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212 results about "Air Travels" patented technology

Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports

A mixer assembly for use in a combustion chamber of a gas turbine engine including a pilot mixer, a main mixer, and a fuel manifold. The pilot mixer includes: an annular pilot housing having a hollow interior; a primary fuel injector mounted in the pilot housing and adapted for dispensing droplets of fuel to the hollow interior of the pilot housing; a plurality of axial swirlers positioned upstream from the primary fuel injector, each of the plurality of swirlers having a plurality of vanes for swirling air traveling through the respective swirler to mix air and the droplets of fuel dispensed by the primary fuel injector; and, a plurality of secondary fuel injection ports for introducing fuel into the hollow interior of the pilot housing. The main mixer further includes: a main housing surrounding the pilot housing and defining an annular cavity; a plurality of fuel injection ports for introducing fuel into the cavity; and, at least one swirler positioned upstream from the plurality of fuel injection ports, each of the main mixer swirlers having a plurality of vanes for swirling air traveling through the respective swirler to mix air and the droplets of fuel dispensed by the main mixer fuel injection ports. The fuel manifold is in flow communication with the plurality of secondary fuel injection ports in the pilot mixer and the plurality of fuel injection ports in the main mixer.
Owner:GENERAL ELECTRIC CO

Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetration

A mixer assembly for use in a combustion chamber of a gas turbine engine includes a pilot mixer, a main mixer, and a fuel manifold positioned between the pilot mixer and main mixer. The pilot mixer includes an annular pilot housing having a hollow interior and a pilot fuel nozzle mounted in the housing and adapted for dispensing droplets of fuel to the hollow interior of the pilot housing. The main mixer includes: a main housing surrounding the pilot housing and defining an annular cavity having an upstream end and a downstream end including an upstream wall, an outer wall and an inner wall; a plurality of fuel injection ports for introducing fuel into the cavity, with the fuel injection ports being circumferentially spaced at a designated axial location of the inner wall of the annular cavity; and a swirler arrangement including at least one swirler in flow communication with the annular cavity, the swirler being incorporated into the outer wall of the annular cavity and extending from an upstream end to a downstream end, wherein each swirler of the arrangement has a plurality of vanes for swirling air traveling through such swirler to mix air and the droplets of fuel dispensed by the fuel injection ports. The main housing further includes a first plurality of passages oriented to provide air jets in a substantially axial direction into the annular cavity and a second plurality of passages oriented to provide air jets in a substantially radial direction into the annular cavity
Owner:GENERAL ELECTRIC CO

Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers

A mixer assembly for use in a combustor of a gas turbine engine, including a pilot mixer, a main mixer, and a fuel manifold positioned between the pilot mixer and the main mixer. The pilot mixer further includes an annular pilot housing having a hollow interior and a pilot fuel nozzle mounted in the pilot housing and adapted for dispensing droplets of fuel to the hollow interior of the pilot housing. The main mixer further includes a main housing surrounding the pilot housing and defining an annular cavity, a plurality of fuel injection ports for introducing fuel into the cavity, and a swirler arrangement including at least three swirlers positioned upstream from the plurality of fuel injection ports, wherein each swirler of the swirler arrangement has a plurality of vanes for swirling air traveling through the respective swirler to mix air and the droplets of fuel dispensed by the fuel injection ports. The swirlers are oriented substantially radially to a centerline axis through the mixer assembly or at an acute angle to the centerline axis through the mixer assembly. Alternatively, at least two swirlers are included substantially parallel to the centerline axis through the mixer assembly along with one or more radial or conical swirlers. In another alternative, the swirler arrangement includes a first swirler oriented substantially parallel to a centerline axis through the mixer assembly, a second swirler oriented at an acute angle to the centerline axis through the mixer assembly, and a third swirler oriented substantially radially to the centerline axis through the mixer assembly.
Owner:GENERAL ELECTRIC CO

Intelli-voyage travel

A system to improve user messaging in a mobile device by providing an intelligent interactive travel as a GUI that receives verbal and text input and outputs offers to provide travel-related information, offers to provide travel-related actions, offers to send a travel-related communication, or offers to save travel-related information, wherein processing content of the user input comprises analyzing message content to collect travel-related parameters relating to geographic travel path, airport information, air travel route information, airline flight information, flight availability, flight status, flight booking information, flight cancelling information, airport fees, baggage fees, local and remote ground transportion options, local and remote weather information, message priority, channel type, channel availability, user schedule, user time zone, user time and date, user travel-related preferences, type of content, and number of recipients, and saving said collected parameters to memory, wherein the travel-related parameter is calculated using a travel-related index, the travel-related index comprising a numerical value based on travel-related hierarchy, wherein the one or more programs include instructions for providing feedback to the user wherein the feedback comprises a graphical or spoken output from the portable electronic device, said output comprising information linked to the user schedule and one or more travel-related parameters, wherein the user schedule parameter is compared to a travel-related parameter and a scheduling database is populated with an entry that uses the comparison data and, wherein specific customized travel-related profile parameters are set to establish priority overrides where a user schedule has a different priority than a travel-related parameter.
Owner:VADODARIA VISHAL

Air-assisted fuel injector for mixer assembly of a gas turbine engine combustor

A mixer assembly for use in a combustion chamber of a gas turbine engine includes a pilot mixer, a main mixer, and a fuel manifold positioned between the pilot mixer and main mixer. The pilot mixer includes an annular pilot housing having a hollow interior and a pilot fuel nozzle mounted in the housing and adapted for dispensing droplets of fuel to the hollow interior of the pilot housing. The main mixer includes: a main housing surrounding the pilot housing and defining an annular cavity; a plurality of fuel injection ports for introducing fuel into the cavity; a post member associated with and extending from each fuel injection port to an inner surface of said annular cavity, the post member including an inner passage therethrough in flow communication with the fuel injection port; a passage surrounding each post member, wherein air is provided therefrom to envelop fuel injected into the annular cavity; and, a swirler arrangement including at least one swirler positioned upstream from the fuel injection ports, wherein each swirler of the arrangement has a plurality of vanes for swirling air traveling through such swirler to mix air and the droplets of fuel dispensed by the fuel injection ports. The air through the passages is either injected substantially straight through or swirled a predetermined amount.
Owner:GENERAL ELECTRIC CO

Intelligent air travel tag for asset self-tracking

A system for luggage self-tracking/identification during air travel involves a programmable, wireless LAN active transceiver preferably located inside each piece of luggage, with controlled access to the airlines' luggage tracking networks. Prior to a flight, each transceiver is loaded with the passenger's itinerary, and logged in the airline's network at check-in. Each transceiver is uniquely identifiable by the luggage tracking network. An example of a preferred identifier would be the utilization of its Medium Access Control (MAC) and its alphanumeric serial keyword to provide unique and secure registration/identification of the transceiver in the airline's network. During the trip, which may include different stopovers before reaching the final destination, the transceiver is able to automatically compare its programmed itinerary with its current location via wireless access to the airports and aircraft wireless LANs. In this way, the transceiver is able to notify airline personnel if there is a disagreement between its programmed itinerary and its current location, thus preventing misrouting. The transceiver's itinerary can be wirelessly re-programmed by airline personnel/network to account for flight changes or delays. Finally, the transceiver has an internal timer that starts counting down from the expected “total traveling time”, accounting for flight changes or delays. If this timer elapses without the itinerary being complete, the transceiver connects to a wireless access point (hotspot) to report itself as a missing luggage, avoiding a worldwide tracking initiative and speeding up recovery time.
Owner:DEFERO SYST

Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers

A mixer assembly for use in a combustor of a gas turbine engine, including a pilot mixer, a main mixer, and a fuel manifold positioned between the pilot mixer and the main mixer. The pilot mixer further includes an annular pilot housing having a hollow interior and a pilot fuel nozzle mounted in the pilot housing and adapted for dispensing droplets of fuel to the hollow interior of the pilot housing. The main mixer further includes a main housing surrounding the pilot housing and defining an annular cavity, a plurality of fuel injection ports for introducing fuel into the cavity, and a swirler arrangement including at least three swirlers positioned upstream from the plurality of fuel injection ports, wherein each swirler of the swirler arrangement has a plurality of vanes for swirling air traveling through the respective swirler to mix air and the droplets of fuel dispensed by the fuel injection ports. The swirlers are oriented substantially radially to a centerline axis through the mixer assembly or at an acute angle to the centerline axis through the mixer assembly. Alternatively, at least two swirlers are included substantially parallel to the centerline axis through the mixer assembly along with one or more radial or conical swirlers. In another alternative, the swirler arrangement includes a first swirler oriented substantially parallel to a centerline axis through the mixer assembly, a second swirler oriented at an acute angle to the centerline axis through the mixer assembly, and a third swirler oriented substantially radially to the centerline axis through the mixer assembly.
Owner:GENERAL ELECTRIC CO

High-performance carbon fiber pre-oxidation furnace

ActiveCN102758270AAvoid burnsPrevention of legitimate discharge problemsFibre chemical featuresFiberCarbon fibers
The invention discloses a high-performance carbon fiber pre-oxidation furnace which is specially designed for carrying out heat treatment on a high-performance carbon fiber material at a temperature below 350 DEG C. A furnace body is designed into a building block structure and is convenient to assemble and disassemble. For the design of the furnace, the requirements of a preparation process of the high-performance carbon fiber material are fully considered and understood and the key special requirements of the preparation process of the high-performance carbon fiber material are met to the greatest extent. According to the requirements of the preparation process of the material, a circulating hot air heating mode is adopted for the pre-oxidation furnace; for a circulating air traveling mode, air is blown to two ends of the furnace body from the middle of the furnace body; and a plurality of heat treatment cavities are connected in series and in parallel to form a system with a certain temperature gradient. An anticorrosion stainless steel structure is adopted for an inner hearth totally; a full-fiber superlight material is adopted as a heat insulating material to carry out heat insulation; a PLC (Programmable Logic Controller) temperature control module is used for temperature control and has the characteristics of high temperature control accuracy, high temperature stability and the like; and according to the pre-oxidation furnace, in a pre-oxidation process, the problems of low heat treatment efficiency, inaccurate temperature control and unideal temperature uniformity in the heat treatment cavities are solved, protofilament combustion is prevented, sufficient supplementation of the oxygen content in the hearth is realized and waste gas is reasonably discharged. The integral high-performance carbon fiber pre-oxidation furnace has relatively low energy consumption and is durable.
Owner:HEFEI RISINE HEATEK
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