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7198062 |
Fluid control valve
A valve is provided for controlling a flow of a fluid between a first environment and a second environment. The valve includes a frame adapted to fit within a perimeter of an aperture in a divider...
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7171819 |
Indirect regenerative air cycle for integrated power and cooling machines
An integrated power and cooling machine having an indirect regenerative air cooling feature may be useful for providing power and environmental control to both ground vehicles, such as tanks, and...
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7159818 |
Multi-spectral air inlet shield and associated inlet structure
A multi-spectral shield and associated inlet structure is provided for reducing the signature of an air inlet port defined within an exterior wall of an aircraft, ship, or land-based vehicle across...
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7070496 |
Air outlet device for a vehicle, especially for an airplane
An air outlet device for a vehicle, especially for an aircraft, comprises a nozzle body with an air intake opening and an air outlet opening. The air outlet device further comprises a holding...
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6955592 |
Air outlet device for vehicles, in particular airplanes, and method for assembling such an air outlet device
An air outlet device ( 1 ) for vehicles, in particular airplanes, comprises a panel ( 2 ) with at least one receiving opening, an air outlet ( 3 ) arranged in the receiving opening, and a sealing...
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6908062 |
Reduced bleed vapor compression cycle environmental control system for aircraft
The present invention relates to A reduced bleed vapor compression cycle environmental control system for an aircraft. The environmental control system provides conditioned external ram air to...
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6887147 |
Air outlet device for a vehicle, especially for an airplane
An air outlet device for a vehicle, especially for an aircraft, comprises a nozzle body with an air intake opening and an air outlet opening. The air outlet device further comprises a holding...
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6845630 |
Electric power and cooling system for an aircraft
The present invention relates to an electrical power and cooling system for use in an aircraft having at least one engine. The electrical power and cooling system comprises a single shaft, a power...
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6589109 |
Air outlet device for a vehicle, especially for an airplane
An air outlet device ( 10 ) for a vehicle, especially for an aircraft, comprises a nozzle body ( 40 ) with an air intake opening ( 44 ) and an air outlet opening ( 46 ). The air outlet device ( 10...
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6565035 |
Apparatus and method for forming an air curtain for use with an aircraft
A system and method for providing an air curtain for impeding the entry of dust, dirt, debris, smoke, insects and other airborne particulate matter into an interior area of an aircraft without the...
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6449963 |
Aircraft air conditioning system and method
An air conditioning system and method are provided for use in an aircraft having a pressurized area and an unpressurized area. The air conditioning system includes an air conditioning pack located...
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6402812 |
Filtered environmental control system
An integrated environmental control (IEC) system includes a decontamination Pressure Swing Adsorption (PSA) system in which a contaminated decontamination bed is purged through a purge exhaust duct...
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6401473 |
Aircraft air conditioning system and method
An air conditioning system and method are provided for use in an aircraft having a pressurized area and an unpressurized area. The air conditioning system includes an air conditioning pack located...
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6389826 |
High capacity air conditioning system with redundant staged recirculation air mixing for an aircraft
In an air conditioning system for an aircraft, two pre-mixing units respectively mix cold air from two air conditioning units with recirculated fuselage interior air from two recirculation units,...
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6375849 |
Integrated environmental control system and humidification system
In an aircraft, tap water is filtered, vaporized and injected into a trim line of an environmental control system. Filtering is performed by a reverse osmosis filter. Hot, humidified air leaving...
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6306032 |
Air-conditioning system for below-deck areas of a passenger aircraft
An aircraft air-conditioning system provides ventilation, air-conditioning and fire protection for a below-deck stairwell and cargo hold that may be equipped with passenger sleeping compartment...
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6289665 |
Aircraft air conditioner energy recovery method
The device involves the placement of an air pump turbine and the aircraft outflow valve in a duct through which all the air flows, with the turbine shaft attached to that of an electric generator,...
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6283410 |
Secondary power integrated cabin energy system for a pressurized aircraft
Increased efficiency of operation in pressurized aircraft may be obtained by employing pressurized air to be discharged from an aircraft cabin 10 as combustion air by applying it to the inlet 42 of...
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6241599 |
Pressure regulating system
The present invention relates to a pressure regulation system for maintaining the air pressure within a defined space at a substantially constant level. The pressure regulation system comprises a...
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6139423 |
Noise reducing bleed air heat ejection device for a heating system
A heat ejection device is disclosed for a heating system. The heat ejection device is adapted to mix ambient air from an interior with bleed air from a heat source. The heat ejection device...
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6128896 |
Aircraft air conditioner energy recovery device
The device involves the placement of an air pump turbine and the aircraft outflow valve in a duct through which all the air flows, with the turbine shaft attached to that of an electric generator,...
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6116541 |
Aircraft cabin outflow valve including aft door modified for noise suppression
An outflow valve for a cabin pressure control system of an aircraft cabin includes an aft door that is modified to disrupt or increase speed of cabin air flowing past the aft door and out of the...
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5897079 |
Air curtain insulating system for aircraft cabin
The present invention encompasses a system and method for insulating an aircraft passenger cabin from ambient temperatures without the need for insulation blankets. Hot bleed air flowing through a...
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5813630 |
Multi-mode secondary power unit
The present invention provides a multi-mode secondary power unit comprising a first starter/generator unit operably coupled to a shaft. The first starter/generator motor is operable in a motor mode...
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5695396 |
Ventilating system for reducing contaminations in the air of an aircraft
An air supply system for an aircraft cabin reduces the concentration of contaminations of the air in the cabin by a flexibly controllable valve system that comprises pairs of valves which on the...
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5490645 |
Fully integrated environmental and secondary power system
An aircraft subsystem provides the aircraft with all its electrical and conditioned air requirements without requiring the extraction of either shaft power and/or pressurized air from the...
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5474120 |
Two-channel cooling for providing back-up cooling capability
A cooling system is provided for compartments containing a heat generating apparatus, such as solid state variable speed constant frequency system, whose functionality is essential and whose...
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5442905 |
Integrated power and cooling environmental control system
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...
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5343692 |
Contaminate neutralization system for use with an advanced environmental control system
An apparatus and method of providing an Environmental Control System (ECS) for use in conjunction with a turbine engine power plant, to deliver a flow of purified, conditioned air to an enclosed...
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5327744 |
Integrated environmental control system for a helicopter
A compact, lightweight integrated environmental control (IEC) system for a helicopter incorporates in operative combination an environmental control system (ECS) and a nuclear/biological/chemical...
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5309735 |
Four wheel air cycle machine
An air cycle machine (10) has four wheels mounted on a common shaft (20) for rotation therewith about a longitudinal axis (12), including a second stage turbine rotor (30) mounted to a first end...
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5143329 |
Gas turbine engine powered aircraft environmental control system and boundary layer bleed
An aircraft gas turbine engine is provided with a starting air turbine that is directly connected through the starter gearbox to the high pressure (HP) shaft and is provided with an apparatus to...
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5125597 |
Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system
An aircraft gas turbine engine is provided with a starting air turbine that is directly connected through the starter gearbox to the high pressure (HP) shaft and is provided with an apparatus to...
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5118053 |
Pressure equalization systems
A system for preventing the sudden depressurization of a compartment in an aircraft from causing structural damage or damage to other critical aircraft components. The system includes a pivotable...
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5069401 |
Compartment partition and pressure relief door therefor
A reuseable panel for equalizing pressure between adjacent compartments includes a frame and a movable floor which is releasably sandwiched within the frame on three sides. When there is a...
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H000535 |
Compact device for continuous removal of water from an airstream-cascade screen
A separator for removing frozen or condensed water from an air stream, such as to aircraft environmental and avionics cooling systems, is described which comprises a generally tubular housing...
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4741255 |
Fluid flow distribution ducts
A fluid flow distribution duct for receiving temperature controlled air from duplicated Environmental Control System units in an aircraft air conditioning system and providing balanced distribution...
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4684081 |
Multifunction power system for an aircraft
The multifunction power system is a combination auxiliary power unit, environmental control system, engine start system, and emergency power system for an aircraft. The system is essentially a...
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4553474 |
Aircraft cabin pressurization system
This invention controls the air pressure in an aircraft cabin in response to a selected landing field altitude and to a selected maximum permissible cabin pressure rate.
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4357860 |
Telescoping conduit for pressurized air
A telescoping conduit for directing air at moderate pressures to a waiting aircraft along a telescoping bridge is disclosed. One telescoping tube is suspended from each segment of the telescoping...
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3842720 |
JET PUMP FOR AIRCRAFT CABIN PRESSURIZATION SYSTEM
The jet pump includes a primary nozzle in communication with the compressor section of the aircraft's turbine engine whereby primary air is bled from the engine for delivery through the primary...
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3728955 |
METHOD AND DEVICES FOR REGULATING THE PRESSURE AND ITS RATE OF VARIATION IN A CHAMBER
A method and devices for regulating the pressure of a compressible fluid in a chamber located in an atmosphere in which the pressure is variable, wherein a single pressure sensor inside the chamber...
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3630138 |
AIR-CONDITIONING SYSTEM WITH POSITIVE PRESSURIZATION
An air-conditioning system in which conditioned air is being provided to a compartment by a choked air-conditioning system having minimum and maximum mass flow rates and wherein an undersized...
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3592120 |
PROCESS OF PRESSURIZATION OF AIRCRAFT, WITH DIFFERENT PRESSURE VALUES IN ITS VARIOUS COMPARTMENTS
A method for controlling the interior pressure of an aircraft. The aircraft has at least one intermediate space situated between the interior cabin space of the aircraft and the exterior of the...
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3577902 |
DIGITAL INTEGRATOR
An aircraft cabin air pressure controller includes a digital integrator having a 1023 counter and a counter which is adjustable for counts of 1022, 1023, or 1024. The two counters are used with a...
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3537510 |
PRESSURE AND TEMPERATURE REGULATOR FOR AIRCRAFT BLEED AIR SYSTEM
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3511161 |
SELECTING THE AIR SOURCE FOR AN AIRCRAFT SUPERCHARGER
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3486435 |
AIRCRAFT PRESSURIZATION SYSTEM
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3453945 |
PREPROGRAMMED CABIN PRESSURIZATION SYSTEM
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3410191 |
Method and apparatus for atmosphere control in closed compartments
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