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Patent Searching and Data


Matches 801 - 850 out of 867

Document Document Title
JP2001086723A
To provide an oscillation-absorbing type generator for reducing oscillations by absorbing the oscillation of the body generated at a helicopter, and generating electricity by using the oscillatory energy of an oscillator that reduces the...  
JP2000516553A
There is described an integrated muffler and exhaust cone 20, for use in a tailcone assembly 10 having a gas turbine engine 12 mounted therein. The integrated muffler and exhaust cone 20 includes a casing defining a conduit for porting t...  
JP2000344200A
To restrain the increase in the weight of an airframe.This auxiliary power unit 1 is provided with an air intake 2, a nozzle unit 3, an exhaust nozzle 4, a turbine 5, a bevel gear 6 and a gearbox 7. The air intake 2 is used to intake hig...  
JP3108098B2  
JP3060382B2
The fuel cell (1) generates direct current electricity which is converted for the aircraft network, air for the air conditioning system, warm water for the aircraft supply and hydrogen. A converter (9) converts the supplied direct curren...  
JP2000177697A
To restrain a gear box from being adversely affected to the minimum even when a rotor is turned out to be in a very unstable condition.This mounting part 60 includes a cross member 62 both the ends of which are mounted on an engine case,...  
JP2000025696A
To provide an energy supply device for use in an aircraft, which generates toxic material and noise less than that in a prior art and has an improved efficiency. In this energy supply device inside an aircraft which is converted for a ma...  
JP2972688B2
To provide a constant speed drive gear unit for an aircraft generator and a generating set for an aircraft having small size, light weight and high efficiency. This constant speed drive unit 10 for an aircraft generator is composed of an...  
JP2964063B2
PURPOSE: To obtain a highly reliable, compact and lightweight combustor which can produce emergency power through harmless and clean combustion while facilitating maintenance. CONSTITUTION: Air from a high pressure air tank is mixed with...  
JPH11240495A
To eliminate the need for a special person to control charging by simplifying the charging of the radio transmitter for unmanned helicopter control. A battery charger composed of a charger 1, a charging current voltage detection circuit ...  
JPH11210869A
To provide a constant speed drive gear unit for an aircraft generator and a generating set for an aircraft having small size, light weight and high efficiency. This constant speed drive unit 10 for an aircraft generator is composed of an...  
JP2897622B2  
JPH10226398A
To provide a boundary layer control mechanism for a short takeoff/ landing distance plane without apprehension generating hot circulation while forming a protruded part behind a pilot seat aerodynamically approximated to an optimum shape...  
JP2768290B2
PURPOSE: To realize an aerial moving body, such as a compact unmanned machine, which is relatively light, and can add to appliances requiring power and lengthen their operating time largely. CONSTITUTION: In a compact unmanned machine 11...  
JPH10169545A
To save a constitution element so as to obtain a high reliability by connecting a control device to both part systems of a hydraulic part system and an electric part system, carrying out suitable sitting or switching of an operating mode...  
JP2683685B2
To provide an auxiliary power system for short distance landing machine which can supply air for controlling a boundary layer stably. A compressor 21 for controlling boundary layer is driven by a first engine 11 through a first gear row ...  
JPH09511714A
An environmental control system has an air cycle machine that includes a compressor, a cooling turbine, a motor/generator, and a power turbine all mounted on a single shaft. The power turbine receives bleed air from the aircraft's engine...  
JPH09272496A
To solve such a problem that the mounting of a tunnel cable transmitting a control signal and a power from a guidance part to a drive source is difficult because a space in which the internal space of a tunnel cover for protecting a tunn...  
JPH09156598A
To provide an auxiliary power system for short distance landing machine which can supply air for controlling a boundary layer stably. A compressor 21 for controlling boundary layer is driven by a first engine 11 through a first gear row ...  
JP2616841B2
The invention relates to secondary power system apparatus and method for use aboard aircraft in place of conventional auxiliary power units (APU's) and emergency power units (EPU's). The invention integrated power unit (IPU) performs the...  
JP2590318B2
A ram air turbine and deployment mechanism has commonly had power-generating means in the form of either one, or both, of a hydraulic pump and electrical generator mounted at the end of a pivotal strut adjacent the ram air turbine. Reloc...  
JPH08313199A
PURPOSE: To enable a long-time flight by a method wherein one end part of a bypass piping is linked to a shunting point on the side of a fuel gas generator of a fuel gas piping while a converging point on the side of a jetting port to th...  
JPH08198195A
PURPOSE: To realize an aerial moving body, such as a compact unmanned machine, which is relatively light, and can add to appliances requiring power and lengthen their operating time largely. CONSTITUTION: In a compact unmanned machine 11...  
JP2519620B2
The invention relates to secondary power system apparatus and method for use aboard aircraft in place of conventional auxiliary power units (APU's) and emergency power units (EPU's). The invention integrated power unit (IPU) performs the...  
JPH07318058A
PURPOSE: To obtain a highly reliable, compact and lightweight combustor which can produce emergency power through harmless and clean combustion while facilitating maintenance. CONSTITUTION: Air from a high pressure air tank is mixed with...  
JPH07315297A
PURPOSE: To provide a kinetic energy storing device, which stores and utilizes flying energy to be lost in deceleration of an airplane, for an airplane. CONSTITUTION: A kinetic energy storing device for an airplane is constructed in such...  
JPH07507677A
(57)【要約】 本公報は電子出願前の出願データであるため 要約のデータは記録されません。  
JPH07505107A
(57)【要約】 本公報は電子出願前の出願データであるため 要約のデータは記録されません。  
JPH07137697A
PURPOSE: To facilitate the balanced design of an airframe by annexedly providing a controller used for operating the rudder of a jet airplane or additionally providing a united generator for controlling actuators as a dissolution type ge...  
JPH05338593A
PURPOSE: To provide a windmill type generating device of an aircraft, which is rotated at a constant rotating speed regardless of the speed of the aircraft by simple constitution, and can generate electric power of constant frequency and...  
JPH05502080A
The invention relates to secondary power system apparatus and method for use aboard aircraft in place of conventional auxiliary power units (APU's) and emergency power units (EPU's). The invention integrated power unit (IPU) performs the...  
JPH05502081A
The invention relates to secondary power system apparatus and method for use aboard aircraft in place of conventional auxiliary power units (APU's) and emergency power units (EPU's). The invention integrated power unit (IPU) performs the...  
JPH052559B2  
JPH0215596U  
JPH01269700A
PURPOSE: To stably maintain control of an aircraft by providing a high speed spool for driving auxiliary driving machines and a low speed spool for driving an emergency power unit at losing propulsion power on a turbofan engine. CONSTITU...  
JPH01237327A
PURPOSE: To raise reliability in emergency by inputting the power generated by two gas turbines to a common gear box, distributing the power to each power device, and supplying compressed oxidant in a storage container to a combustion ch...  
JPH01164700A
PURPOSE: To improve efficiency by cooling an airframe with a propellant, and spouting the heated propellant after this heat exchange from a nozzle in a missile exposed to a high temperature by aerodynamic heating, etc. CONSTITUTION: The ...  
JPH01501809A  
JPS6469721A
PURPOSE: To use a gas turbine multipurposely by communicating a turbine impeller at a boss of a centrifugal compressor through a clutch and connecting a source of a load and pressure on halfway of a duct connecting a gas inlet to the tur...  
JPS645183B2
An integrated drive-generator system having a drive input shaft with a mechanical differential positioned in coaxial relation with the drive input shaft, a generator positioned alongside said differential and drive input shaft, and a hyd...  
JPS6342094B2  
JPS63501210A
A deployment-retraction apparatus (10) for an air turbine (12) of an aircraft movable from a stowed inoperative position within the aircraft to an extended operable position externally of and in the airstream of the aircraft, and being r...  
JPS6321200U  
JPS62243933A
An aircraft emergency power unit having a high pressure air storage tank (22), an aviation fuel storage tank (24), and a combustor (26) which combusts pressurised air and aviation fuel in a stoichiometrically fuel rich ratio to produce a...  
JPS62501203A  
JPS626353B2
A radiant-energy-sensing power system applicable to aircraft having jet-type engines, vehicles having gas turbine engines, and missiles, comprising photovoltaic type cells mounted in the proximity of the combustion chamber of a jet engin...  
JPS625840B2  
JPS61285200A
A ram air turbine and deployment mechanism has commonly had power-generating means in the form of either one, or both, of a hydraulic pump and electrical generator mounted at the end of a pivotal strut adjacent the ram air turbine. Reloc...  
JPS60502221A  
JPS58217704A  

Matches 801 - 850 out of 867