Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
93 words
A method for separating particles from a gas stream in a vacuum chamber comprising passing said stream of gas containing particles to be separated into said vacuum chamber through a capillary inlet at a supersonic speed to form a standing barrel shock wave extending from said capillary inlet to the surface of a skimmer having an axially concentric outlet and to form a particle beam axially concentric therewith and passing out of said vacuum chamber through said outlet, said outlet extending through the Mach disk of said shock wave and being unobstructed thereby.
Claim 2
Independent Claim
93 words
A method for separating particles from a gas stream in a vacuum chamber comprising passing said stream of gas containing particles to be separated into said vacuum chamber through a capillary inlet at a supersonic speed to form a standing barrel shock wave extending from said capillary inlet to the surface of a skimmer having an axially concentric outlet and to form a particle beam axially concentric therewith and passing out of said vacuum chamber through said outlet, said outlet extending through the Mach disk of said shock wave and being unobstructed thereby.
Claim 3
Dependent Claim
21 words
The method of claim 1 wherein said skimmer has a conical outer surface forming an angle between 40° and 70° .
Claim 4
Dependent Claim
191 words
A particle beam separator comprising: a first vacuum chamber; introduction means for introducing a time-varying mixture of gas and particles into said first vacuum chamber so as to define a supersonic jet therein, said supersonic jet forming a standing barrel shock wave having a Mach disk and a central axis, said particles forming a particle beam extending along said central axis and substantially confined to a radially inward cross section of said shock wave, said cross section taken orthogonally to said central axis; a first skimmer having a first conical surface which radially narrows to a first apex opposed to said introduction means, said first conical surface forming a first outer angle between 40° and 70° so that said shock wave attaches thereto, said first skimmer having a first aperture in said first apex, said first aperture being axially aligned with said central axis, said first apex being spaced so that said first skimmer pierces said Mach disk so that said particle beam exits said first vacuum chamber via said first aperture and so that most of said gas is diverted along said conical surface; and a first vacuum exhaust port.
Claim 5
Dependent Claim
191 words
A particle beam separator comprising: a first vacuum chamber; introduction means for introducing a time-varying mixture of gas and particles into said first vacuum chamber so as to define a supersonic jet therein, said supersonic jet forming a standing barrel shock wave having a Mach disk and a central axis, said particles forming a particle beam extending along said central axis and substantially confined to a radially inward cross section of said shock wave, said cross section taken orthogonally to said central axis; a first skimmer having a first conical surface which radially narrows to a first apex opposed to said introduction means, said first conical surface forming a first outer angle between 40° and 70° so that said shock wave attaches thereto, said first skimmer having a first aperture in said first apex, said first aperture being axially aligned with said central axis, said first apex being spaced so that said first skimmer pierces said Mach disk so that said particle beam exits said first vacuum chamber via said first aperture and so that most of said gas is diverted along said conical surface; and a first vacuum exhaust port.
Claim 6
Dependent Claim
34 words
The separator of claim 3 wherein said first skimmer defines a first plane through said first apex and orthogonal to said central axis, said first vacuum exhaust port being downstream of said first plane.
Claim 7
Dependent Claim
87 words
The separator of claim 4 further comprising: a second vacuum chamber downstream of and communicating with said first aperture; said a second skimmer having a second apex with a second aperture second aperture being coaxial with said central axis and in communication with said second vacuum chamber, said second skimmer being downstream of said second vacuum chamber so that said particle beam exits and second vacuum chamber via said second aperture and said gas is further separated from said particle beam; and a second vacuum exhaust port.
Claim 8
Dependent Claim
34 words
The separator of claim 5 wherein said second skimmer defines a second plane through said second apex and orthogonal to said central axis, said second vacuum exhaust port being downstream of said second plane.
Claim 9
Dependent Claim
14 words
The separator of claim 4 wherein said introduction means includes a capillary inlet tube.
Claim 10
Dependent Claim
55 words
The separator of claim 7 wherein said introduction means further includes: nebulizer means for dispersing into droplets a time-varying solution containing solvent and sample compounds to be analyzed; and desolvation means for evaporating said solvent from said droplets to provide that said sample compounds are largely desolvated, said desolvation means communicating with said nebulizer means.
Claim 11
Dependent Claim
333 words
A liquid chromatograph to mass spectrometer interface comprising: nebulizer means for dispersing into droplets a time-varying solution containing solvent and sample compounds to be analyzed; desolvation means for evaporating said solvent from said droplets so that said sample compounds are largely desolated, said desolvation means communicating with said nebulizer means; a first vacuum chamber; introduction means for introducing a time-varying mixture of gas and particles into said first vacuum chamber so as to define a supersonic jet therein, said supersonic jet forming a standing barrel shock wave having a central axis, said particles forming a particle beam extending along said central axis and substantially confined to a radially inward cross section of said shock wave, said cross section taken orthogonally to said central axis; a first skimmer having a first conical surface which radially narrows to a first apex opposed to said introduction means, said first conical surface forming a first outer angle between 40° and 70° so that said shock wave attaches thereto, said first skimmer having a first aperture in said first apex, said first aperture being axially aligned with said central axis, said first skimmer defining a first plane through said first apex and orthogonal to said central axis said first apex being spaced so that said first skimmer pierces said Mach disk so that said particle beam exists said first vacuum chamber via said first aperture and so that most of said gas is diverted along said conical surface; a first vacuum exhaust port downstream of said first plane; a second vacuum chamber downstream of and communicating with said first aperture; a second skimmer having a second apex with a second aperture, said second aperture being coaxial with said central axis and in communication with said second vacuum chamber, said second skimmer being downstream of said second vacuum chamber so that said particle beam exits said second vacuum chamber via said second aperture and said gas is further separated from said particle beam; and a second vacuum exhaust port.
Claim 12
Dependent Claim
333 words
A liquid chromatograph to mass spectrometer interface comprising: nebulizer means for dispersing into droplets a time-varying solution containing solvent and sample compounds to be analyzed; desolvation means for evaporating said solvent from said droplets so that said sample compounds are largely desolated, said desolvation means communicating with said nebulizer means; a first vacuum chamber; introduction means for introducing a time-varying mixture of gas and particles into said first vacuum chamber so as to define a supersonic jet therein, said supersonic jet forming a standing barrel shock wave having a central axis, said particles forming a particle beam extending along said central axis and substantially confined to a radially inward cross section of said shock wave, said cross section taken orthogonally to said central axis; a first skimmer having a first conical surface which radially narrows to a first apex opposed to said introduction means, said first conical surface forming a first outer angle between 40° and 70° so that said shock wave attaches thereto, said first skimmer having a first aperture in said first apex, said first aperture being axially aligned with said central axis, said first skimmer defining a first plane through said first apex and orthogonal to said central axis said first apex being spaced so that said first skimmer pierces said Mach disk so that said particle beam exists said first vacuum chamber via said first aperture and so that most of said gas is diverted along said conical surface; a first vacuum exhaust port downstream of said first plane; a second vacuum chamber downstream of and communicating with said first aperture; a second skimmer having a second apex with a second aperture, said second aperture being coaxial with said central axis and in communication with said second vacuum chamber, said second skimmer being downstream of said second vacuum chamber so that said particle beam exits said second vacuum chamber via said second aperture and said gas is further separated from said particle beam; and a second vacuum exhaust port.