U.S. patent number 3,709,630 [Application Number 05/062,020] was granted by the patent office on 1973-01-09 for pneumatic motor for medical instruments.
This patent grant is currently assigned to Howmet International, Inc. Zweigniederlassung Kiel. Invention is credited to Arnold Keller, Fritz G. Pohl.
United States Patent |
3,709,630 |
Pohl , et al. |
January 9, 1973 |
**Please see images for:
( Certificate of Correction ) ** |
PNEUMATIC MOTOR FOR MEDICAL INSTRUMENTS
Abstract
The invention relates to a small pneumatic motor for a rotating
medical instrument, especially for drilling or milling instruments.
A shaft with a turbine is supported in a housing with the gas inlet
end of the turbine arranged towards the output end of the motor.
The driving gas flows to the turbine inlet side via channels
arranged longitudinally in the housing along the periphery of the
turbine and then back to the input end of the housing. Discharge of
driving gas at the output end of the housing toward the patient is
avoided in this way.
Inventors: |
Pohl; Fritz G.
(Kiel-Dietrichsdorf, DT), Keller; Arnold
(Kiel-Dietrichsdorf, DT) |
Assignee: |
Howmet International, Inc.
Zweigniederlassung Kiel (Kiel-Dietrichsdorf,
DT)
|
Family
ID: |
5749416 |
Appl.
No.: |
05/062,020 |
Filed: |
August 7, 1970 |
Foreign Application Priority Data
|
|
|
|
|
Oct 28, 1969 [DT] |
|
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P 19 54 130.1 |
|
Current U.S.
Class: |
415/199.5;
173/218; 415/904; 433/106; 433/132; 606/180; 477/208 |
Current CPC
Class: |
A61C
1/05 (20130101); A61B 17/1628 (20130101); F01D
15/06 (20130101); Y10S 415/904 (20130101); Y10T
477/88 (20150115); A61B 17/1626 (20130101) |
Current International
Class: |
A61B
17/16 (20060101); A61C 1/05 (20060101); A61C
1/00 (20060101); F01D 15/06 (20060101); F01D
15/00 (20060101); A61c 001/05 (); F01d 001/10 ();
A61b 017/32 () |
Field of
Search: |
;415/503,182,199
;192/3R,3TR ;173/163 ;32/26,27 ;128/305 ;417/408 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Herrmann; Allan D.
Claims
What we claim is:
1. A pneumatic turbine powered surgical motor apparatus for
rotating a medical instrument comprising, in combination, an
elongated housing having a longitudinal axis, an input end and an
output end, a shaft rotatably mounted in said housing concentric
with said axis and projecting from said output end adapted to drive
a cutting instrument, a pressurized gas connection and an exhaust
gas connection defined on said housing at said input end, an axial
flow turbine having a rotor rotatably mounted in said housing
concentric thereto and drivingly connected to said shaft, said
turbine having an inlet disposed toward said housing output end and
an exit disposed toward said housing input end, first passage means
longitudinally defined in said housing concentrically extending
about the periphery of said turbine and communicating with said
pressurized gas connection and said turbine inlet, and second
passage means defined in said housing communicating with said
exhaust gas connection and said turbine exit whereby pressurized
gas entering said pressurized gas connection and first passage
flows toward said housing output end to said turbine inlet, enters
said turbine inlet and reverses its direction of flow to flow
through said turbine toward said housing input end and from said
turbine exit to said exhaust gas connection.
2. In a pneumatic turbine powered surgical motor apparatus as in
claim 1, a nozzle member within said housing located adjacent said
turbine inlet, nozzles defined in said nozzle member for directing
pressurized gas into said turbine, said nozzle member including an
annular bushing circumscribing said shaft and extending toward said
turbine exit and being radially spaced from said shaft and turbine
rotor by small running clearances.
3. In a pneumatic turbine powered surgical motor apparatus as in
claim 1 wherein said first passage means comprises an annular
chamber concentrically disposed about said turbine and said second
passage means comprises a plurality of passages axially defined in
said housing extending between said turbine exit and said exhaust
gas connection.
Description
BACKGROUND OF THE INVENTION
The invention relates to a hand-actuated pneumatic motor for a
drilling and/or milling instrument for medical application. It
relates especially to a small turbine used for driving a precision
drilling or precision milling instrument. The speed of such
precision drill or precision milling instrument is very high. It is
possible, for instance, with such motor driven precision drilling
instruments or precision milling instruments to impart to the
instrument shaft a speed of about 100,000 rpm without a speed
transmission gear being arranged between the turbine and the shaft.
With known turbine-driven precision drilling or milling instruments
the air discharged from the turbine leaves the cylindrical housing
on the side of the rotating instrument which, in the case of
operations with open wounds increases the danger of infection.
Another danger existing additionally is that of an air emboly. The
use of nitrogen instead of air as a driving fluid does not
completely eliminate this danger and suffers from additional
shortcomings.
Also, precision drilling instruments and precision milling
instruments have become known which are not driven by means of a
compressed air driven turbine but by means of a compressed air
driven piston sickle motor, the pistons of which consist of
individual discs rotating eccentrically with respect to the axis of
rotation. With such piston motor driven precision drilling
instruments or precision milling instruments it is possible to
supply and to discharge the air at the drive end of the housing,
i.e. to the end facing away from the tool. Such compressed-air
motors, however, in case of high speeds tend to produce disturbing
noises. In addition, with such motors the fineness of the work is
not guaranteed under all conditions. Finally, such compressed air
motors develop a higher torque than compressed-air turbines which
might induce the doctor to demand a higher torque by exerting a
pressure on the drill or the milling instrument which might impair
the precision of the work.
SUMMARY OF THE INVENTION
It is the object of the invention to provide a turbine driven
rotating instrument for medical application in which the gas
leaving the turbine is discharged away from the area of the
instrument.
The hand operated pneumatic motor for a drilling or milling
instrument comprises a cylindrical housing, a shaft supported in
the housing and projecting from one front side thereof and a
compressed gas driven turbine adapted to drive the shaft.
In accordance with the invention the compressed gas is supplied and
discharged at the end (input end) of the housing facing away from
the shaft projecting end (output end) with the fluid gas inlet end
of the turbine facing toward the output end of the housing and the
fluid gas exit end of the turbine facing toward the input end of
the housing, and the compressed gas is supplied to the inlet end of
the turbine through channels arranged along the outer periphery of
the turbine.
Thus, the flow direction of the compressed air is reversed within
the housing. The compressed air flows from the input end of the
housing toward the output end thereof until it approximately
arrives at the inlet nozzles of the turbine. Within the turbine the
air flows in the opposite direction to the exit end of the turbine
which is arranged towards the input end of the housing.
Small amounts of air might still escape at the inlet end of the
turbine towards the tool because the air at the exit from the
nozzles, i.e. directly before entering the blades of the turbine
rotor, is subjected to an impact pressure, i.e. a certain
overpressure which might drive small amounts of air through the
output end towards the instrument. Here it must be taken into
consideration that a certain running clearance must necessarily be
provided between the exit end of the nozzles and the inlet end of
the blades of the turbine rotor.
To avoid also the exit of these small amounts of air, the nozzle
member with the nozzles is provided with a bushing extending
towards the turbine exit end, said bushing having a small running
clearances with both the instrument shaft and the turbine rotor.
These small running clearances constitute additional flow
resistance which prevent these small amounts of air from escaping
at the output end of the housing towards the instrument. The
suction effect of the gaseous jet leaving the nozzles is so great
that even a vacuum is formed which draws in a certain amount of air
from the output end of the housing and drives it through the
turbine to the turbine exit end.
The invention in addition offers the advantage that it is possible
without any difficulties to dimension the channels for the gas
leaving the turbine so amply that practically the entire gas
pressure available may be transformed into a high velocity and thus
into turbine energy.
In a preferred embodiment of the invention, the turbine is
constructed to have two stages with a stator arranged between the
two stages.
Suitably, the two stages of the turbine are arranged on a turbine
rotor common to both stages, said stator being constructed in two
stages in the form of two annular halves. After having pushed the
two annular halves of the stator into a corresponding annular
groove of the turbine rotor, the stator is fixed on its outer
periphery inside the housing by means of correspondingly designed
bushings. This is a very simple manner of fixing the stator,
however, other constructions are not excluded.
It is recommendable to supply the pressure gas at the input end of
the housing through a centrically arranged line and to lead off the
exhaust gas at the input end via a likewise approximately
centrically disposed conduit of larger diameter which surrounds the
pressure gas line.
Suitably, a manually operated control valve or a manually actuated
control slide is arranged in the housing near the input end
thereof.
An element to actuate the control valve or control slide is adapted
to act on a brake member, which with a closed control valve or the
control slide brakes the instrument shaft.
Suitably, the brake member is held in its brake release position by
means of a spring and is movable into its braking position in
dependence on the closing of the control valve or the control
slide. A positive actuation and braking of the tool is obtained in
this manner independently of the respective extent of wear on the
brake surface.
The brake member is suitably constructed as a centrally arranged
bolt with a pivotal lever arranged between the bolt and a
spring-biased slide by means of which the control valve or control
slide, respectively, is movable.
With a brake air pressure of 5-6 kp/cm.sup.2 and a direct drive of
the tool shaft by means of the turbine rotor the invention secures
a speed of about 100,000 rpm. The construction according to the
invention is distinguished by its low noise at that speed and in
that it allows the finest precision work with safety. Air
consumption in this operation is 200 to 300 l/min.
BRIEF DESCRIPTION OF THE DRAWING
Further improvements and features of the invention are described by
way of the enclosed drawing which shows one embodiment of the
invention on an enlarged scale. In practice, the diameter of the
cylindrical housing only is about 20 mm.
In the drawings,
FIG. 1 shows a longitudinal sectional view of a pneumatic motor
constructed in accordance with the invention, and
FIG. 2 a partial sectional view taken on line II--II of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT
The cylindrical housing 1 comprises an output member 2 and an input
member 3, with a sleeve 4 being fastened on the output member 2 by
shrinking or pressing, for example. The input member 3 is provided
with an external thread 5 which may be threaded into a
corresponding internal thread 6 of the sleeve 4.
The instrument shaft 7 is supported in the ball bearings 8, 9 and
10.
The turbine rotor consists of the rotor member 11 with the two
blade rings 12 and 13. A stator 14 is stationarily arranged between
the blade rings. On the left-hand side of the blade ring 12 as
shown in FIG. 1, a nozzle member 15 is stationarily arranged in
which blowing nozzles 16 are provided. Compressed air flows to the
blowing nozzles 16 via an annular chamber 17 and channels 18
provided in the output member 2. An intermediate member 20 is
provided between the sleeve-shaped end 19 of the output member 2
and the left-hand end of the input member 3. The intermediate
member 20 is provided with a projecting sleeve 21. The outer
periphery of the stator 14 is fixedly clamped between sleeve 21 and
a shoulder 22 formed on the output member 2. The clamping action is
effected by pressing the input member 3 against the intermediate
member 20 with the aid of screw connection 5, 6.
Compressed air enters the input member 3 via the centric bore 23.
It is supplied through a hose (not shown) which is screwed to the
bore 24 of the input member 3. The compressed air flows through the
radial bore 27 via a control slide 25 which will be described
herebelow in more detail, through an axial bore 26 and an oblique
bore 28 of the input member 3 to an annular chamber 29, which is
provided between the sleeve 4 on the one side and the left-hand end
of the input member 3 and the right-hand end of the intermediate
member 20 on the other side. The sleeve shaped end 19 of the output
member 2 is provided with radial projections 30 by means of which
this end is centrally guided within the sleeve 4. Wide channels
remain open between these projections 30 for the passage of the
compressed-air from the annular chamber 29 to an annular chamber 31
which is provided between the remaining part of the sleeve 19 and
the output member 2 on the one side and the sleeve 4 on the other
side.
The compressed air flows from this annular chamber 31 into the
annular chamber 17 via channels 18. Then it passes via the blowing
nozzles 16 into the first blade ring 12. It is deviated in the
stator 14 after having left the first blade ring 12. Then the air
flows through the second blade ring 13 of the turbine rotor. From
here it flows through the chamber 32 to a plurality of exit bores
33 which are provided in the intermediate member 20 (see FIG. 2).
The exit bores 33 open into bores 34 of the input member 3 which
terminate in a chamber 35. This chamber 35 is connected with a hose
or pipe 36 arranged centrally with respect to the bore 24 and
through which the exhaust air is discharged into the atmosphere,
for example.
In the shown embodiment, there are altogether six of the bores 33
and 34 arranged in such a way to leave sufficient space between
them for the bores 26, 28 through which compressed air is supplied.
A running clearance 37 is provided between the right-hand end of
the nozzle member 15 and the left-hand end of the turbine rotor 11.
The nozzle member 15 is provided with a bushing 38 extending a
considerable length towards the input member 3. The bushing 38 is
formed integrally with the nozzle member 15. The running clearance
37 passes over into a small running clearance 39 provided between
the bushing 38 and a bore 40 of the turbine rotor 11. On the other
side there is a small running clearance 41 between the bushing 38
and the instrument shaft 7. The gap 37 thus communicates with the
bearing 9 and thus with the free atmosphere at the instrument end
only through the long narrow gaps 39 and 41. It has been found that
this construction suffices to prevent the exit of very small
quantities of air towards the instrument end.
The shaft 7 is provided with a bore 42 to receive the instrument.
The instrument is clamped in the bore 42 by three centrally
arranged wedges 43, for example. These wedges are retained by a
resilient sleeve 44 consisting of rubber, for example, which is
rigidly connected with a metallic outer sleeve 45 by vulcanization.
When the instrument spindle is being plugged into the bore 42 the
wedges 43 are slightly pressed outwardly stressing the elasticity
of the sleeve 44, thereby clamping the instrument spindle.
A circular plate-shaped control slide 25 is supported in a
corresponding recess 46 of the input member 3, said control slide
being provided with a sickle-shaped control opening 47. In the
position shown in FIG. 1 the control opening 47 connects the bore
23 through which compressed air is supplied, with the radial bore
27. The control slide is sealed by sealings 48 and is supported in
its position by a disc 49. A pin 50 fixedly connected with the
slide 25 serves to actuate said slide, said pin 50 being pivotally
supported in an actuating slide 51. The actuating slide 51 is
forced by means of a spring 52 into a position in which the control
slide 25 is closed. Towards the outside, the actuating slide 51 is
closed by means of a sleeve 53 which surrounds the input member 3.
A slot 54 is provided in the sleeve 53 with a projection 55 of the
actuating slide 51 engaging therethrough. The slot 54 constitutes
an elongated hole which serves to guide the projection 55 of the
actuating slide. On the projection 55, there is mounted by means of
a screw 56 an actuating rod 57 with a grip projection 58 by means
of which the control slide 25 may be operated. The actuating rod 57
is in addition guided by means of an elongated slot 59 provided
therein and being in engagement with a pin 60, said pin being
fastened on the input member 3.
A nut 61 lies close to the inner race of the ball bearing 10 which
race rotates with the shaft 7, said nut being screwed onto a
threaded end 62 of the shaft 7. A brake member 63 formed as a
concentric bolt is adapted to lie close to said threaded end and is
provided with a head 64. The brake member is axially movably guided
in a bushing 65 and has its head 64 pressed against a swivel beam
67 by means of a spring 66 which swivel beam 67 is pivotally
supported in a bore 68 of the input member 3. The swivel beam 67
outer end is located in a recess in the actuating slide 51 and
passes through a slot 71 of a cover plate 69 which separates the
control slide 25 from the actuating slide 51. The slot 71 serves to
guide both the swivel beam 67 and the pin 50 of the control slide
25.
In the left-hand end position (not shown) the actuating slide 51
forces the outer end of the swivel beam 67 to the left. In this way
the brake member 63 is also forced to the left on the front side of
the threaded end 62 of the shaft 7 against the tension of the
spring 66. Accordingly, with the control slide 25 closed, the shaft
7 is braked by means of the brake member 63. The bore 26 is closed
by means of a plug 72 near its left hand end (FIG. 1). Plug 72
separates the bore 26 supplying the compressed air from an annular
chamber 70 on the left-hand side of the input member 3 into which
the exhaust air bores 33 of the intermediate member 20 open.
* * * * *