Abstract: The invention provides an air chiller unit mounted on an aircraft for sending cooled air to a service cart etc. for serving meals. The air chiller unit 1 comprises a refrigeration cycle unit equipped on a casing 10. The refrigeration cycle unit is equipped with a refrigerant compressor 20, a condenser 30 and an evaporator 40, and the cooled air is sent to a galley etc. via a blower device 60. The casing 10 is formed of a honeycomb panel. Since the honeycomb panel has high flexural rigidity, the base plate can reliably support the refrigeration cycle unit by itself. Further, since the honeycomb panel has good heat insulating property, the efficiency to cool air is improved.

Abstract: The invention provides a microwave oven capable of reducing the electromagnetic noises in the 2.45 GHz band generated during operation of the microwave oven. A microwave oven 1 comprises a microwave oven main body 2 having a heating chamber 3, and a door attached thereto. A ferrite sheet 14 disposed to cover the gap formed between the microwave oven main body 2 and the door 5 reduces the electric waves leaking through a choke groove 6 formed to a door panel 7. A punching metal plate 11 disposed on an outer side of a rear window film 10 and a wire mesh sheet 19 disposed on an inner side of a front window glass 13 shields the electric waves leaking through the window of the door 5, and the shielded electric waves are flown via a copper tape 20, an aluminum tape 17 and an EMI gasket 18 to a door case 8. Ferrite sheets 21 and 24 reduce the electric waves leaking through the gap of the door 5.

Abstract: The invention provides an audio plug capable of preventing excessive stress from being applied to a plug by enabling a plug body to be detached from a plug-in portion equipped with a channel plug, thus preventing damage and deterioration of function of the plug or a connecting portion between a cable and the plug. An audio plug 1 is equipped with a plug body 2 connected to a cable 3 leading to a headset, and an adapter 20 having channel plugs 30 and 31 that can be plugged into a jack 73, capable of transmitting audio signals from the jack 73 to the plug body 2 when attached. Since the adapter 20 is detachably attached to the plug body 2 by magnetic force, when a force greater than the magnetic force is applied from the cable 3, the plug body 2 is detached from the adapter 20 leaving the adapter 20 plugged into the jack 73, thus preventing poor contact or disconnection caused by excessive force applied to a connecting portion 5 of the cable 3.

Abstract: The invention provides a microwave oven capable of reducing the electromagnetic noises in the 2.45 GHz band generated during operation of the microwave oven. A microwave oven 1 including a microwave oven main body 2 having a heating chamber 3, and a door attached thereto. A ferrite sheet 14 disposed to cover the gap formed between the microwave oven main body 2 and the door 5 reduces the electric waves leaking through a choke groove 6 formed to a door panel 7. A punching metal plate 11 disposed on an outer side of a rear window film 10 and a wire mesh sheet 19 disposed on an inner side of a front window glass 13 shields the electric waves leaking through the window of the door 5, and the shielded electric waves are flown via a copper tape 20, an aluminum tape 17 and an EMI gasket 18 to a door case 8. Ferrite sheets 21 and 24 reduce the electric waves leaking through the gap of the door 5.

Abstract: In a continuous molding apparatus equipped with a long core 10 having a curvature disposed on a plane, a release film supplied from a lower release film feeder 20 is sent onto the core 10, and prepreg sheets supplied from a prepreg sheet feeder 30 are laminated thereon and preformed. A release film supplied from a release film feeder 40 is disposed on top of the laminated body, before the body is sent into a hot press 50. A puller 60 moves the laminated body without loading tension thereto. The laminated body enters a postcure device 70 in which thermosetting of the material is completed.

Abstract: The invention aims at reducing the beating noise generated from motors of equipments placed in a galley unit of an aircraft. A galley unit 1 of an aircraft includes a cabinet 10 formed of honeycomb panels and the like. The cabinet 10 has a counter 50 for cooking, and a compartment 20 formed under the counter 50 for storing service carts 30. A plurality of ovens 100 for heating warm dishes are provided above the counter 50. Each oven 100 has a fan motor for making the inner heat even. If all the fan motors of the ovens are driven at the same rotation frequency, a beating noise will be generated from the motor and amplified through the compartment 20. Therefore, the rotation frequencies of the fan motors are slightly varied.

Abstract: A galley body includes a storage unit 100 having a pair of guide rails 110 disposed on the bottom thereof for guiding a device to be mounted detachably to the galley. A connect panel 200 formed integrally to the galley body for connecting the device is disposed at the back of the storage unit 100. A connector 210 is disposed on the connect panel 200. A pair of guide holders 230, 240 is implanted in the connect panel 200 on both sides of the connector 210. The guide holders 230, 240 are formed for example of metal pipes having a light receiving member 232 or a light emitting member 242 composing the photocoupler disposed in the inside thereof, respectively. On the other hand, guide pins mounted on the device to be connected and corresponding to the guide holders 230, 240 have a light emitting member or a light receiving member composing the photocoupler disposed in the inside thereof, respectively.

Abstract: A cockpit door comprises a hinge 20 provided to one surface and a latch device provided to the other side that can be operated only from the cockpit side. To the inside of a door panel is disposed a reinforcement member 110 formed by laminating multiple layers of sheets with thermoplastic adhesives, the sheets formed by laminating aromatic polyamide fiber onto a honeycomb panel and processing the same into sheet form. A titanium alloy reinforcement plate 400 is disposed to cover the gap G1 between the door body and flap 60. Mounting portions 150 and 160 are provided to the rim of the reinforcement member body 110, and rivet holes 180 are provided thereto. The mounting portion is bent 90 degrees and fixed to the frame by rivets.

Abstract: The invention provides a hybrid relay generating low electric noise used for controlling the on/off of an electrical equipment. A hybrid relay 30 inserted to a line L supplying power to a load 20 has lines L1 and L2 branched in parallel. A first mechanical relay 31 is inserted to the first line L1, and a semiconductor relay 33 and a second mechanical relay 32 are inserted serially to the second line L2. When turned on, the second mechanical relay 32 is closed, the semiconductor relay 33 is closed, and then the first mechanical relay 31 is closed, and finally the semiconductor relay 33 is opened. When turned off, the opposite operation is carried out. The semiconductor relay will not always be closed, and the generation of electric noises by the mechanical relay can be prevented.

Abstract: The invention provides a manual trash compactor for a trash bin disposed inside a lavatory unit of an aircraft. A trash bin 100 disposed within a wash basin in a lavatory unit of an aircraft has a lid 50 through which trash is thrown in disposed on an upper surface of the wash basin. Below the lid 50 is equipped a container 120 for trash. A trash compactor 150 has a trash compressing member 152 pivotably disposed via a shaft 154 on a frame 130. The trash compressing member 152 is pivoted manually using a handle 170 to compress and reduce the quantity of the trash inside the container 120.

Abstract: The invention provides a device for automatically opening and closing a lid of a trash bin in noncontact fashion disposed in a lavatory unit of an aircraft. On the upper portion of a trash bin100 disposed in a lavatory unit of an aircraft is attached a lid 50 that pivots via a shaft 250. The reflective infrared radiation sensor 200 attached to a lid frame 60 irradiates infrared radiation IR and detects an object. When the object is detected, a control means drives the DC motor 220 to pivot the shaft 250 via a rotating lever 240 and link arms 242 and 244 to open the lid 50 downward. The fully closed state and the fully opened state of the lid 50 can be detected by position detecting sensors 260 and 262.

Abstract: A door lock device includes a latch projecting from the side surface of the door, and a hook supported opposite to the latch in a doorjamb such that the hook can turn between a latch detaining position and a latch releasing position. A hook control member turns between a hook detaining position at a locking position and a hook releasing position. First, second and third rocking plates are interlocked with the hook control member. When a solenoid actuator rod engaging with the third rocking plate projects upward to fasten the door lock device, the third rocking plate is turned clockwise by a pin, and the second rocking plate having a pin pressed against the third rocking plate turns clockwise. Conversely, when the rod is retracted the door lock device is unfastened.

Abstract: The invention provides an improved air chiller unit mounted on an aircraft for sending cooled air to service carts used for serving meals. An air chiller unit 1 includes a refrigeration cycle unit housed in a casing 10. The refrigeration cycle unit comprises a compressor 20, a condenser 30 and an evaporator 40 for a refrigerant, and the cooled air is sent to a galley via a blower device 60. The casing 10 is formed of honeycomb panels. The compressor 20 is supported via a pair of vibration isolation mounting devices 26 on a base plate of the casing 10. The vibration isolation mounting device 26 is formed of a triangular prism-shaped bracket and an A-shaped vibration isolation rubber, which functions to isolate vibration at normal times, and when a large load is received, functions to support the compressor device 20 with high spring constant with the rubber vibration isolator compressed.

Abstract: The invention provides a catch device of a cockpit door of an aircraft with improved safety. A cockpit door 1 disposed between a cockpit 2 and a passenger cabin 3 in an aircraft comprises a door body 10 that opens toward the cockpit via a hinge 12. A latch device 100 for opening and closing the door is provided on the cockpit side, and a bolt 120 thereof engages with a catch device 200 provided on a wall adjacent to the door. The catch device 200 has a solenoid device which restrains the rotatably disposed catch device by electromagnetic force. When trouble occurs to the solenoid, the restrained status of the catch member is released and the cockpit door may be opened. In such case, a pit pin 300 is inserted to the catch device to restrict rotation of the catch member.

Abstract: The invention provides an audio plug capable of preventing excessive stress from being applied to a plug by enabling a plug body to be detached from a plug-in portion equipped with a channel plug, thus preventing damage and deterioration of function of the plug or a connecting portion between a cable and the plug. An audio plug 1 is equipped with a plug body 2 connected to a cable 3 leading to a headset, and an adapter 20 having channel plugs 30 and 31 that can be plugged into a jack 73, capable of transmitting audio signals from the jack 73 to the plug body 2 when attached. Since the adapter 20 is detachably attached to the plug body 2 by magnetic force, when a force greater than the magnetic force is applied from the cable 3, the plug body 2 is detached from the adapter 20 leaving the adapter 20 plugged into the jack 73, thus preventing poor contact or disconnection caused by excessive force applied to a connecting portion 5 of the cable 3.

Abstract: A cockpit door body 10 can be opened toward a cockpit in a direction shown by arrow R1 by a crew inside a cockpit 3 by manipulating a knob on a first hinge device 40. When rapid decompression occurs in the cockpit, a mechanical pressure-sensitive device of the first hinge device 40 operates to release a bolt from a catch. By the difference in pressure between the cabin and the cockpit, the door body 10 opens in the direction of arrow R1 to thereby reduce pressure difference. When rapid decompression occurs in cabin 4, a second latch device 60 detects this pressure difference and operates mechanically to rotate a link lever 62 to release a stopper 64 from a catch 66. Flaps 30 and 32 are opened toward cabin 4 in the direction of arrow R2 by the difference in pressure between the cockpit and cabin to thereby reduce pressure difference.

Abstract: The invention provides a method for simultaneously forming a surface texturing pattern (embossed pattern) on the surface of an FRP product when manufacturing the FRP product by hot-pressing a prepreg material. A prepreg material 2 is a woven sheet formed by weaving a weft 10 and a warp 20 which is impregnated with thermosetting resin 40. A release film laminate 100 formed by sandwiching an adhesive film 130 between release films 110 and 120 is placed on a surface to be provided with surface texturing, before subjecting the same to hot-pressing. The softening temperature of the adhesive film 130 is close to the curing temperature of the thermosetting resin 40, so as to allow the thermosetting resin 40 to be pushed into the space between hard FRP fibers during hot-pressing and to form the surface texturing pattern on the surface of the member.

Abstract: A washstand unit 10, a waste storage compartment 11, a mirror 12, an upper cabinet 13 and a lighting equipment 14 are disposed on a side panel 5. Fitting concave portions 15 and 16 are formed on the washstand unit 10 for receiving portions of the waste storage compartment 11 and lighting equipment 14. Fitting portions 19, 20 and 21, 22 are formed on the mirror 12 for receiving portions of the upper cabinet 13 and lighting equipment 14. The washstand unit 10, the waste storage compartment 11, the mirror 12, the upper cabinet 13 and the lighting equipment 14 are mounted independently on the side panel 5 without assembling.

Abstract: A coffee maker 1 capable of being used normally and conveniently during use and downsized when not in use to provide working space, comprises a coffee maker body 2 equipped with an apparatus for brewing coffee, a holder 4 capable of mounting a coffee server 5, and folding arms 3 having plural arms 21, 22 linked to form a set of arms and connected revolvably between the coffee maker body 2 and the holder 4. The coffee server 5 can be mounted on the holder 4 when the arms 3 are extended. When the coffee maker 1 is not used, the holder 4 is elevated and folded to make space for other purposes. A lock mechanism can be provided to unlockably lock the elevated holder 4 to the body 2.

Abstract: A galley 1 has a main body 10 constructed of a panel material, and the galley main body 10 has a table 20, a sink 30, a storage compartment 40 and a service cart housing compartment 60. A hot-water supply unit 100 has a hot-water tank 10 with an electric heater and an electric instantaneous water heater 120 and is supplied with electric power by a control unit 150. The hot-water tank 110 and a hot-water tap 180 are connected via a hot-water supply line 190. In response to a command from a device that manages the electric power in the aircraft, the control unit 150 provides hot water using the instantaneous water heater 120 when the electric power consumption in the aircraft is low.