Automatic nozzle for firefighting systems

1. An automatic nozzle ( 10 ) for firefighting low-pressure water mist systems comprising a nozzle body ( 200 ) and shutter means ( 107 ), said nozzle body ( 200 ) comprising a plurality of axial-symmetric components ( 101 - 106 ) defining an inlet opening and a plurality of inner cavities, which are fluid-dynamic connected each other by means of one or more openings, being said components ( 101 - 106 ) located in a way to share the same symmetry axis and configured to generate:

a radial spray ( 10 ′) through a circumferential opening ( 15 ), which extends all over the circumference of a second component ( 102 ), said circumferential opening ( 15 ) being formed between a base ( 14 ) of a cylindrical wall of the second component ( 102 ) and an upper surface ( 16 ) of a hollow body ( 13 ) of a third component ( 103 ), and

two or more full cone sprays ( 10 ″) by means of the fluid passage through cylindrical openings ( 26 ) on a circular and axial-symmetric body ( 24 ) of a fifth component ( 105 ), configured to define a turbulent motion of the fluid in at least two correspondent cylindrical cavities ( 23 ) of a fourth component ( 104 ), said two or more full cone sprays ( 10 ″) out coming through at least two orifices ( 22 ) fed by the at least two correspondent cylindrical cavities ( 23 ),

wherein said axis of each of said cylindrical openings ( 26 ) of the fifth component ( 105 ) is inclined of a first angle (β) ranging between 10° and 80° with respect to an upper surface (S) of the circular and axial-symmetric body ( 24 ), the axis of each of said cylindrical openings ( 26 ) has a second inclination of a second angle (γ) ranging between 30° e 90° and laying on a plane (FF), which is tangent to the upper surface (S) of the circular and axial-symmetric body ( 24 ) and contains the intersection points (R′, R) between the upper surface (S) and the axis of said cylindrical openings ( 26 ) converging towards a same orifice of the two or more orifices ( 22 ), said second angle (γ) being comprised between the projection of the axis of said cylindrical openings ( 26 ) on the plane (FF) and a straight line (r), passing through the intersection points (R′, R″);

and wherein said cylindrical openings ( 26 ) fluid-dynamically connect an internal cavity ( 19 ) of the fourth component ( 104 ) with cylindrical cavities ( 23 ) of the same fourth component ( 104 ), localized upstream of the at least two orifices ( 22 ).

2. The automatic nozzle ( 10 ) according to claim 1 , wherein said upper surface ( 16 ) of the hollow body ( 13 ) of the third component ( 103 ) and said base ( 14 ) of an annular edge ( 6 ) of the second component ( 102 ) have correspondent external radius which differ of a length (ΔI_) greater or equal to 1 mm.

3. The automatic nozzle ( 10 ) according to claim 1 wherein said upper surface ( 16 ) of the hollow body ( 13 ) of the third component ( 103 ), creating the circumferential opening ( 15 ) of the radial spray ( 10 ′), in its radially inner portion is shaped to form a recess ( 31 ) with the annular edge ( 6 ) of a cylindrical central body ( 3 ) of the second component ( 102 ), to create in an annular cavity ( 7 ) fluid vortexes, which improve water nebulization at the exit of the circumferential opening ( 15 ).

4. The automatic nozzle ( 10 ) according to claim 1 , wherein said upper surface ( 16 ) of the hollow body ( 13 ) of the third component ( 103 ) comprises a radially outer surface ( 16 ″), forming a gap ( 32 ), whose width gradually increases toward the water exit, to break the water layer in small droplets.

5. The automatic nozzle ( 10 ) according to claim 1 , wherein said at least two or more orifices ( 22 ) are inclined of an angle (a) ranging between 10° and 80° with respect to the symmetry axis of the fourth component ( 104 ).

6. The automatic nozzle ( 10 ) according to claim 1 , wherein said second component ( 102 ) comprises the cylindrical central body ( 3 ) having an opening ( 4 ), which is co-axial to the cylindrical central body ( 3 ) and crosses the cylindrical central body ( 3 ) all over its length, and the annular edge ( 6 ), co-axial to the cylindrical central body ( 3 ) and having a smaller height than the cylindrical central body ( 3 ).

7. The automatic nozzle ( 10 ) according to claim 6 , wherein said cylindrical central body ( 3 ) of the second component ( 102 ) comprises one or more not co-axial openings ( 5 ), which cross the cylindrical central body all over its length.

8. The automatic nozzle ( 10 ) according to claim 6 wherein said cylindrical central body ( 3 ) and the annular edge ( 6 ) create an annular cavity ( 7 ), which is closed on one side by a wall ( 8 ) and open on the opposite side, where the third component ( 103 ) is steadily connected.

9. The automatic nozzle ( 10 ) according to claim 1 , wherein said fifth component ( 105 ) comprises the circular and axial-symmetric body ( 24 ), having a thickness smaller than the maximum diameter of said circular and axial-symmetric body ( 24 ) and a central passing-through opening ( 25 ), which completely crosses the circular and axial-symmetric body ( 24 ).

10. The automatic nozzle ( 10 ) according to claim 1 , wherein said shutter means ( 107 ) comprise a cylindrical body ( 28 ), crossing all components ( 101 - 106 ) of the nozzle body ( 200 ) and is co-axial to said further components.

11. The automatic nozzle ( 10 ) according to claim 10 , wherein said shutter means ( 107 ) comprise at the lower end a cavity ( 29 ), which is suitable to accommodate an end of a thermal bulb ( 27 ) and at the upper end a seat ( 30 ), which is suitable to accommodate sealing means ( 33 ), which, adhering at the inner walls of a second opening ( ) of a first component ( 101 ), prevent water passages, when the thermal bulb ( 27 ) is not broken.