An embodiment of the present invention relates to the field of mechanical devices, and more particularly to lifting devices of heavy equipment such as a steam turbine, a gas turbine, a generator, a motor, and a compressor.
During installation or maintenance, heavy equipment such as a steam turbine, a gas turbine, a generator, a motor, and a compressor often needs to be lifted (including the operations of moving from a lower to a higher position and vice versa). Some automatic lifting devices exist, but these lifting devices usually cannot be used to lift equipment that is heavy. For example, during assembly of a gas turbine, if a rotor and an exhaust casing can be lifted together, assembly costs can be reduced greatly, and assembly efficiency can be improved.
However, currently during lifting, when lifting points (that is, lifting positions) are disposed on struts of a star-shaped exhaust casing, some struts of the exhaust casing are likely to deform or be damaged due to heavy loads applied to them. Therefore, currently, the lifting point can only be set on the rotor. A device capable of lifting the exhaust casing and the rotor together without damaging struts of the exhaust casing is not available yet. Similarly, during lifting of other star-shaped heavy equipment, this phenomenon also occurs in which some struts deform or is damaged during lifting operation because loads are concentrated on the struts.
An embodiment of the present invention provides a device for lifting equipment having a plurality of outwardly extending struts each of which comprises a head portion and a root portion connected to the head portion, the device being characterized in comprising a plurality of separate connection parts, the connection parts being capable of being connected at a first position and a second position to the head portion of the struts, and the first position and the second position being located two sides of the central axis of the strut respectively, so that the first position and the second position are respectively capable of bearing the gravity load of the equipment and balancing the stress load which the strut incurs when the equipment is lifted by the device. It should be noted that “a first position and a second position” does not mean there is only one first position and one second position.
In an embodiment of the present invention, a plurality of separate connection parts are used to fix a plurality of outwardly extending struts of star-shaped equipment respectively, so that the gravity load can be distributed to multiple struts of the star-shaped equipment. In this manner, the situation where the gravity load is concentrated on a strut is avoided. Meanwhile, the manner of the connection on two sides of the central axis of the root portion of one strut can balance the local load, which is mainly stress incurred at the junction of the root portion and the head portion of the strut, incurred during lifting operation. It should be noted that the position that balances the local load incurred in lifting operation is likely to also bear a certain part of the gravity load. However, in the embodiment of the present invention, the main function of the position is to balance the local load incurred.
In an embodiment, the connection parts further have third positions at one end thereof, and the third positions of two adjacent connection parts are located on two sides of a central axis of the root portion of one strut, so that the head portion of one strut is capable of connecting two adjacent connection parts at the third positions.
In the above embodiment, the third positions of two adjacent connection parts are connected to one strut, so as to connect the adjacent connection parts. In this way, during lifting of equipment that is heavy, a connection part may be connected to two struts, so that the gravity load of the equipment can be distributed to more struts instead of one. Therefore, more struts can bear the gravity load, thereby protecting the struts from being damaged.
In an embodiment, each of the connection parts has two pairs of a first position and a second position, so that each of the connection parts is capable of connecting to two struts.
The embodiment enables a connection part to connect two struts. In this manner more struts will bear the gravity load of the equipment.
In an embodiment, the head portion of the strut has connection mechanisms at the first position and the second position respectively, and the connection part has a first group of connection mechanisms and a second group of connection mechanisms whose positions correspond to those of the connection mechanisms of the head portion of the strut respectively, so that the connection part is capable of being connected to the strut at the first position and the second position respectively.
In an embodiment, the first group of connection mechanisms and the second group of connection mechanisms of the connection part and the connection mechanisms of the head portion of the strut are all holes.
In an embodiment, one of the first group of connection mechanisms and the second group of connection mechanisms of the connection part forms a tight connection with the connection mechanisms of the head portion of the strut, so that one position among the first position and the second position is capable of bearing the gravity load of the equipment.
The tight connection between one of the first group of connection mechanisms and the second group of connection mechanisms of the connection part and the connection mechanisms of the head portion of the strut makes the connection part in close contact with the strut, so as to ensure that the strut can bear the gravity load at the corresponding first position or second position. It should be noted that, the so-called “tight connection” refers to that two connection mechanisms are connected together with no substantial space for movement.
In an embodiment, the other of the first group of connection mechanisms and the second group of connection mechanisms is capable of being connected to the connection mechanisms on the head portion of the strut by using connection components. so that the other position among the first position and the second position can balance the local load incurred in lifting operation. Besides, the diameters of the connection components are smaller than the diameters of the connection mechanisms on the head portion of the strut, and are also smaller than the diameters of the first group of connection mechanisms or the second group of connection mechanisms which is connected to the connection components.
In the embodiment of the present invention, the stress incurred at the junction of the head portion and the root portion of the strut of the equipment can be reduced or eliminated, thereby protecting the strut. Manufacturing errors always occur in mechanical manufacturing. When multiple tight connection fits exist between two components, it is difficult or even impossible to perform assembly, because it is difficult to align or pair connection mechanisms which are fitted later than others, thereby making it difficult to perform assembly. To facilitate the connection of the connection part and the strut in an embodiment of the present invention, in an embodiment of the present invention, the diameter of the connection components such as a pin is smaller than the diameter of the connection mechanisms on the connection part and the strut connected to the pin, thereby facilitating connection and fixing.
In an embodiment, the connection part is provided with a third connection mechanism at the third position, and two adjacent connection parts are connected at the third positions to the head portion of a strut through the third connection mechanisms, so that the third positions may not only bear the gravity load of the equipment, but also balance the stress load incurred in lifting operation.
In an embodiment, the first position and the second position of the connection part are symmetrically located relative to the central axis of the root portion of a strut, and the third positions of the two adjacent connection parts for connecting to the head portion of a strut are symmetrical relative to the central axis of the root portion of the strut.
In an embodiment, the connection parts are arc. A lifting point of the equipment is located between the third position of the connection part and the first position or the second position which is closer to the third position. The equipment is a combination of an exhaust casing and a rotor of a gas turbine.
The following accompanying drawings are only intended to schematically illustrate and explain embodiments of the present invention, but are not intended to limit the scope of the present invention, where:
1 Strut
2 Equipment
3 Head portion
4 Root portion
5 First group of connection mechanisms
6 Second group of connection mechanisms
7 Connection part
8, 9 Connection mechanisms on a strut
10 Pin
11 Bolt
12 Pulling part
A, B, E, F First position and second position
C, D Third position
To make the technical features, objectives, and effects of the present invention be understood more clearly, embodiments of the present invention are illustrated with reference to the accompanying drawings.
In order to lift heavy equipment having the foregoing structure during installation or maintenance, an embodiment of the present invention provides a device, and the device has a plurality of separate connection parts 7. The shape of the connection part 7 may be any as long as the connection part 7 and the head portion 3 of the strut 1 can be connected together. To facilitate lifting of an exhaust casing and a rotor of a cylindrical gas turbine (the rotor causes the gravity load in lifting operation to be very big), the connection parts 7 are in the shape of arc, in order to prevent interference between the connection parts 7 and a casing body. The connection parts 7 may also be selectively in the forms such as a beam and a plate corresponding to the shape of the to-be-lifted equipment. Stiffness of the connection parts needs to be high, and a specific stiffness value may be determined according to a maximum load incurred during lifting. The number of the connection parts 7 may be selected according to the number of the struts 1. For example, referring to
The connection part 7 of the lifting device may be connected, at a first position and a second position A, B, to the head portion 3 of a strut, and the first position and the second position A, B are located on two sides of a central axis of the root portion 4 of the strut respectively. When the device is used to lift the equipment 2, the first position is capable of bearing the gravity load of the equipment 2, and the second position is capable of balancing a local load (mainly stress incurred at the junction of the head portion and the root portion of the strut) incurred during lifting. In this manner, a plurality of separate connection parts 7 are connected to multiple struts, so as to distribute the gravity load of the equipment to more than one strut, and meanwhile balance the local load incurred during lifting, thereby better protecting the struts of the to-be-lifted equipment from damaging. Since the connection part 7 and the strut 1 are in contact with each other at the second position, the second position is very likely to bear a certain part of the gravity load of the equipment.
Alternatively, the first position may have the function of balancing the local load incurred by the lifting, and the second position may have the function of bearing the gravity load of the equipment 2. In all examples in the following description, the first position has the function of bearing the gravity load of the equipment and the second position has the function of balancing the load incurred by the lifting, and the case in which the first position has the function of balancing the local load incurred during lifting and the second position has the function of bearing the gravity load of the equipment is not described.
As shown in
As shown in
Preferably, the third positions C, D of two adjacent connection parts 7 for connecting to the head portion 3 of a strut are symmetrical relative to the central axis of the root portion 4 of the strut. In this way, local stress incurred at third positions by adjacent connection parts 7 connected to a strut 1 can be better balanced.
In the embodiment where the connection part 7 has the third position, a lifting point may be selected to be located between the third position C, D of the connection part 7 and the first position or the second position A, B which is closer to the third position. For example, as shown in
An embodiment in which the connection parts 7 and the strut 1 are connected at the first position and the second position A, B and the third positions C, D is illustrated below with reference to
To facilitate assembly, the diameters of the pins 10, which are the connection components used at the second positions B, E, are smaller than the diameters of the connection mechanisms 8, 9 (for example, holes) on the head portions 3 of the struts, and are also smaller than the diameters of the second group of connection mechanisms connected to the pins 10. Gaps exist between the pins 10 and the connection mechanisms 8, 9 of the struts and between the pins 10 and the second group of connection mechanisms of the connection part 7, so as to ensure that during installation, the pins 10 can be inserted into the connection mechanisms smoothly. As shown in
Preferably, the third positions, for connecting to the root portion 4 of a strut 1, of two adjacent connection parts 7 are symmetrically disposed relative to the central axis of the root portion 4 of the strut.
Further, it should be noted that, the connection part 7 may not have only one pair of the first position and the second position A, B shown in
Persons skilled in the art may easily figure out that other connection mechanisms may be used to replace holes in the first positions, the second positions, and a third position on the connection part 7. The head portion 3 of the struts may be provided with other connection mechanisms instead of holes. However, since the head portions of the struts of some existing exhaust casing have holes, lifting can be performed with these holes saving the cost to prepare connection mechanisms during installation or maintenance. Meanwhile, holes at the second positions B, E of the connection part 7 may not be disposed, as shown in
The connection mechanisms 8, 9 on the head portion 3 and the connection mechanisms 5, 6 on the connection part 7 may be symmetrical relative to the central axis of the root portion 4. However, an alternative in which the connection mechanisms 8, 9 on the head portion 3 and the connection mechanisms 5, 6 on the connection part 7 are asymmetrical relative to the central axis of the root portion also can work.
It should be noted that, the connection part 7 may not be, as shown in
In the embodiments of the present invention, a plurality of separate connection parts, instead of a single connection part, are used to fix a plurality of the outwardly extending struts of the equipment respectively. In this manner each connection part can bear the gravity load of the equipment during lifting and balance the incurred local load at the positions on two sides of the center line of the root portion of the strut. In this way, the gravity load of the lifted equipment can be distributed to multiple struts, thereby the situation where the gravity load is concentrated on a strut is avoided. Meanwhile, the manner of the connection located on two sides of the central axis of the root portion of one strut can balance the local load on the strut incurred during lifting.
Although the device of the present invention is illustrated above with reference to the example of lifting the exhaust casing and the rotor of the gas turbine, persons skilled in the art can understand that the device of the present invention is not limited to lifting the exhaust casing and the rotor of the gas turbine. The device may be used to lift multiple kinds of heavy equipment having a plurality of struts, which include a generator, a motor, and so on.
It should be understood that, although the specification is described according to embodiments, it is not true that each embodiment includes only one independent technical solution. The description manner of the specification is only for clarity, persons skilled in the art shall regard the specification as a whole, and the technical solutions of the embodiments may also be combined appropriately to form other embodiments understandable to persons skilled in the art.
The above embodiments of the present invention are only exemplary, and are not intended to limit the scope of the present invention. Any equivalent change, modification, and combination made by persons skilled in the art without departing from the idea and principle of the present invention shall fall within the protection scope of the present invention.
This application is the national phase under 35 U.S.C. §371 of PCT International Application No. PCT/CN2013/088239 which has an International filing date of Nov. 29, 2013, which designated the United States of America, the entire contents of which are hereby incorporated herein by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/CN2013/088239 | 11/29/2013 | WO | 00 |