Anti-icing system for aircraft

Claim 2

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. a fan means having an inlet to receive air from said chamber and to move said air to the inlet portion of the tube means, c. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, d. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, e. power supply and control means adapted to selectively supply electric power as a main eergy source to, and cause operation of, said fan means and said heater to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member, f. wherein said aircraft structure comprising a leading edge structure, and said system comprising a modular system which can be inserted in, and removed from, said leading edge structure, g. said leading edge structure being a movable leading edge device mounted to a main structure, and said system being positioned totally in said leading edge device.

Claim 3

The system as recited in claim 1, wherein said surface member comprises a skin portion of said leading edge structure, and said chamber comprises an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means.

Claim 4

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. a fan means having an inlet to receive air from said chamber and to move said air to the inlet portion of the tube means, c. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, d. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, e. power supply and control means adapted to selectively supply electric power as a main energy source to, and cause operation of, said fan means and said heater to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member, f. said valve means comprising an outlet valve and an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet valve being drawn into the venturi entrance portion to pass through the fan means.

Claim 5

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. a fan means having an inlet to receive air from said chamber and to move said air to the inlet portion of the tube means, c. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, d. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, e. power supply and control means adapted to selectively supply electric power as a main energy source to, and cause operation of, said fan means and said heater to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member, f. said valve means comprising an outlet valve and an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet valve being drawn into the venturi entrance portion to pass through the fan means.

Claim 6

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. a fan means having an inlet to receive air from said chamber and to move said air to the inlet portion of the tube means, c. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, d. pressure relief valve means communicating between said chamber and an ambient air location. said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, e. power supply and control means adapted to selectively supply electric power as a main energy source to, and cause operation of, said fan means and said heater to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member, f. said aircraft structure comprising a leading edge structure, and said system comprising a modular system which can be inserted in, and removed from, said leading edge structure, g. said leading edge structure being a moveable leading edge device mounted to a main structure, and said system being positioned totally in said leading edge device, h. said surface member comprising a skin portion of said leading edge structure, and said chamber comprising an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means, i. said fan means being located in an upstream direction, relative to flow of air in the system, from the heater, so that air from the fan means passes through the heater and then to the inlet of the tube means, j. said valve means comprising an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet valve being drawn into the venturi entrance portion to pass through the fan means.

Claim 7

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. a fan means having an inlet to receive air from said chamber and to move said air to the inlet portion of the tube means, c. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, d. pressure relief valve means communicating between said chamber and an ambient air location. said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, e. power supply and control means adapted to selectively supply electric power as a main energy source to, and cause operation of, said fan means and said heater to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member, f. said aircraft structure comprising a leading edge structure, and said system comprising a modular system which can be inserted in, and removed from, said leading edge structure, g. said leading edge structure being a moveable leading edge device mounted to a main structure, and said system being positioned totally in said leading edge device, h. said surface member comprising a skin portion of said leading edge structure, and said chamber comprising an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means, i. said fan means being located in an upstream direction, relative to flow of air in the system, from the heater, so that air from the fan means passes through the heater and then to the inlet of the tube means, j. said valve means comprising an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet valve being drawn into the venturi entrance portion to pass through the fan means.

Claim 8

An electrically powered deicing system for an aircraft having a plurality of surface members, each of which has an exposed surface area upon which ice tends to collect, with each surface member defining a related enclosed chamber adjacent thereto, said system comprising: a. a plurality of deicing units, each of said units comprising: 1. a hot air distribution tube means having an inlet portion, said tube means being positioned in the chamber of a related surface member and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with its related surface member,

Claim 9

An electrically powered deicing system for an aircraft having a plurality of surface members, each of which has an exposed surface area upon which ice tends to collect, with each surface member defining a related enclosed chamber adjacent thereto, said system comprising: a. a plurality of deicing units, each of said units comprising: 1. a hot air distribution tube means having an inlet portion, said tube means being positioned in the chamber of a related surface member and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with its related surface member,

Claim 10

a fan means having an inlet to receive air from said related chamber and to move said air to the inlet portion of the tube means, 3. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with this surface member, 4. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, 5. at least some of said surface members being leading edge member, and each deicing unit for the leading edge members comprising a modular unit which can be inserted in, and removed from, said leading edge members. 6. at least some of surface members being a movable leading edge device mounted to a main structure, with each related modular unit for the leading edge devices being positioned totally in its related leading edge device, b. control means adapted to selectively supply power to, and cause operation of, said fan means and said heater of each of said deicing units to cause heated air to be directed selectively through the distribution tube means of selected deicing units whereby said deicing units can be operated sequentially so as to minimize peak power requirements for the system.

Claim 11

a fan means having an inlet to receive air from said related chamber and to move said air to the inlet portion of the tube means, 3. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with this surface member, 4. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, 5. at least some of said surface members being leading edge member, and each deicing unit for the leading edge members comprising a modular unit which can be inserted in, and removed from, said leading edge members. 6. at least some of surface members being a movable leading edge device mounted to a main structure, with each related modular unit for the leading edge devices being positioned totally in its related leading edge device, b. control means adapted to selectively supply power to, and cause operation of, said fan means and said heater of each of said deicing units to cause heated air to be directed selectively through the distribution tube means of selected deicing units whereby said deicing units can be operated sequentially so as to minimize peak power requirements for the system.

Claim 12

The system as recited in claim 5, wherein each of said surface members comprises a skin portion of said leading edge structure, and said chamber comprises an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means.

Claim 13

An electrically powered deicing system for an aircraft having a plurality of surface members, each of which has an exposed surface area upon which ice tends to collect, with each surface member defining a related enclosed chamber adjacent thereto, said system comprising: a. a plurality of deicing units, each of said units comprising: 1. a hot air distribution tube means having an inlet portion, said tube means being positioned in the chamber of a related surface member and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with its related surface member, 2. a fan means having an inlet to receive air from said related chamber and to move said air to the inlet portion of the tube means, 3. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, 4. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, 5. said valve means of each deicing unit comprising an outlet valve and an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet valve being drawn into the venturi entrance portion to pass through the fan means, b. control means adapted to selectively supply power to, and cause operation of, said fan means and said heater of each of said deicing units to cause heater air to be directed selectively through the distribution tube means of selected deicing units whereby said deicing units can be operated sequentially so as to minimize peak power requirements for the system.

Claim 14

An electrically powered deicing system for an aircraft having a plurality of surface members, each of which has an exposed surface area upon which ice tends to collect, with each surface member defining a related enclosed chamber adjacent thereto, said system comprising: a. a plurality of deicing units, each of said units comprising: 1. a hot air distribution tube means having an inlet portion, said tube means being positioned in the chamber of a related surface member and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with its related surface member, 2. a fan means having an inlet to receive air from said related chamber and to move said air to the inlet portion of the tube means, 3. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, 4. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, 5. said valve means of each deicing unit comprising an outlet valve and an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet valve being drawn into the venturi entrance portion to pass through the fan means, b. control means adapted to selectively supply power to, and cause operation of, said fan means and said heater of each of said deicing units to cause heater air to be directed selectively through the distribution tube means of selected deicing units whereby said deicing units can be operated sequentially so as to minimize peak power requirements for the system.

Claim 15

An electrically powered deicing system for an aircraft having a plurality of surface membsrs, each of which has an exposed surface area upon which ice tends to collect, with each surface member defining a related enclosed chamber adjacent thereto, said system comprising: a. a plurality of deicing units, each of said units comprising: 1. a hot air distribution tube means having an inlet portion, said tube means being positioned in the chamber of a related surface member and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with its related surface member, 2. a fan means having an inlet to receive air from said related chamber and to move said air to the inlet portion of the tube means, 3. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, 4. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, b. control means adapted to selectively supply power to, and cause operation of, said fan means and said heater of each of said deicing units to cause heated air to be directed selectively through the distribution tube means of selected deicing units, c. at least some of said surface members being leading edge members, and each deicing unit comprising a modular unit which can be inserted in, and removed from, said leading edge structure, d. at least some of said surface members being a movable leading edge device mounted to a main structure, with a related modular unit being positioned totally in said leading edge device, e. each of said surface members comprising a skin portion of said leading edge structure, and said chamber comprising an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means, f. each of said fan means being located in an upstream direction, relative to flow of air in the system, from the heater, so that air from the fan means passes through the heater and then to the inlet of the tube means, g. said valve means of each deicing unit comprising an outlet valve and an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet value being drawn into the venturi entrance portion to pass through the fan means, whereby said deicing units can be operated sequentially so as to minimize peak power requirements for the system.

Claim 16

An electrically powered deicing system for an aircraft having a plurality of surface membsrs, each of which has an exposed surface area upon which ice tends to collect, with each surface member defining a related enclosed chamber adjacent thereto, said system comprising: a. a plurality of deicing units, each of said units comprising: 1. a hot air distribution tube means having an inlet portion, said tube means being positioned in the chamber of a related surface member and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with its related surface member, 2. a fan means having an inlet to receive air from said related chamber and to move said air to the inlet portion of the tube means, 3. an electric heater arranged to heat the air which travels through the tube means and is discharged in heat exchange relationship with the surface member, 4. pressure relief valve means communicating between said chamber and an ambient air location, said valve means being arranged to discharge air from the chamber when pressure in the chamber exceeds a predetermined pressure level, and to admit ambient air into said chamber when pressure in the chamber is below a predetermined pressure level, b. control means adapted to selectively supply power to, and cause operation of, said fan means and said heater of each of said deicing units to cause heated air to be directed selectively through the distribution tube means of selected deicing units, c. at least some of said surface members being leading edge members, and each deicing unit comprising a modular unit which can be inserted in, and removed from, said leading edge structure, d. at least some of said surface members being a movable leading edge device mounted to a main structure, with a related modular unit being positioned totally in said leading edge device, e. each of said surface members comprising a skin portion of said leading edge structure, and said chamber comprising an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means, f. each of said fan means being located in an upstream direction, relative to flow of air in the system, from the heater, so that air from the fan means passes through the heater and then to the inlet of the tube means, g. said valve means of each deicing unit comprising an outlet valve and an inlet valve positioned to admit air into the inlet of the fan means, the inlet of the fan means being provided with a venturi entrance portion, with ambient air passing through the inlet value being drawn into the venturi entrance portion to pass through the fan means, whereby said deicing units can be operated sequentially so as to minimize peak power requirements for the system.

Claim 17

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. an electrically powered compressor means having an inlet to receive air from said chamber and to compress said air to an extent to cause a sufficient rise in temperature of said air sufficient to accomplish adequate deicing, and then move said air to the inlet portion of the tube means, c. power supply and control means adapted to selectively supply electric power to, and cause operation of, said compressor means to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member to cause said adequate deicing, d. said aircraft structure comprising a leading edge structure, and said system comprising a modular system which can be inserted in, and removed from, said leading edge structure, e. said leading edge structure being a moveable leading edge device mounted to a main structure, said system being positioned totally in said leading edge device.

Claim 18

An electrically powered deicing system for an aircraft structure which has a surface member having an exposed surface area upon which ice tends to collect, and which defines an enclosed chamber adjacent thereto, said system comprising: a. a hot air distribution tube means having an inlet portion, said tube means being positioned in said chamber and having outlets to discharge hot air into said chamber so as to be in heat exchange relationship with said surface member, b. an electrically powered compressor means having an inlet to receive air from said chamber and to compress said air to an extent to cause a sufficient rise in temperature of said air sufficient to accomplish adequate deicing, and then move said air to the inlet portion of the tube means, c. power supply and control means adapted to selectively supply electric power to, and cause operation of, said compressor means to cause heated air to be directed through said distribution tube means and in heat exchange relationship with the surface member to cause said adequate deicing, d. said aircraft structure comprising a leading edge structure, and said system comprising a modular system which can be inserted in, and removed from, said leading edge structure, e. said leading edge structure being a moveable leading edge device mounted to a main structure, said system being positioned totally in said leading edge device.

Claim 19

The system as recited in claim 9, wherein said surface member comprises a skin portion of said leading edge structure, and said chamber comprises an elongate duct having a lengthwise axis along said leading edge structure, said elongate duct serving as a return passageway to return air discharged from the tube means back to the fan means.

Claim 20

The system as recited in claim 10, wherein said compressor means comprises an electric motor positioned to be in heat exchange relationship with air passing into said tube means, whereby heat generated by said motor is utilized for deicing.