1904 results about "Engine room" patented technology

In an air intake structure (14) of an aircraft engine pod, the link or connection between the air intake lip (15), the front reinforcing frame (16) and the acoustic panel (17) is implemented in such a way that the lip (15) can be dismantled without breaking the link between the frame (16) and the panel (17). Moreover, the internal, rear part (15a) of the lip (15) normally covers the front part (17a) of the panel (17), as well as the members (22, 24) ensuring the link between the latter and the frame (16).

The mounting direction, posture, or location of an electronic control unit provided with a respiratory filter in a waterproof case is not restricted in an engine room or the like. Raised protective walls that surround the portion at which the respiratory filter is arranged are provided, and at least two concave portions for drainage that each extend through different positions of the protective walls are provided.

A passive cooling system for an auxiliary power unit (APU) installation on an aircraft is provided. The system is for an auxiliary power unit having at least a compressor portion of a gas turbine engine and an oil cooler contained separately within a nacelle. The system includes the auxiliary power unit housed within the nacelle of the aircraft, an engine exhaust opening defined in the aft portion of the nacelle and communicating with the gas turbine engine, at least a first air inlet duct communicating with a second opening defined in said nacelle and with said compressor portion and the oil cooler is located within a second duct communicating with an opening other than the engine exhaust opening of said nacelle and with the engine exhaust opening. Exterior cooling air and engine exhaust ejected through said engine exhaust opening entrain cooling air through said second duct to said oil cooler, and thus provide engine oil cooling. An exhaust eductor is also provided.

An environmental control system for an aircraft cabin includes a plurality of electrically-driven ported shroud cabin air compressors, each cabin air compressor compressing ram air received from the aircraft exterior, a heat exchange circuit comprising a primary heat exchanger receiving airflow from at least one of the cabin air compressors, and the secondary heat exchanger supplying airflow to the aircraft cabin, and an air cycle machine comprising a compressor adapted to receive airflow from the primary heat exchanger and supply compressed air to the secondary heat exchanger. The environmental control system may further comprise an air recirculation system, having an aft recirculation fan adapted to receive a portion of recirculation air from the aircraft cabin, and a recirculation heat exchanger, disposed in the heat exchange circuit in series with the primary and secondary heat exchangers, and adapted to receive airflow from the aft recirculation fan.

The soundproof casing is divided to an engine room 1, a muffler room 2 and a radiator room 3. The engine room 1 includes the engine E and a work machine unit (generator unit G). The muffler room 2 includes mufflers M1, M2. The radiator room includes a radiator R. An electric fan D is provided between an air intake aperture 22a and the radiator. The radiator room and the muffler room are communicated. An air flow duct 4 to communicate the engine room and the muffler room is provided. An engine fan F is provided just opposite to an entrance of the air flow duct. An inter-cooler I is provided in the air flow duct. The soundproof type engine driven work machine including aforementioned apparatuses is offered to improve the cooling efficiency as well as reducing unfavorable noise.

A thermal management system for an aircraft is provided. The aircraft includes a primary air conditioning system which compresses and cools outside air to create inside air. The inside air pressurizes the internal volume of the aircraft and ventilates a first object in the internal volume. An exhaust exhausts a portion of the inside air to allow more outside air to be drawn into the aircraft. A cooler cools a coolant which in turn controls temperature of at least two objects in the internal volume.

An engine is activated to drive a generator when an electrical output is required. The required electrical output (PO) is searched and the necessary engine output is calculated. The basic driving point (NO, TO) which obtains maximum fuel efficiency is set at that output (S101-S105). The load of the generator is controlled so as to reach the set basic driving point. When the catalyst temperature is lower than a set value, while maintaining the required electrical output, the basic driving point is varied to a driving point (Ncold, Tcold) which will raise the exhaust gas temperature (S106-108). Furthermore when the temperature of the peripheral engine components in the engine room is higher than a set value, while maintaining the required electrical output, the driving point is varied to a driving point (Nheat, Theat) which will lower the exhaust gas temperature (S109-S111). Hence while maintaining the electrical output, it is possible satisfy each component temperature condition. Therefore while maintaining drivability, fuel efficiency performance, lowering exhaust gas emissions and component deterioration can suppressed.

A portion between a front end of an air guide plates, which forms an air duct portion, and the front exterior member of the vehicle is sealed by a seal portion. Therefore, hot air leaking from inside of an engine room, is positively prevented from being drawn into the air duct portion after it flows around the front end of the air guide plate.

A fire barrier panel of the kind suitable for lining car decks and engine rooms of high speed aluminum ferries is described. The panel (10) includes a relatively thin layer of inorganic insulating material (12) adhered to a lightweight support structure (14). The layer of inorganic insulating material may be an intumescent material made from mineral fibers. The decribed lightweight support structure (14) is a honeycomb panel having a honeycomb core (18) of non-combustible aluminum foil provided with two face skins made of glass reinforced plastics resin material (16). This construction of the honeycomb panel (14) is lightweight and has high stiffness and rigidity suitable for stiffening and supporting the insulating material into a rigid panel. The layer of intumescent material (12) supported on the panel expands when exposed to high temperatures to form a thick fire insulating barrier panel. Because the panels are self-supporting, and therefore support structures, installation costs are much lower than for prior art fire insulation systems.

The present invention discloses guide blades of an axial flow fan shroud for guiding the air blown by an axial flow fan in an axial direction, and more particularly, to a guide blade structure capable of preventing the backflow of high temperature heat from an engine room toward a condenser. A guide blade 35 of an axial flow fan shroud 30 comprises: a leading edge 37 for introducing the air blown by an axial flow fan 10 including a number of blades 12; a trailing edge 39 extended from the leading edge 37 to downstream; and an air flow guide surface 38 for guiding the blown air between the leading and trailing edges 37 and 39, wherein if a first outlet area a is defined by at a radius r from a root in the total length R of an angle of projection Aout of the guide blade 35 and a second outlet area b is defined by the remainder, the angle of projection Aout increases as approaching a tip with respect to an axial line in the second outlet area b.

The invention provides a four wheeled utility vehicle which can efficiently introduce a cooling air into an engine room from a front side of the vehicle. The vehicle is provided with a cabin arranged between front wheels and rear wheels and accommodating a seat of the vehicle and an operating portion in front of the seat to steer the vehicle; an engine room arranged within the cabin or at a position rearward of the cabin to accommodate an engine of the vehicle therein, and configured to be covered by a wall surface at least in a front side and an upper side of the engine; an air duct extending forward from the engine room, and introducing an engine room cooling air into the engine room.

A bleed air system for an aircraft has a gas turbine engine and operating method. The system includes an environmental control system (ECS) for providing cabin airflow to the aircraft, including operating modes such as first and second air cycle machine operating modes and heat exchanger operating modes. The ECS includes first, second and third bleed ports each configured to provide engine bleed air from gas turbine engine compressors to the ECS. The ECS includes a bleed air system sensor arrangement configured to sense one or more bleed air system conditions, an environmental control system controller that selects an environmental control system operating mode that provides required cabin air flow and temperature at an optimal specific fuel consumption of the gas turbine engine at the sensed system conditions, and a bleed port valve controller which determines an operating pressure required to operate the environmental control system in the selected mode.

The invention provides a high-power vertical shaft tidal generating set. A gravity type pylon base (1) is connected with a pylon (2) through a universal ball hinge (3); an engine room (4) is arranged at the top end of the pylon; the periphery of the engine room is distributed with ropes (6) used by anchor chain plate holes (5) for connecting a floating bucket (7) and an anchor chain on an anchor (8); a water turbine spindle (9) is sleeved on the pylon, and both ends of the water turbine spindle are provided with bearings; water turbine blades (12) are uniformly distributed and fixed on a shaft hub (14) of the spindle through a spoke (13); an umbrella-shaped gear (15) on the spindle is engaged with a small umbrella-shaped gear (17) on a shaft of a generator (16) in the engine room; sealing shaft sleeves (18) are additionally arranged at the upper end of the spindle, on the lower wall of the engine room and on the pylon; and the base and the universal ball hinge are connected through a flange plate (19). The high-power vertical shaft tidal generating set provides clean renewable energy sources required by production and life for coastal areas, numerous islands and remote areas and particularly for residents on islands which cannot be covered by the national grid, and has positive social benefit.

A drive component for driving an electric water pump for causing engine coolant to flow is mounted in an engine compartment. When the ignition is off and the temperature of a exhaust heat recovery device is above a temperature, an ECU estimates a peak temperature in the engine compartment after the stop of the engine. When the peak temperature is above a temperature, the ECU stops the engine and drives the electric water pump and an electric fan for cooling the drive component for driving the electric water pump.

The invention discloses a stand-by safety chain monitoring and protecting device for a wind power generation control system, comprising a power supply, a cable-twisting switch, an engine-room vibration protection switch, a grid protection switch, a converter protection switch, an engine room and tower support emergent stop button, a distributed heartbeat signal monitoring switch, a rotary speed protection switch and a safety chain relay, wherein the power supply generates power signals and is respectively connected in series with the cable-twisting switch, the engine-room vibration protection switch, the grid protection switch, the converter protection switch, the engine room and the tower support emergent stop button, the distributed heartbeat signal monitoring switch, the rotary speed protection switch and the safety chain relay. The monitoring and protecting device adopts an active safety design, runs independent of a PLC system and monitors relevant signals at real time; and when incidents endangering the safety of a machine set occur, the monitoring and protecting device actively controls a pitch system to realize full feathering, thereby achieving the safe shut-down of the machine set.

The invention discloses a front body framework structure of an automobile. The front body framework structure of the automobile comprises an automobile body A post, a front protective cross beam, a front engine room framework assembly and a front floor framework assembly, wherein the front engine room framework assembly comprises a front engine room longitudinal beam, and a plurality of longitudinal beams and cross beams, which are connected with the front engine room longitudinal beam and are used for dispersing and transferring collision energy; and the front floor framework assembly comprises a front floor longitudinal beam, a lower door sill, and a plurality of longitudinal beams and cross beams, which are connected with the front floor longitudinal beam and the lower door sill and are used for dispersing and transferring collision energy. Through the technical scheme, a plurality of structural beams are welded to form a closed annular body framework structure; the plurality of longitudinal beams and cross beams are used for absorbing and transferring the collision impact load, so that the front part is deformed and absorbs energy sufficiently; the number of impact energy transfer passages is large; the energy is reasonably dispersed; the energy is absorbed in time; the invasion amount of a front baffle plate is small; the deformation of the floor and a middle passage is small; the deformation of a cab is reduced; and thus, the damage to a passenger in the collision, and the maintenance cost of the automobile are reduced.

This invention provides a copper foil for a printed wiring board, which comprises a copper foil, an alloy layer (A) comprising copper, zinc, tin and nickel which is formed on a surface of the copper foil, said surface to be brought into contact with a substrate for a printed wiring board, and a chromate layer which is formed on a surface of the alloy layer (A,. The copper foil for a printed wiring board has the following features: even if a printed wiring board is produced using a long-term stored copper foil, the interface between the copper foil and the substrate is only slightly corroded with chemicals; even if the copper foil contacts a varnish containing an organic acid, e.g., a varnish for an acrylic resin, in the formation of a copper-clad laminate, the bond strength is sufficient. Even if a printed circuit board made by using the copper foil is placed in a high temperature environment, e.g., in an engine room of an automobile, for a long period of time, blistering of the copper circuit from the substrate due to deterioration of the interface between the copper circuit and the substrate does not take place.

An upper mounting part of a front strut assembly adapted to reinforce the rigidity of the periphery of a frontal mounting hole, rear mounting hole, and central mounting hole by a lower cowl panel mounted for integrally welding to the shock absorber housing upper panel placed at both sides of the engine room, and a lower cowl reinforcing means welded onto the lower cowl panel is disclosed. The structure minimizes resonance generated by the load transmitted from the outside of the vehicle, reduces driving noise and improves the vehicle ride and steering.

The invention relates to a wind power generation climbing hoisting crane, which belongs to hoisting machinery and consists of a machine stem, an upper holding clamp, a lower holding clamp, a hydraulic boom and a pulley hook connected with a hinging rope, wherein the upper end and the lower end in a cavity of the machine stem are provided with chain wheels which are in meshed connection by using a ring chain. The clamp body of the lower holding clamp is fixed at the lower end of the machine stem, and the clamp body of the upper holding clamp is sleeved on the outer wall of the machine stem through movable fit and an inner seat of the clamp body is provided with a ratchet to mesh the chain; and the upper holding clamp is provided with a jaw driven by a hydraulic tank, and the lower holding clamp is provided with a jaw driven by the hydraulic tank. The wind power generation climbing hoisting crane can be widely applied to large-sized wind generating sets such as the hoisting of the parts of a tower tube, an engine room, a wind wheel hub and the like, is applicable to hoisting operations of high altitude and superaltitude heavy equipment, is not limited by the maximum lifting height and fields, can perform hoisting operations on flat grounds, hillsides and sea surface, is electromechanically integrated with high automation degree, can be controlled on the ground, has light weight, is convenient for assembly and disassembly, transition and transportation, and has high operational efficiency.