Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
167 words
A centrifugal blower comprising a rotatable impeller and a volute positioned circumferentially around at least a portion of the impeller to receive airflow from the impeller and direct it to a volute exit, the blower being designed to produce a preestablished airflow from said volute exit, a) said volute being characterized by an axial dimension H which changes as a function of Θ, the angular displacement from the volute exit, and said volute being characterized by a radial dimension G which changes as a function of Θ; b) at least one of the function G(Θ) and H(Θ) being characterized by an abrupt discontinuity, and the functions G(Θ) and H(Θ) being related as follows: G(Θ)=g.sub.o (Θ.sup.h·tanα·/H(Θ) -1), where g o is a constant; h is the axial dimension of the volute at the volute origin; and α is the average angle of airflow exiting the impeller; and c) the volute having a cross-sectional area which maintains a substantially constant pressure field around the impeller at said pre-established airflow.
Claim 2
Dependent Claim
167 words
A centrifugal blower comprising a rotatable impeller and a volute positioned circumferentially around at least a portion of the impeller to receive airflow from the impeller and direct it to a volute exit, the blower being designed to produce a preestablished airflow from said volute exit, a) said volute being characterized by an axial dimension H which changes as a function of Θ, the angular displacement from the volute exit, and said volute being characterized by a radial dimension G which changes as a function of Θ; b) at least one of the function G(Θ) and H(Θ) being characterized by an abrupt discontinuity, and the functions G(Θ) and H(Θ) being related as follows: G(Θ)=g.sub.o (Θ.sup.h·tanα·/H(Θ) -1), where g o is a constant; h is the axial dimension of the volute at the volute origin; and α is the average angle of airflow exiting the impeller; and c) the volute having a cross-sectional area which maintains a substantially constant pressure field around the impeller at said pre-established airflow.
Claim 3
Dependent Claim
33 words
The blower of claim 1 in which said volute comprises a subvolute region axially offset from said impeller and characterized an inner radius which is less than the outer radius of said impeller.
Claim 4
Dependent Claim
21 words
The blower of claim 2 in which said subvolute region extends over at least 30° of the circumference of said blower.
Claim 5
Dependent Claim
17 words
The blower of claim 2 in which the subvolute region extends from 90° to the volute exit.
Claim 6
Dependent Claim
29 words
The blower of claim 4 in which the inner radius of the volute is less than 90% of the impeller outer radius over an arc of at least 45°.
Claim 7
Dependent Claim
27 words
The blower of claim 4 in which the axial extent of the volute is at least twice the axial extent of the impeller over said subvolute region.
Claim 8
Dependent Claim
25 words
The blower of claim 1 in which H(Θ) is selected from the group consisting of a Fermi function and a superposition of several Fermi functions.
Claim 9
Dependent Claim
33 words
The blower of claim 1 in which the discontinuity is characterized by a change in the first derivative of said function of at least 5% over an angular change of 30° or less.
Claim 10
Dependent Claim
33 words
The blower of claim 1 in which said volute comprises a subvolute axially offset from said impeller and characterized by an inner radius which is less than the outer radius of said impeller.
Claim 11
Dependent Claim
21 words
The blower of claim 9 in which said subvolute region extends over at least 30° of the circumference of said blower.
Claim 12
Dependent Claim
17 words
The blower of claim 9 in which said subvolute region extends from 90° to the subvolute exit.
Claim 13
Dependent Claim
29 words
The blower of claim 11 in which the inner radius of the volute is less than 90% of the impeller outer radius over an arc of at least 45°.
Claim 14
Dependent Claim
27 words
The blower of claim 11 in which the axial extent of the volute is at least twice the axial extent of the impeller over said subvolute region.