| Document |
Document Title |
|
JP2002519237A |
A method and system for providing nitrogen-enriched air (NEA) to aircraft fuel tanks using multiple air separation modules (ASMs). The ASMs employ membranes having different permeabilities and selectivities which are particularly selecte...
|
|
JP2002166895A |
To provide a fuel feeding device for a pilotless helicopter allowing lengthening a flying distance and a flying time and returning always assuredly corresponding to a residual volume of fuel.This device comprises a main pump P2 adapted t...
|
|
JP2002161819A |
To constantly suck fuel regardless of a flight attitude of an airplane.In this fuel tank 2, atmospheric pressure or air pressure is applied to fuel of the fuel tank and the fuel is sucked through a fuel pipe by a fuel pump. In a tip of t...
|
|
JP2002506780A |
An apparatus (1) for use with a container (100) for storing a substance. Typically, the substance is a volatile liquid, such as hydrocarbon fuels, alcohol or distilled liquids. The apparatus (1) acts to prevent filling and evaporative lo...
|
|
JP2002019062A |
To provide a composite material having a light weight and a high strength without bringing about a decrease in the strength and without degrading even at a cryogenic temperature, and a container constituted of the composite material and ...
|
|
JP2001348000A |
To provide a low cost nitrogen separator preventing deterioration of airframe performance caused by increase in engine bleed air quantity and improving a mounting property from reduction of size and weight by improving a nitrogen separat...
|
|
JP3187427B2 |
A compartmentalized tank divided into a plurality of compartments are fluidly connected to a filling chamber wherein the filling chamber has an overflow fluid passage to each of the plurality of compartments and a fluid channel elevation...
|
|
JP2001138999A |
To fill a helicopter tank almost full while maintaining the function of a vent passage of the helicopter tank in a perfect state. Regarding the vent valve and vent passage for the helicopter tank, the vent valve is provided with a closin...
|
|
JP3078818B2 |
Parallel transfer pumps (92,94) operate to transfer fuel from auxiliary tanks (52,60,66) to the main tank (10). A pressure sensor (106) in the pump discharge line in combination with tank level rate means (86,88,90) sequences pumps (92,9...
|
|
JP2000505838A |
(57) [Summary] Before use essentially a) 30-90% by weight porous foundation material. b) Teach a fuel tank gasket (20) consisting of 10 to 70% by weight of additives, which must have an affinity for the porous foundation material. The po...
|
|
JP2000120500A |
To provide a firing control system capable of inexpensively preventing fuel in the fuel tank of an internal combustion engine and the like from being in danger of catching fire.This firing control system is equipped with a first delivery...
|
|
JP2000097050A |
To supply a fuel without using an accessory gear box and a gear pump having a large weight by using a centrifugal pump to discharge the fuel by driving a motor as a pump.A fuel supplying device mainly comprising a centrifugal pump 19 in ...
|
|
JP2905876B1 |
[wrap up] [Task] Provided is a fuel tank capable of stably supplying fuel in the tank to the engine side regardless of the navigation posture of the navigation body. The fuel suction pipe 4 and the delivery pipe 5 are connected to the up...
|
|
JP2811009B2 |
|
|
JPH10203492A |
To fill sealing compound automatically by making working fluid act on a cylinder in the time set in a first timer to operate a piston of a master cylinder and push out sealing compound into a seal hose from a seal cartridge. A stream of ...
|
|
JP2775397B2 |
PURPOSE: To provide a liquid ballast device and fuel tank device which can be simply manufactured with low cost and prevent the liquid from abrupt inclination in all directions. CONSTITUTION: A boat 1 is an either-passenger compact boat ...
|
|
JPH09175499A |
To improve the multi-stage type space flight and transporting device, utilize the propulsion device of a flight device to be released for the whole of the space flight and transporting device, concurrently guarantee the storage of fuel i...
|
|
JPH09169299A |
To provide an apparatus for reducing heat filled in a airplane especially in a super-sonic aircraft during flight for exhausting a part of heat incoming through the outer shell before reaching and heating the aircraft cabin and the fuel ...
|
|
JPH08506073A |
Large amounts of hazardous goods, especially liquid ones such as fuel, may be carried in safety containers, whether tank semitrailers, oil tankers, containers for hazardous goods or aircraft, and be transported with practically no risk f...
|
|
JPH08151000A |
PURPOSE: To provide an integral fuel tank capable of holding soundness of whole structure in the case where excessive pressure is generated inside thereof without increasing weight. CONSTITUTION: An integral fuel tank is realized without...
|
|
JPH0840394A |
PURPOSE: To effectively control the center of gravity of an aircraft and inertia moment by quickly transporting a fuel, and to take emergency measure when a fuel tank is damaged. CONSTITUTION: A fuel transport device comprises a fuel tan...
|
|
JPH07317564A |
PURPOSE: To restrict flame-out or power descent in a fuel engine by providing an accumulating means accumulating vapor and fuel for delivering fuel to an engine, while minimizing the amount of undissolved vapor delivered to the engine, a...
|
|
JPH0751998Y2 |
|
|
JPH0751997Y2 |
|
|
JPH0750320Y2 |
|
|
JPH07286930A |
PURPOSE: To enable the fuel leak position of an aircraft to be detected easily and quickly by sealing a portion of the aircraft encompassing the fuel leak position against outside air under pressure, and pressurizing and forcing fluid in...
|
|
JPH07257493A |
PURPOSE: To suppress accumulation of static electricity between fuel and fuel tank due to shaking of fuel by providing a conductive three-dimensional lattice arranged in an internal film of a fuel tank main unit, and electrically connect...
|
|
JPH07215298A |
PURPOSE: To display the relation of the residual fuel and the fuel amount necessary to return to a base on the screen of a multifunction display device (MFD), and generating a caution-and-warning when the aircraft cannot to return to the...
|
|
JPH07145850A |
PURPOSE: To form ducts provided for accommodating a fluid and subjected to a vibration load in a container where vibration phenomena could occur, and other components, so that the ducts and the other components can be readily and surely ...
|
|
JPH07125697A |
PURPOSE: To restrain temperature in a fuel tank below the flash point of fuel without excessively increasing the thickness of the outer shell of the fuel tank by arranging a thermal cutting off layer consisting of a heat isolating layer ...
|
|
JPH07117798A |
PURPOSE: To reduce the weight by discharging fluid without pressurizing a fluid sealing bladder by high pressure gas or the like in a discharging device of the fluid from a fuel tank or the like of an artificial satellite. CONSTITUTION: ...
|
|
JPH0737239B2 |
|
|
JPH0694818B2 |
A fuel control (23) for an aircraft engine (10) employs super contingency logic (76) in response to low rotor speed of a helicopter (130) engine failure (131) or entry into an avoid region of a flight regime following engine failure (133...
|
|
JPH06316298A |
PURPOSE: To prevent heat inflow due to aerodynamic, heating by forming a sandwiched layer upon interposing an insulated layer and a heat storage layer between two structural members. CONSTITUTION: Two insulated layers 2 and 2 consisting ...
|
|
JPH0672393A |
PURPOSE: To provide an insert for an airtight caisson made of synthetic material which can be readily fixed to the caisson, has a simple structure and exerts excellent nonpermeability in a high temperature condition. CONSTITUTION: An ins...
|
|
JPH061298A |
PURPOSE: To withstand impact without increasing the strength of the side wall of a fuel tank so as to make the fuel tank lightweight by providing an impact damper for absorbing the inertia of fuel to relax impact, on the tank side wall i...
|
|
JPH05302528A |
PURPOSE: To provide an arrangement for heating aircraft fuel that does not need the necessity of an electrical heating element. CONSTITUTION: This arrangement for heating aircraft fuel has a viscous drag generator 4, a typical electric m...
|
|
JPH05155391A |
PURPOSE: To allow a rubber tank to be simply and easily installed on a tank supporting material for aircrafts or the like by attaching different bonded fabrics to the outer surface of a rubber tank and the corresponding parts of a tank s...
|
|
JPH05116689A |
PURPOSE: To allow the drop-fuel tank of an aircraft to be cast-off without being constrained by the residual fuel quantity and the speed-acceleration of the aircraft. CONSTITUTION: This aircraft fuel tank cast-away device is formed of a ...
|
|
JPH05479Y2 |
|
|
JPH05478Y2 |
|
|
JPH0453760B2 |
|
|
JPH0496600U |
|
|
JPH04221295A |
PURPOSE: To solve a problem related to the conventional fixed type pylon device where a positional relationship between an airframe and an on-board article suspended from the pylon device is fixed, and the flatter characteristic and perf...
|
|
JPH04208695A |
PURPOSE: To facilitate the formation of a covered layer by the expansion materials and secure the sufficient bulletproof performance by forming the covered layer by the expansion material through the spraying onto the whole surface of th...
|
|
JPH04154499A |
PURPOSE: To prevent explosion and firing of a combustible with certainty by controlling the feed rate of a nitrogen-enriched gas feed means according to the result of detection of the density of nitrogen or oxygen in a gaseous phase port...
|
|
JPH04124000A |
PURPOSE: To keep off any performance-degradation in a helicopter by way of decreasing the extent of air resistance along with reduction in an external fuel tank, by constituting this tank so as to make its form expand or contract in keep...
|
|
JPH0439995U |
|
|
JPH04103498A |
PURPOSE: To dispense with a plane-leg so as to decrease the plane weight or to increase the a useful load by adopting the following procedures: when a space plane takes off, it is connected to a trolley with an engine, it makes a take-of...
|
|
JPH0420112B2 |
|
