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JPH052559B2 |
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JPH0215596U |
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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...
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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...
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JPH01501809A |
Duplication of engine and secondary power system components in individual auxiliary and emergency power units is avoided in an integrated power unit including a gas turbine engine 10 having a centrifugal compressor 28 and a turbine 40, a...
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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...
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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...
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JPS6342094B2 |
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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...
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JPS6321200U |
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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...
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JPS62501203A |
Deployment mechanism for a ram air turbine has conventionally consisted of a strut pivotally mounted within a storage bay of an aircraft and which pivots to a downwardly-extending position to bring the ram air turbine into deployed posit...
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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...
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JPS625840B2 |
An emergency hydraulic power system for aircraft which becomes operable upon aircraft engine failure includes a hot gas turbine for driving a hydraulic pump, a decomposition chamber to provide hot gas for driving the turbine, a normally ...
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JPS60502221A |
(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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JPS58217704A |
A rotary propeller (22) can act as the rotor of a ram air turbine for driving a load (64) or as a propulsion propeller driven by an engine (64) and the speed of the rotor (22) is controlled by rotating a reference shaft (37) at a control...
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JPS5758598A |
The unit comprises a prime mover 4 (auxiliary engine), a variable geometry compressor 22, and controlled emission turbine 24 which is shaft-coupled to the compressor and cooperating with the compressor to form an environmental control un...
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JPS5620840A |
A freewheel device for connecting a power input to a selected one of a plurality of outputs so as to transmit rotary motion in one direction of rotation and to over-run when the speed of the selected one of the outputs exceeds that of th...
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JPS5435249B1 |
An emergency hydraulic power supply for providing hydraulic power to an aircraft system in event of engine failure including a hydraulic pump, a hot gas turbine for driving the pump, a decomposition chamber for decomposing fuel to provid...
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JPS5411843B2 |
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JPS5137348A |
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JPS5116597A |
1476059 Helicopter rotor drive H OSBERGER 16 June 1975 [19 June 1974] 25517/75 Heading B7W A helicopter rotor 1 normally driven through shaft 2 by motor 4 is provided with an auxiliary drive which, in the event of failure of motor 4 or i...
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JPS5096000A |
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JPS5020655B1 |
1286728 Variable-speed gearing SUNSTRAND CORP 22 July 1970 [13 Aug 1969] 35627/70 Heading F2D In a constant speed drive for an aircraft alternator, comprising a planetary differential 17 controlled by an hydrostatic transmission 24, 56, ...
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JPS5050512A |
Prodn. of high pressure gases for driving a pneumatically operated energy source, partic. for starting aircraft jet engines in flight in an emergency or on the ground where no starting equipment is available, comprises (i) storing a quan...
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JPS4913899A |
An emergency hydraulic power supply for an aircraft or the like, including a hydraulic pump arranged to be driven by a turbine in turn driven by hot gas from a decomposition chamber, a fuel pump driven by the turbine for supplying fuel t...
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JPS386730B1 |
968,687. Charging and discharging batteries. KAMAN AIRCRAFT CORPORATION. Dec. 29, 1960 [Feb. 29, 1960], No. 44657/60. Heading H2H. A load 10 is supplied alternatively from a primary source comprising an A.C. generator 20 and a rectifier ...
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JPS3420945Y1 |
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