John Thomas Stanko, 532117 Greenway Ave, Prior Lake, MN 55379

6360992, Mar 26, 2002

Apr 10, 2000

09/546121

John Stanko - Rolling Hills Estates CA
Lowell Pearson - Hermosa Beach CA

Honeywell International Inc. - Morristown NJ

B64D 1500

244134R, 244134 C, 239296, 239290

A hybrid deicing system for deicing ice or snow covered surfaces comprises a source of pressurized air and a source of pressurized deicing fluid. A nozzle assembly receives the pressurized air and the pressurized deicing fluid at a forward position, a middle position or a rearward position of the nozzle assembly. The nozzle assembly discharges the pressurized deicing fluid and pressurized air as a first independent stream within a second independent stream.

7431240, Oct 7, 2008

Aug 17, 2000

09/640063

John Stanko - Redondo Beach CA, US
Lowell Pearson - Hermosa Beach CA, US

Honeywell International Inc. - Morristown NJ

B64D 15/00

244134C, 244134 R, 239722, 134123

This invention overcome the disadvantage of the prior systems and produces a high velocity specially formed and constituted pressure aerodynamic stream for efficiently and effectively removing ice from an aircraft. The specially formed stream includes a stream within a stream, wherein a deicing fluid such a glycol is entrained within and encased by a surrounding jacket of entraining fluid such air. This deicing is now known as coaxial stream/stream within a stream deicing. The special nozzle allows the stream to maintain fluid separation over its flight path so that aircraft contact is made by to be known as coaxial stream/stream within a stream deicing. The coaxial stream/stream within a stream deicing is further enhanced by pressurizing the stream to deliver the stream as a high pressure high velocity stream to improved the aerodynamic sweeping action of the airstream.

6293498, Sep 25, 2001

Feb 18, 2000

9/507404

John Stanko - Redondo Beach CA
Lowell Pearson - Hermosa Beach CA

Honeywell International Inc. - Morristown NJ

B64D 1500

244134R

This invention overcomes the disadvantage of the prior systems and produces a high velocity specially formed and constituted pressure aerodynamic stream system for efficiently and effectively removing ice from an aircraft. The specially formed stream system includes a stream within a stream, wherein a deicing fluid such a glycol is entrained within and encased by a surrounding jacket of entraining fluid such as air. This deicing is now known as coaxial stream/stream within a stream deicing. The special nozzle allows the stream to maintain fluid separation over its flight path so that aircraft contact is made by to be known as coaxial stream/stream within a stream deicing. The coaxial stream/stream within a stream deicing is further enhanced by pressurizing the stream to deliver the stream as a high pressure, high velocity stream to improve the aerodynamic sweeping action of the airstream.

6047926, Apr 11, 2000

Jun 17, 1997

8/877272

John Stanko - Redondo Beach CA
Lowell Pearson - Hermosa Beach CA

AlliedSignal Inc. - Morristown NJ

B64D 1500
F23D 1110
B08B 300

244134R

This invention overcomes the disadvantage of the prior systems and produces a high velocity specially formed and constituted pressure aerodynamic stream system for efficiently and effectively removing ice from an aircraft. The specially formed stream system includes a stream within a stream, wherein a deicing fluid such a glycol is entrained within and encased by a surrounding jacket of entraining fluid such as air. This deicing is now known as coaxial stream/stream within a stream deicing. The special nozzle allows the stream to maintain fluid separation over its flight path so that aircraft contact is made by to be known as coaxial stream/stream within a stream deicing. The coaxial stream/stream within a stream deicing is further enhanced by pressurizing the stream to deliver the stream as a high pressure, high velocity stream to improve the aerodynamic sweeping action of the airstream.