US1030153A - Device to balance thrust in turbines. - Google Patents
Device to balance thrust in turbines. Download PDFInfo
- Publication number
- US1030153A US1030153A US63776611A US1911637766A US1030153A US 1030153 A US1030153 A US 1030153A US 63776611 A US63776611 A US 63776611A US 1911637766 A US1911637766 A US 1911637766A US 1030153 A US1030153 A US 1030153A
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- Prior art keywords
- drum
- steam
- axial
- thrust
- turbine
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
- F01D3/04—Machines or engines with axial-thrust balancing effected by working-fluid axial thrust being compensated by thrust-balancing dummy piston or the like
Definitions
- FIG. 1 is a sectional view of a construction of a known device.
- Fig. 2 is a sectional view of the device according to the invention.
- Fig. 3 is a diagram of a development of the cross section of Fig. 2.
- FIG. 1 of the drawing which is a particular construction of a known form of device
- a B designates that part of the turbine drum which is provided with moving blades.
- steam when passing through different stages of blades, relaxes progressively from the boilers pressure to that of the condenser, thus causing an axial thrust in the direction of the arrow CD.
- a set of pack ing rings is provided in E and a certain pressure caused to act on the rear G of the drum.
- This pressure is regulated by throttling more or less the annular space m through which steam is admitted to act on the rear side G of the drum.
- one or more packing rings R conveniently disposed and which, for example, as in the drawing, are fixed on to the shaft of the drum in order to participate in its movement due to the axial thrust.
- the steam which is to act against the rear of the drum is admitted into the space N behind the packing rings R (of which one only is shown in the drawing) whence it passes through the annular space m whose section varies according to the relative position of R and of the part a of the casing.
- the steam under pressure is led into the space N by means of any external pipe L.
- the diagram Fig. 3 is the development of the cross section; in said diagram X is the section of passage of the steam and s the total displacement of the collar-ring R in relation to the fixed part S.
- the line T U instead of being oblique, could be broken or curved in any manner.
- the steam to balance the axial thrust is led through I to G and its throttling in a, between I and G, slackens slightly the balancing eifect on G and eliminates totally the axial oscillations of the rotor.
- thrust bearings can be dispensed with.
- the axial position of the rotor with respect to the turbine casing can be regulated by means of the part S secured by means of the nut M.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Witnesses A. BARBEZAT.
DEVICE T0 BALANCE THRUST IN TURBINES.
APPLIOATION FILED JULY 10, 1911.
Patented June 18, 1912.
ALFRED BARBEZAI', 0F LESQUIN, NEAR LILLE, FRANCE.
DEVICE T0 BALANCE THRUST IN TURBINES.
Specification of Letters Patent.
Patented June 18, 1912.
Application filed July 10, 1911. Serial No. 637,766.
To all whomit may concern! Be it known that I, ALFRED BARBEZAT,
the combined action of steam, admitted be hind the rear bottom of the turbine drum, with one or more packing rings which participate in the axial displacement of the drum and increase or diminish the section through which said steam is admitted behind the bottom of the drum; therefore increasing or diminishing the pressure .on said bottom proportionally to the increase or decrease of axial thrust.
The invention is illustrated by way of example in the accompanying drawings in which- Figure 1 is a sectional view of a construction of a known device. Fig. 2 is a sectional view of the device according to the invention. Fig. 3 is a diagram of a development of the cross section of Fig. 2.
In Fig. 1 of the drawing, which is a particular construction of a known form of device, A B designates that part of the turbine drum which is provided with moving blades. As known, steam, when passing through different stages of blades, relaxes progressively from the boilers pressure to that of the condenser, thus causing an axial thrust in the direction of the arrow CD.
To balance this axial thrust a set of pack ing rings is provided in E and a certain pressure caused to act on the rear G of the drum. This pressure is regulated by throttling more or less the annular space m through which steam is admitted to act on the rear side G of the drum. To this purpose there are provided one or more packing rings R, conveniently disposed and which, for example, as in the drawing, are fixed on to the shaft of the drum in order to participate in its movement due to the axial thrust. The steam which is to act against the rear of the drum is admitted into the space N behind the packing rings R (of which one only is shown in the drawing) whence it passes through the annular space m whose section varies according to the relative position of R and of the part a of the casing. The steam under pressure is led into the space N by means of any external pipe L.
The above described device works as follows: If, owing to the axial-thrust of the drum, said drum is shifted in the direction CD shown by the arrow in the drawing, the packing-rings R fixed on to the turbine shaft are shifted in the same direction, thus causing an immediate increase of the section of the annular passage m and therefore also an increase ofthe pressure on the rear G of the turbine drum; this pressure is opposite in direction to that shown by the arrow CD and increases until it equals the latter. Should the drum, for any reason, be shifted in the opposite direction to that indicated by the arrow C D, the section of the annular space m will decrease according to the displacement of the drum and therefore practically no more steam will be admitted behind the rear bottom of the drum, thus allowing the low-pressure steam in B to pass through the packing rings E and enter the space behind G; the counter-pres sure thus diminishes and the axial thrust whose normal direction is that of the arrow CD shifts the drum back toward the right. Such a construction would in practice show a great disadvantage, in fact, the. slightest axial displacement of the rotating part of the turbine causing great variation of the balancing pressure of the rear of the drum G, the rotor would oscillate axially and therefore the moving part R would press against the fixed part S of the casing and owing to this friction these parts should soon wear out and an accurate balancing of the axial thrust become impossible.
The construction according to the invention which is shown in Fig. 2 obviates entirely the above stated disadvantage. A collar-ring R with a screw like or inclined face is keyed on the motor shaft and turns in front of a fixed circular part S, whose position can be regulated at will by the pro vision on the said fixed part S of a screw thread. WVhen, owing to the axial thrust of the drum, the ring It is shifted in the one or the other direction, the steam is throttled as necessary by the collar-ring R closing up more or less the inclined opening m without both parts R and S touching each other in any case. The Working of this device, together with a constant throttling device shown at a, eliminates totally the axial oscillations of the rotor.
The diagram Fig. 3 is the development of the cross section; in said diagram X is the section of passage of the steam and s the total displacement of the collar-ring R in relation to the fixed part S. The line T U instead of being oblique, could be broken or curved in any manner.
The steam to balance the axial thrust is led through I to G and its throttling in a, between I and G, slackens slightly the balancing eifect on G and eliminates totally the axial oscillations of the rotor. Owing to the above described device, thrust bearings can be dispensed with. The axial position of the rotor with respect to the turbine casing can be regulated by means of the part S secured by means of the nut M.
Having thus described and ascertained the nature of my invention and in what manner it has to be performed, What I claim is:
In a steam turbine, an automatic device to balance the axial thrust comp-rising, in combination, an automatically working throttling device located behind the rear of the turbine-drum and consisting of a rotating collar-ring with a screw-like or inclined face keyed on the turbine shaft and of a fixed circular part of smaller external diameter than the inner diameter of the collarring, means for regulating the axial distance between said fixed part and the rotating collar-ring, means for admitting steam under pressure in the annular space between the fixed part and the rotating collar-ring of said automatic throttling device and a constant steam throttling device located be-- tween the rear of the turbine-drum, and the automatic throttling device all for the purpose specified and substantially as set forth.
ALFRED BARBEZAT.
Witnesses EDOUARD LUGNEL, CHRISTOPHER J. KING.
Copies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents,
Washington, D. C.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US63776611A US1030153A (en) | 1911-07-10 | 1911-07-10 | Device to balance thrust in turbines. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US63776611A US1030153A (en) | 1911-07-10 | 1911-07-10 | Device to balance thrust in turbines. |
Publications (1)
Publication Number | Publication Date |
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US1030153A true US1030153A (en) | 1912-06-18 |
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Application Number | Title | Priority Date | Filing Date |
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US63776611A Expired - Lifetime US1030153A (en) | 1911-07-10 | 1911-07-10 | Device to balance thrust in turbines. |
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Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2605147A (en) * | 1949-09-17 | 1952-07-29 | Raichle Ludwig | Thrust balancing for vertical shafts |
US2866620A (en) * | 1957-10-03 | 1958-12-30 | Worthington Corp | Means for counterbalancing starting thrust in turbine driven pump units |
US2869820A (en) * | 1951-04-18 | 1959-01-20 | Bristol Aero Engines Ltd | Rotors for axial flow compressors or turbines |
US2952494A (en) * | 1956-10-12 | 1960-09-13 | Tiraspolsky Wladimir | Revoluble engines and motors for subterranean drilling |
US2963268A (en) * | 1957-03-25 | 1960-12-06 | Gen Electric | Pressurized seal |
US3129767A (en) * | 1962-01-12 | 1964-04-21 | Walter G Finch | Torque converting propeller |
-
1911
- 1911-07-10 US US63776611A patent/US1030153A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2605147A (en) * | 1949-09-17 | 1952-07-29 | Raichle Ludwig | Thrust balancing for vertical shafts |
US2869820A (en) * | 1951-04-18 | 1959-01-20 | Bristol Aero Engines Ltd | Rotors for axial flow compressors or turbines |
US2952494A (en) * | 1956-10-12 | 1960-09-13 | Tiraspolsky Wladimir | Revoluble engines and motors for subterranean drilling |
US2963268A (en) * | 1957-03-25 | 1960-12-06 | Gen Electric | Pressurized seal |
US2866620A (en) * | 1957-10-03 | 1958-12-30 | Worthington Corp | Means for counterbalancing starting thrust in turbine driven pump units |
US3129767A (en) * | 1962-01-12 | 1964-04-21 | Walter G Finch | Torque converting propeller |
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