binh C. Truong; Stephen A. Wlles; Ravinder Jaln; Dinanath R. Gharmalkar; Danny Valdez; Stephen A. Kelekian; Gary L. Bartz |
| An electromechanical flight deck door locking system capable of functioning to keep a cockpit door locked in the event of an interruption in electrical power to the system. The flight deck door locking system includes a locking assembly including a locking component and a manually graspable handle for displacing the locking component. Further, the locking system includes an electronic control panel configured to receive data from an individual seeking access to the cockpit and for electrically locking and unlocking the locking assembly. The locking system also includes a mechanical locking assembly, such as a key lock, whereby a user can use a key to lock and unlock the door if electrical power to the system is unavailable. | ||||||
| 116 | Airplane door lock system | US10691386 | 2003-10-22 | US06817577B2 | 2004-11-16 | Robert M. Semprini |
| A door lock system for an airplane is operative to alternately operate spaced doors to provide controllable entry into a restricted area located between the spaced doors. | ||||||
| 117 | Cockpit door of aircraft | US10735624 | 2003-12-16 | US20040144895A1 | 2004-07-29 | Hironobu Takahama |
| The cockpit door has a hinge on one side and a latch device on the other side that can be operated only from the cockpit side. To the inner side of the door panel is mounted a reinforcement member 100 having a body formed by laminating layers of aromatic polyamide fiber sheets and thermoplastic adhesive and subjecting the same to hot pressing to form an integral member. Mounting portions 150 and 160 are formed to the rim portion of the reinforcement member body 110, and rivet inserting holes 180 are machined to the portions. The mounting portions are bent by 90 degrees, and fixed to a frame using rivets. | ||||||
| 118 | Pressure rate of change sensitive latching method and apparatus | US10300681 | 2002-11-19 | US06745982B2 | 2004-06-08 | Michael G. Lehmann |
| A rate of change in pressure identifies a rapid decompression event in an aircraft, and automatically unlatches a door to allow rapid equalization of pressure throughout the aircraft, allowing for use of doors with greater structural integrity then in current use. | ||||||
| 119 | Airplane door lock system | US10691386 | 2003-10-22 | US20040089766A1 | 2004-05-13 | Robert M. Semprini |
| A door lock system for an airplane is operative to alternately operate spaced doors to provide controllable entry into a restricted area located between the spaced doors. | ||||||
| 120 | Ballistic resistant flight deck door assembly having ventilation feature | US10162450 | 2002-06-04 | US06702230B2 | 2004-03-09 | Sami Movsesian; Stephen A. Wiles; Dinanath Gharmalkar; Behrooz Afghani; Jerry D. Smets; Eisen Kaoru Inouye |
| A ballistic resistant flight deck door assembly for an aircraft is disclosed that also enables pressure equalization within the aircraft in the event of a sudden loss of cabin pressure within the flight deck or cabin. The door assembly includes a door having a plurality of spaced apart panels of ballistic material and a honeycomb support panel. A ventilation area is formed in the door by a plurality of apertures in each of the ballistic panels that are arranged such that no two apertures of the two ballistic panels are perfectly aligned with each other. The blowout panel and ventilation area therefore allows airflow through the door to help equalize pressure within the flight deck in the event of a loss of depressurization of the flight deck without compromising the door's ability to provide ballistic protection for the occupants in the flight deck. | ||||||
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