Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
204 words
A cartridge for ejecting chaff dipoles for use in an aircraft defense system to disrupt enemy radar, said cartridge comprising: (a) a shell for receiving a plurality of chaff dipoles, said shell having a base portion and an open mouth portion; (b) a plurality of chaff dipoles, said dipoles having at least first and second portions; (c) a pressurized gas cartridge mounted in the base of the cartridge for expelling said dipoles through said open mouth portion; (d) a first piston means mounted between said gas cartridge and said chaff dipoles, said first piston means having axially and forwardly extending spaced apart leg means that contact the inner walls of said cartridge and a portion of said dipoles, said piston and leg means retaining said first portion of chaff dipoles in their initial loaded position for a predetermined portion of their flight path after ejection; (e) a second piston means closing the mouth of said cartridge, said second piston having rearwardly and axially extending leg means for retaining said second portion of the dipoles after ejection: whereby the pressurized gas ejects the first piston, the chaff dipoles and said second piston to form an elongated pattern of dispersion a predetermined distance from said aircraft.
Claim 2
Dependent Claim
204 words
A cartridge for ejecting chaff dipoles for use in an aircraft defense system to disrupt enemy radar, said cartridge comprising: (a) a shell for receiving a plurality of chaff dipoles, said shell having a base portion and an open mouth portion; (b) a plurality of chaff dipoles, said dipoles having at least first and second portions; (c) a pressurized gas cartridge mounted in the base of the cartridge for expelling said dipoles through said open mouth portion; (d) a first piston means mounted between said gas cartridge and said chaff dipoles, said first piston means having axially and forwardly extending spaced apart leg means that contact the inner walls of said cartridge and a portion of said dipoles, said piston and leg means retaining said first portion of chaff dipoles in their initial loaded position for a predetermined portion of their flight path after ejection; (e) a second piston means closing the mouth of said cartridge, said second piston having rearwardly and axially extending leg means for retaining said second portion of the dipoles after ejection: whereby the pressurized gas ejects the first piston, the chaff dipoles and said second piston to form an elongated pattern of dispersion a predetermined distance from said aircraft.
Claim 3
Dependent Claim
152 words
A cartridge for ejecting chaff dipoles for use in an aircraft defense system to disrupt enemy radar, said cartridge comprising: (a) a shell for receiving a plurality of chaff dipoles, said shell having a base portion and an open mouth portion; (b) a plurality of chaff dipoles, said dipoles having at least first and second portions; (c) a pressurized gas cartridge mounted in the base of the cartridge for expelling said dipoles through said open mouth portion; (d) a first piston means mounted between said gas cartridge and said chaff dipoles, said first piston means having axially and forwardly extending narrow leg means that are spaced generally the width of the individual legs; (e) a second piston means closing the mouth of said cartridge: whereby the pressurized gas ejects the first piston, the chaff dipoles and said second piston to form an elongated pattern of dispersion a predetermined distance from said aircraft.
Claim 4
Dependent Claim
152 words
A cartridge for ejecting chaff dipoles for use in an aircraft defense system to disrupt enemy radar, said cartridge comprising: (a) a shell for receiving a plurality of chaff dipoles, said shell having a base portion and an open mouth portion; (b) a plurality of chaff dipoles, said dipoles having at least first and second portions; (c) a pressurized gas cartridge mounted in the base of the cartridge for expelling said dipoles through said open mouth portion; (d) a first piston means mounted between said gas cartridge and said chaff dipoles, said first piston means having axially and forwardly extending narrow leg means that are spaced generally the width of the individual legs; (e) a second piston means closing the mouth of said cartridge: whereby the pressurized gas ejects the first piston, the chaff dipoles and said second piston to form an elongated pattern of dispersion a predetermined distance from said aircraft.
Claim 5
Dependent Claim
207 words
A cartridge for ejecting chaff dipoles for use in an aircraft defense system to disrupt enemy radar, said cartridge comprising: (a) a shell for receiving a plurality of chaff dipoles, said shell having a base portion and an open mouth portion; (b) a plurality of chaff dipoles, said dipoles having at least first and second portions; (c) a pressurized gas cartridge mounted in the base of the cartridge for expelling said dipoles through said open mouth portion; (d) a first piston means mounted between said gas cartridge and said chaff dipoles, said first piston means having axially and forwardly extending spaced apart leg means that contact the inner walls of said cartridge and a portion of said dipoles, said piston and leg means retaining said first portion of chaff dipoles in their initial loaded position for a predetermined portion of their flight path after ejection; (e) a second piston means closing the mouth of the cartridge; (f) a mandrel mounted in the center of the first piston, said mandrel extending through said dipoles generally the length of said cartridge; whereby the pressurized gas ejects the first piston, the chaff dipoles, and the second piston to form an elongated pattern of dispersion a predetermined distance from said aircraft.
Claim 6
Dependent Claim
207 words
A cartridge for ejecting chaff dipoles for use in an aircraft defense system to disrupt enemy radar, said cartridge comprising: (a) a shell for receiving a plurality of chaff dipoles, said shell having a base portion and an open mouth portion; (b) a plurality of chaff dipoles, said dipoles having at least first and second portions; (c) a pressurized gas cartridge mounted in the base of the cartridge for expelling said dipoles through said open mouth portion; (d) a first piston means mounted between said gas cartridge and said chaff dipoles, said first piston means having axially and forwardly extending spaced apart leg means that contact the inner walls of said cartridge and a portion of said dipoles, said piston and leg means retaining said first portion of chaff dipoles in their initial loaded position for a predetermined portion of their flight path after ejection; (e) a second piston means closing the mouth of the cartridge; (f) a mandrel mounted in the center of the first piston, said mandrel extending through said dipoles generally the length of said cartridge; whereby the pressurized gas ejects the first piston, the chaff dipoles, and the second piston to form an elongated pattern of dispersion a predetermined distance from said aircraft.
Claim 7
Independent Claim
49 words
A device as claimed in claims 1 or 2 or 3 wherein said first piston means at the base of the shell further comprises a cylindrical extension for guidance and sealing in said shell, said extension being mounted in a cylindrical guide formed in the base of said shell.
Claim 8
Dependent Claim
23 words
A device as claimed in claim 4, wherein said extension further includes a cylindrical recess for receiving a portion of said gas cartridge.
Claim 9
Dependent Claim
27 words
A device as claimed in claim 4, which further comprises a groove formed in said extension at a mouth of said recess for receiving a sealing ring.
Claim 10
Dependent Claim
33 words
A device as claimed in claim 2 or 3, wherein said second piston in the mouth of said shell is cup-shaped and defines a groove adjacent said mouth for receiving a sealing ring.
Claim 11
Dependent Claim
25 words
A device as claimed in claim 1 or 2 or 3, said forwardly extending leg means clampingly contacting an inner wall defined by said shell.
Claim 12
Dependent Claim
22 words
A device as claimed in claim 8, wherein the length of the forwardly extending leg means generally corresponds to the shell cross-section.
Claim 13
Dependent Claim
42 words
A device as claimed in claim 1 or 2 or 3, which further comprises a spacer ring mounted in said shell between the first piston and the shell base portion, said ring having a groove formed therein for receiving a sealing ring.