U.S. patent number 3,680,977 [Application Number 05/050,052] was granted by the patent office on 1972-08-01 for framed impeller.
Invention is credited to Charles Louis Marsot, Denis Rabouyt.
United States Patent |
3,680,977 |
Rabouyt , et al. |
August 1, 1972 |
FRAMED IMPELLER
Abstract
An impeller with a rotor carrying a set of fan blades has a
circular duct of streamlined profile surrounding the rotor blades,
the latter having their tips interconnected by a ring received with
small clearance in an annular groove on the inner duct periphery so
that this periphery is flush with the inner ring surface. Elastic
inserts in the gap between the ring and the duct may be used to
minimize or eliminate the intervening clearance.
Inventors: |
Rabouyt; Denis (Paris,
FR), Marsot; Charles Louis (Paris, FR) |
Family
ID: |
9036714 |
Appl.
No.: |
05/050,052 |
Filed: |
June 29, 1970 |
Foreign Application Priority Data
Current U.S.
Class: |
415/173.6;
415/174.2; 416/190; 277/402; 277/419; 277/562; 277/414; 415/174.5;
415/210.1; 416/192; 277/369 |
Current CPC
Class: |
B64C
11/001 (20130101); F01D 11/08 (20130101); Y02T
50/60 (20130101); Y02T 50/671 (20130101) |
Current International
Class: |
B64C
11/00 (20060101); F01D 11/08 (20060101); F01d
009/00 (); F16j 015/38 () |
Field of
Search: |
;415/170,171,172,173,174,210 ;277/65,95 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Raduazo; Henry F.
Claims
We claim:
1. An impeller for the circulation of an ambient fluid, comprising
a rotor with a set of blades radiating from an axis; a circular
duct of airfoil cross-section fixedly centered on said axis, said
duct having an inner periphery provided with an annular groove and
lined with a sheet-metal sheath projecting beyond the edges of said
groove to form a pair of annular shoulders within said groove; a
ring centered on said axis and interconnecting said blades, said
ring projecting radially into said groove with small axial
clearance from said shoulders; and sealing means in said groove
bridgeing said axial clearance, said sealing means including a pair
of elastic annular strips mounted in said groove on said shoulders
and extending therefrom into contact with said ring.
2. An impeller as defined in claim 1 wherein said ring has a
substantially flat inner peripheral surface flush with the inner
periphery of said sheath.
3. An impeller as defined in claim 1 wherein said ring is provided
with two outwardly directed radial flanges confronting said
shoulders, said strips bearing upon said flanges at locations
spaced radially outwardly from said sheath.
Description
Our present invention relates to an impeller, such as a blower or
fan, for circulating air or some other ambient fluid.
The intensity of a flow generated by such an impeller can be
enhanced by channeling this flow through a short duct or shroud of
air-foil cross-section presenting a streamlined profile to the
fluid stream, this duct framing the rotor of the impeller whose
blades terminate at a short distance from the inner duct periphery.
The duct has the dual purpose of concentrating the flow by
converging in the direction of fluid passage and of minimizing
turbulence in a zone surrounding the rotor blades with resulting
increase in operating efficiency. The latter function, of course,
calls for a minimum spacing between the blade tips and the
stationary duct, yet a certain tolerance must always be maintained
to allow for unavoidable eccentricities of the rotor mounting with
reference to the duct axis.
Attempts to minimize this tolerance by interconnecting the free
ends of the blades with the aid of a concentric ring inside the
duct have not solved the problem. Though such a ring reinforces the
rotor structure, it does not eliminate existing eccentricities and
requires, therefore, a certain radial spacing from the duct in
order to prevent contact between the two relatively rotating
bodies. Moreover, the presence of such a ring diminishes the
effectiveness of the rotor, by reducing the cross-sectional area of
the channel swept by the blades, and creates added discontinuities
giving rise to further turbulence.
Thus, our invention aims at providing an improved impeller of the
framed-rotor type wherein peripheral turbulence is effectively
suppressed with avoidance of the aforestated drawbacks.
A more particular object is to provide a combination of a
flow-guiding duct with a ring-reinforced rotor enabling the
utilization of the entire cross-sectional area of the flow channel
defined by the duct for the generation of forced circulation or
thrust.
These objects are realized, in accordance with our present
invention, by providing the inner duct periphery with an annular
groove receiving, with small clearance, a ring interconnecting the
free ends of the blades, the ring preferably having a substantially
flat inner peripheral surface flush with the inner duct periphery
so as to form part of a channel wall free from major
discontinuities.
In the simplest case, the ring may be a relatively thin ferrule of
cylindrical shape somewhat smaller than the relative shallow
groove. In a more sophisticated arrangement, designed to throttle
the fluid flow through the meandering gap between the ring and the
groove wall, this gap may be further reduced or eliminated with the
aid of preferably elastic sealing means in actual or potential
contact with the rigid ring. The latter may be formed with one or
more outwardly directed radial flanges which, in co-operation with
an insert or filler interleaved therewith, lengthen the flow path
around the rotor periphery and which could also be used to shield a
set of swivel heads in the ring facilitating an adjustment of the
blade pitch.
The problem of fitting the blade ring in the groove of the duct may
be solved in various ways, as by making the duct in several axially
or peripherally adjoining sections or by molding the duct directly
about the rotor. If the ring is a sufficiently deformable ferrule,
it could also be snapped into the groove of an integrally
constructed duct.
The above and other features of our invention will be described in
detail with reference to the accompanying drawing in which:
FIG. 1 is an axial view, partly in section, of an impeller
embodying our invention;
FIG. 2 is a face view of the impeller shown in FIG. 1;
FIG. 3 is a fragmentary sectional view taken on the line III -- III
of FIG. 2 but drawn to a larger scale;
FIGS. 4 and 5 show, on a still larger scale, modifications of the
assembly illustrated in FIG. 3;
FIGS. 6 and 7 are enlarged views generally similar to FIG. 3,
showing further modifications; and
FIGS. 8 and 9 are views similar to part of FIG. 5, illustrating yet
other variants.
In FIGS. 1-3 we have shown an impeller which may be used as an air
screw on an aircraft not further illustrated and which comprises a
motor 1 driving a streamlined hub 2 of a rotor having several (here
four) propeller blades 3 radiating from that hub. The free ends of
these blades are interconnected by a ring 4 in the form of a thin
ferrule received within an annular groove 8 on the inner peripheral
surface 7 of a duct or shroud 5 of streamlined cross-section. Duct
5 is supported by struts 6 on the stationary engine housing of
motor 1.
As best seen in FIG. 3, the inner peripheral surface 4a of ring 4
is flush with the inwardly convex surface 7 of duct 5 so as to
define therewith a substantially continuous channel wall. The
circular edges 10 of ring 4 are closely spaced from similar edges 9
of a sheet-metal sheath 5a which envelops the body of duct 5 and
extends slightly past the sides of groove 8.
The thrust of the propeller shown in FIGS. 1-3 is somewhat
diminished by an equalizing flow passing through the narrow gap
between edges 9 and 10 from the high-pressure region behind the
rotor blades 3 to the low-pressure region ahead of these blades.
This bypass path can be blocked, as shown in FIG. 4, by the
provision of a seal generally designated 11. Seal 11 comprises a
pair of strips 12, 13, of rubber or other elastomeric material,
mounted on a pair of shoulders 5', 5" which are formed by the
projecting edges of sheath 5a inside groove 8 so as to bear upon
the outer peripheral surface of ring 4. FIG. 4 also shows a screw
24 serving to fasten this ring to a corresponding blade 3.
In FIG. 5 we have illustrated a modified ring 4' of U-profile
formed with two radial flanges 14, 15 received in the groove 8.
Sealing strips 16 and 17, similar to those of the preceding
embodiment, bear upon the outer surfaces of these flanges at
locations spaced radially outwardly from the supporting shoulders
5' ,5".
According to FIG. 6, the flanged ring 4' co-operates with a
tripartite insert, also preferably of elastic material, consisting
of three labyrinth sections 18, 18' and 18" axially separated by
narrow gaps which receive the ring flanges 14 and 15.
As shown in FIG. 7, an elastic filler 19 of polyurethane foam or
other cellular material forms similar annular recesses 19a, 19b to
accommodate the flanges 14 and 15.
FIGS. 8 and 9 illustrate the possibility of using a flanged ring 4'
as a journal bearing for the rotor blades 3 whose pitch can be
controlled from within the hub 2 (FIG. 1), by conventional means
not shown, and which terminate in studs 20 (FIG. 8) or 20' (FIG. 9)
received in respective sockets 22, 23. These sockets may be formed
by individual bosses, as in FIG. 8, or by a continuous hollow
ridge, as in FIG. 9, with interposition of bearing sleeves 25, 25'
around the studs. FIG. 9 shows the bearing sleeve 25' as a
spherically convex bushing 21 on stud 20'. Antifriction layers
(e.g. of Teflon), not shown, may be inserted between these bearing
sleeves and the coacting stud surfaces.
* * * * *