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Matches 901 - 950 out of 1,582

Document Document Title
JP2011504773A
The present invention relates to Testa (100) for examining the reliability of the cockpit oxygen distribution circuit (1) which has a plurality of component parts (20, 30, 40, 50) which secure the supply of oxygen to the member of the co...  
JP2011504844A
The present invention relates to an energy supply system which operates at least one air-conditioning system (26) of an airplane in at least one air line network and at least one electric line network, An air line network is connected to...  
JP2011031780A
To provide a heat exchanger for an aircraft which can prevent an iced component from accumulating in a low temperature channel.The heat exchanger for the aircraft 7 includes: a core 10 having a plurality of high temperature channels 16 f...  
JP4630286B2  
JP4630287B2  
JP4625053B2  
JP4617469B2  
JP4614970B2  
JP4614972B2  
JP4614971B2  
JP4614969B2  
JP4610568B2  
JP2011500411A
The system has a control device (26) arranged to ensure that air provided by an air supply device (18) enters into airplane region to be aerated e.g. airplane passenger cabin (12), via an air inlet (24) with velocity and temperature. The...  
JP2010540310A
An outflow valve for an aircraft has a frame for arrangement in an opening of an outer shell of the aircraft, a first flap pivotably arranged in the frame for controlling a flow cross-section of at least one first inflow opening and at l...  
JP4589396B2  
JP2010535664A
The invention relates to a valve for controlling a fluid flow from a first environment to a second environment, having a frame for disposing a separating element in the region of an opening, said element separating the first environment ...  
JP4575380B2  
JP2007516895A5  
JP2007516895T5  
JP2010533096A
An aircraft cockpit that includes comfort and/or security adjustable equipment in which the adjustments are controlled by an adjustment management system so that, by the unique selection of a position desired by the pilot from at least t...  
JP2010208488A
To achieve efficient thermal control by a simple configuration and an improved degree of freedom of an attachment arrangement including design. An aerial 11 is arranged on an outer wall of a flight vehicle body 10, and a pressurized cham...  
JP4538005B2  
JP4537399B2  
JP4537106B2  
JP2010528222A
The pump has a pneumatic actuator (10) arranged on a high pressure air supplying pipe (2). A power circuit is arranged between a pressure source and a pressurization pipe (14), and delivers controlling pressure to a controlling chamber (...  
JP2010525978A
An object of the present invention is the air exhaust provided with a net (10) attached to a level on the surface of flight dynamics of an airplane, and is the net, A plurality of openings demarcated in an insertion zone allocated by ext...  
JP4510634B2
Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet eng...  
JP4509110B2  
JP4490963B2  
JP4487792B2  
JP4489776B2  
JP4483150B2  
JP2010519119A
The present invention relates to the body (1) of an airplane or a spacecraft which has at least one shell element (2) and structural element (7). Between at least one shell element (2) and structural element (7), a gap (5, 9) to which ai...  
JP2010517677A
[Means for Solution] An expansion type harness crew mask is provided with expansion type harness with a compressed gas distribution system connected independently to expansion type harness with oxygen supplied to a mask from an oxygen re...  
JP2010105516A
To suppress inconvenience that a low temperature air flow passage is closed through the deposition of a freezed moisture content on an inlet side surface of a low temperature gas flow passage of a core part without preparing a particular...  
JP2010100285A
To provided a method and a system for providing a secondary power to an aircraft system.In one embodiment, an aircraft system architecture for providing the power to an environmental control system includes an electric generator 316 oper...  
JP2010513119A
The present invention relates to a cooling system for airplanes provided with the inspiratory port (4) where air flows into the rum air pipeline (2) through an inspiratory port (4) from the circumference of an airplane, and the exhaust p...  
JP4453795B2  
JP2010511562A
It has a pressure control actuator (30) which operates a pressure valve, which operates a static-overpressures valve of an airplane cabin especially and which is a control unit (100) and operates an operating member (20) according to an ...  
JP2010064733A
To provide a method and a system for controlling the temperature of an air separation module efficiently.This inert gas generating system 10 in aircraft is provided with a compressor system 14 having a first compressor 16 being driven by...  
JP4435168B2  
JP2010507525A
It is a sound wave absorber for airplane air pipe lines, and is the sound wave absorber, At least one crookedness pipe part (1;1') which covered each inner wall with a sound wave absorbent material is included, being constituted so that ...  
JPWO2008065709A1
航空機において調質空気を供給するに際し、 酸素濃度および湿度の中の少なくとも一方が 調整された調質空気を航空機において生成す る。その生成された調質空気を、航空機...  
JP2010505696A
The arrangement has pipelines (1, 2) connected to turbines (Ta, Tb), and arranged downstream from the turbines. An outlet of a heat exchanger (11) is connected to a pipeline (4), and feeds temperature-reduced fresh air to the pipeline (4...  
JP2010504767A
A respiratory mask (1) for a crew of an airplane or a passenger contains a rigid body portion (3) fit for a user's face, and the rigid body portion contains an element for carrying gas suitable for breathing to a user. A respiratory mask...  
JP4414463B2  
JP4412562B2  
JP4410790B2  
JP2010502501A
The present invention relates to an air supply system of an airplane, especially a passenger plane, and is this air supply system, It connects with an open air system which can supply the open air fresh to an airplane cabin, and this ope...  
JP2010501404A
A cooling system (10) which cools heat load (28, 34) in an airplane, While combining with a cold generating device (12) and this cold generating device (12) thermally, it connects with the 1st heat load (28), It has the 1st cold conveyan...  

Matches 901 - 950 out of 1,582