The assembly further includes at least one air bleed line (80) from the compressor (14) and at least one valve (84) for controlling air flow through the bleed line (80).
The invention also relates to a hydraulic system, an air bleed system and a method of controlling at least two wind turbine blades.
The actuating shaft (74) is biased so as to prevent air from entering the dispensing lid (10) through the air bleed valve (60) to assist in dispensing fluid from the fluid container (12) when the valve actuating member (72) is set to a first position.
A simplified air bleed balancing control system for a pair of aircraft gas turbine engines reduces the number of pressure transducers and differential pressure transducers.
Noise attenuator, especially for an aircraft turbofan engine air bleed system, comprises a perforated attenuator plate (16) extending over the outlet of an air bleed valve (1) and an intermediate attenuator plate (20) upstream of the first.
balance of bleed air demand
The supply unit (20) is connected to the bleed air device (22) and is designed to supply the oxidation agent based on bleed air dispensed.
cabin pressure bleed
The bleed air system has an opening which may be selectively closed to block bleed air, or opened to allow bleed flow from the compressor into the chamber.
The air intake tube protrudes through a top port of the container.
Individual VOC: whole air canister sampling; off line analysis by GC/FID (MS
A sample of air is tested on a continuous basis by drawing air via conduits (10, 11) through a chamber (12) containing the detector (13).
A bleed air system bleeds a quantity of air from the compressor into a chamber at least at low power conditions of the engine.
Support in the case of air sampling: TGC, tube XAD-D
The invention also concerns the turbomachine using this cover to form a sealed space (17), in particular with a view to collecting air.
1 out of 4 samples of air taken in the security check area
A thermoelectric device is coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air.
The system includes the bleed air system, the air conditioning system, the air distribution system, the cabin pressure control system, the wing anti-ice system and the avionics ventilation system.
Advantageously, the filter may be associated with the engine bleed air supplies without impeding the performance of the engine by decreasing the flow rate or supply of air from the bleeds to the ECS.
A sample of the dilution air shall be taken at a constant flow rate near the ambient air-inlet (after the filter if one is fitted).
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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