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JPH0414320Y2 |
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JPH0419079B2 |
A measure of the enroute weight of an aircraft is continuously provided by determining the zero fuel weight during takeoff, adding the weight of total fuel as measured by fuel quantity sensors (16, 17, 18) interrupting the latter measure...
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JPH0455193A |
PURPOSE: To ensure light weight and rigidity and to absorb shock of a tank at a crash or a fall of a helicopter by providing a shock absorbing member integrally attached or upper and lower surfaces of a honeycomb core through an adhesive...
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JPH045199A |
PURPOSE: To reduce air resistance to a flying aircraft so as to prevent deterioration in its performance by providing an additional fuel container mounted on the aircraft with a constitution in which the shape thereof viewed from the fly...
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JPH03130799U |
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JPH0338444Y2 |
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JPH03121219A |
PURPOSE: To simply and positively perform emergency shudown of an engine when an output shaft of the engine fractures by breaking a tube conveying incompressive fluid in conformity to the movement of the output shaft, and depressurizing ...
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JPH037244B2 |
Method and apparatus for detecting the presence of liquid in a container includes an elongate rod (or other vibratory element) which extends into the container to contact liquid when a certain amount of liquid is present, a piezo-electri...
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JPH02117299U |
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JPH02158325A |
PURPOSE: To reduce costs and weight and to improve impact resistance by a method in which a load shearing layer is constituted by curing a filament- wound inner skin, and the flexibility of the layer is increased by the incorporation of ...
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JPH0224719B2 |
A liquid reservoir, such as an oil tank, for use in missiles or aircraft which are subjected to extreme flight attitudes. The reservoir has a wall rotationally symmetrical about the longitudinal axis of the reservoir, and the liquid cont...
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JPH0216960Y2 |
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JPH0232499U |
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JPH01306398A |
PURPOSE:To enable the prevention of evaporation of cold liquid fuel, make the pressurization of a fuel tank and the use of a pressure bomb unneeded, and enable the reduction in weight of a fuel device by providing a condensor in a bent p...
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JPH01148997U |
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JPH01104900U |
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JPH0195996A |
PURPOSE: To eliminate the danger of explosion by using as a pressurized gas a nitrogen-rich gas obtained by removal of oxygen from air, in a device in which fuel boiling at reduced atmospheric pressure and tank damage at the increase of ...
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JPS63318499A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS63284098A |
An aircraft fuel system adapted for the automatic extraction and dispersion of entrapped puddles of water in an aircraft fuel tank as a function of fuel flow supply to at least one propulsion engine. Scavenge pipes, positioned to be imme...
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JPS6351919B2 |
The fuel tank as disclosed is provided particularly for storage of aggressive fuel as they are used for and in control jets, attitude positioning systems in satellite and space vehicles. The fuel tank is of a spherical configuration and ...
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JPS63135479A |
A storage container for effectively containing hydrocarbon fuels over a broad temperature range without significant loss of hydrocarbon fuel vapors, the container having a fluid impermeable housing and a seal disposed between opposed mat...
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JPS6319554Y2 |
An electrohydraulic servo system to actuate the power shaft of a fuel control system from the cockpit throttle including electrical devices responsive to the position of the throttle that actuates a hydraulic piston for moving the power ...
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JPS63125497A |
An aircraft having a propulsion system which utilizes a dual fuel system having an inner tank for containing a cryogenic fuel and an outer tank surrounding the inner tank for containing a second fuel wherein the second fuel is a fuel hav...
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JPS6357399A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS62244796A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS62244797A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS62168798A |
A first and a second conduit section (10,12) each have end portions (11, 13) which are covered by a dielectric insulating material (14, 22) The dielectric material (14, 22) covers an outer side surface (16, 24), an end surface (18, 26), ...
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JPS6291399A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6287697A |
The scavenge oil system disclosing the invention has a scavenge oil outlet located at the bottom of a blower housing whereby lubricating oil can flow thereto by gravity in most attitudinal positions of the housing. When the blower housin...
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JPS6243316A |
PURPOSE:To improve safety by enclosing the accommodated fuel by the fire extinguishing agent, in a fuel tank for vehicle. CONSTITUTION:A outer container 3 is installed, keeping an interval by a spacer 4 between a container 1, so as to en...
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JPS623306B2 |
PURPOSE:To maintain gas-liquid separation even under high acceleration in random directions by receiving a proper number of propellant cells provided with a propellant holder in a propellant tank body provided with a propellant filling p...
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JPS61183800U |
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JPS6142085B2 |
Apparatus for degrading safety fuel of the type containing an antimisting polymer and comprising a cylindrical vaned stator and vaned rotor in radially concentric array, whereby rotation of the rotor will cause safety fuel pumped through...
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JPS61115800U |
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JPS6121895A |
A fuel supply system for use in rotary wing aircraft is described. The system comprises a separating means (10) for: receiving an air, vapour and fuel mixture at relatively low pressure from a fuel tank; separating the air and the vapour...
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JPS619400A |
A controllable fluid damper 14 for a fluid-containing tank 10 in a space vehicle comprising a hollow sphere 14. The wall of the sphere 14 is a honeycomb structure of six-sided cells 24 arranged with respect to the sphere 14 so that the o...
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JPS6055399B2 |
Disclosed is a fueling receiver adapted for connection to a tank. The receiver includes a body member which is affixable to the tank. Pivotally attached to the body member is a nipple member which includes a nipple for receiving a fuel n...
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JPS6044199B2 |
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JPS60179399A |
(57) [Abstract] Since this gazette is application data in front of an electronic application, the data of an abstract is not recorded.
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JPS6027831Y2 |
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JPS6099891A |
A toroidal tank truss supporting structure for a toroidal tank having a torus portion, with a hollow interior, and a torus shell enclosing the hollow interior is provided. The internal support structure includes a plurality of ring-bulkh...
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JPS59163199A |
A modular nozzle system particularly suitable for refueling aircraft fuel tanks includes a nozzle valve linkage mechanism which permits the nozzle body to have a shorter length than previous designs. The mechanism can be accommodated in ...
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JPS5990685U |
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JPS599068Y2 |
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JPS5924700U |
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JPS5828479B2 |
A cryostatic device comprising an inner wall and an outer wall connected at their upper parts by a filling orifice, a vacuum being made between the two walls, wherein the tank of cryogenic liquid, which is defined by the inner wall, is d...
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JPS587520B2 |
1429910 Emptying tanks SUNDSTRAND CORP 23 July 1974 [23 July 1973] 32461/74 Heading B8T [Also in Division B7] A fuel tank, particularly for monofuel supplying a hot gas turbine for driving an hydraulic pump in an emergency control system...
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JPS5754677B2 |
1447079 Fuel containers; aircraft fuel tanks J VIDILLES 12 Nov 1973 [20 Nov 1972] 52347/73 Headings B7H and B7W In a fuel tank including a leakproof elastomeric reservoir 1 contained within a chamber 3 comprising at least two part shells...
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JPS5750720B2 |
A burst disc unit for safety relief use in a fuel tank, responsive to temperature, and bursting at a predetermined temperature. It includes a housing with a disc element sealed thereon, and eutectic material in the housing supporting the...
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JPS5771752U |
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