CN216464380U - Preassembling tool - Google Patents

Preassembling tool Download PDF

Info

Publication number
CN216464380U
CN216464380U CN202122281884.0U CN202122281884U CN216464380U CN 216464380 U CN216464380 U CN 216464380U CN 202122281884 U CN202122281884 U CN 202122281884U CN 216464380 U CN216464380 U CN 216464380U
Authority
CN
China
Prior art keywords
support
section
mandrel
rotor
tool according
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202122281884.0U
Other languages
Chinese (zh)
Inventor
于德庆
赵波
蔡明�
李洪岩
王君禹
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AECC Harbin Dongan Engine Co Ltd
Original Assignee
AECC Harbin Dongan Engine Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by AECC Harbin Dongan Engine Co Ltd filed Critical AECC Harbin Dongan Engine Co Ltd
Priority to CN202122281884.0U priority Critical patent/CN216464380U/en
Application granted granted Critical
Publication of CN216464380U publication Critical patent/CN216464380U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Rotary Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The utility model discloses a preassembly tool which comprises a mandrel and a support; the support is of a hollow rotary body structure, an inner hole is formed in the support along the axial direction, the inner hole is divided into three sections from top to bottom, the first section is in clearance fit with the outer diameter of the rotor, the second section is matched with the mandrel, and the third section is a vent hole; the side wall of the mandrel is radially provided with a key slot penetrating through the mandrel and used for installing the blade. The pre-assembly tool provided by the utility model simulates the assembly of the blades and the rotor in the pump shell, and the blades and the rotor are assembled in the pump after being tested without being clamped, so that the repeated disassembly condition is avoided, the blade scrapping caused by repeated disassembly is prevented, and the assembly efficiency is improved.

Description

Preassembling tool
Technical Field
The utility model relates to the field of assembly of aviation pump products, in particular to a pre-assembly tool.
Background
The aviation pump product needs to rotate after assembling the blades and the rotor, so that a gap is ensured between the blades and the rotor, clamping stagnation is avoided, if clamping stagnation exists, the blades and the rotor need to be integrally disassembled and removed and then re-selected, a plurality of pairs of blades and rotors are assembled by the pump, and one clamping stagnation can lead to the disassembly of other parts together. The whole stereoplasm anodization that carries out of blade is handled, and stereoplasm treatment back blade surface is more fragile, relapses the dismouting and can lead to blade surface to jump the stubble, and then leads to the blade to scrap, and relapse the dismouting and influence efficiency.
Disclosure of Invention
The utility model aims to provide a preassembly tool to solve the problem that blades are scrapped due to repeated disassembly and assembly.
In order to realize the task, the utility model adopts the following technical scheme:
a preassembly tool comprises a mandrel and a support;
the support is of a hollow revolving body structure, an inner hole is formed in the support along the axial direction, the inner hole is divided into three sections from top to bottom, the first section is in clearance fit with the outer diameter of the rotor, the second section is matched with the mandrel, and the third section is a vent hole; the side wall of the mandrel is radially provided with a key groove penetrating through the mandrel and used for installing the blade.
Further, the preassembly tool further comprises an orientation pin;
the directional pin is a square pin and is used for matching with a pin hole formed in the support to install the rotor of the pump in the support.
Further, the inner diameters of the first section, the second section and the third section of the inner hole are gradually increased.
Further, the bottom end fillet of the first section of the inner hole of the support is not more than R0.1.
Further, the support is of a boss-shaped structure, and the first section of the inner hole is located in the protrusion of the boss.
Furthermore, the pin hole is formed in the end face of the first section of the inner hole.
Further, a shaft shoulder is arranged between the second section and the third section of the inner hole of the support for assembling the mandrel.
Further, a pair of key slots is vertically arranged on the mandrel, and the key slots penetrate through the axis of the mandrel.
Further, the distance from the pin hole in the support to the axis of the support is the same as the distance from the positioning pin hole in the rotor to the axis of the support.
Compared with the prior art, the utility model has the following technical characteristics:
the pre-assembly tool provided by the utility model simulates the assembly of the blades and the rotor in the pump shell, and the blades and the rotor are assembled in the pump after being tested without being clamped, so that the repeated disassembly condition is avoided, the blade scrapping caused by repeated disassembly is prevented, and the assembly efficiency is improved.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic top view of the pedestal portion.
The reference numbers in the figures illustrate: 1 mandrel, 2 supports, 3 inner holes, 4 first section, 5 second section, 6 third section, 7 pin holes and 8 orientation pins.
Detailed Description
Referring to the drawings, the utility model provides a pre-assembly tool which simulates the assembly of a blade and a rotor in a pump shell, and the blade and the rotor are assembled in a pump after being tested and not clamped, so that the repeated disassembly condition is avoided.
As shown in the figure, the preassembly tool comprises a mandrel 1, a support 2 and an orientation pin 8;
the support 2 is of a hollow revolving body structure, an inner hole 3 is formed in the support 2 along the axial direction, the inner hole 3 is divided into three sections from top to bottom, a first section 4 is in clearance fit with the outer diameter of the rotor, a second section 5 is in fit with the mandrel 1, and a third section 6 is a vent hole; a key groove penetrating through the mandrel 1 is formed in the side wall of the mandrel 1 along the radial direction and used for mounting a blade; the orientation pin 8 is a square pin and is used for matching with a pin hole 7 arranged in the support 2 to install the rotor of the pump in the support 2.
Wherein, the inner diameters of the first section 4, the second section 5 and the third section 6 of the inner hole 3 are gradually increased.
The bottom end fillet of the first section 4 of the inner hole 3 of the support 2 is not more than R0.1, so that assembly interference is prevented; the support 2 is of a boss-shaped structure, and the first section 4 of the inner hole 3 is positioned in the bulge of the boss.
And the third section 6 of the inner hole 3 of the support 2 is used for integrally penetrating the support 2 and preventing the influence of the internal air on assembly during assembly.
The pin hole 7 is arranged on the end surface of the first section 4 of the inner hole 3.
And a shaft shoulder is arranged between the second section 5 and the third section 6 of the inner hole 3 of the support 2 and is used for assembling the mandrel 1.
In the scheme, a pair of key grooves is vertically arranged on the mandrel 1, and the key grooves penetrate through the axis of the mandrel 1.
The upper end of the mandrel 1 is provided with a reticulate pattern, so that the friction force is improved. The mandrel 1 is provided with a cross-hatched portion having an outer diameter smaller than the outer diameter of the remaining portion.
The distance from the pin hole 7 on the support 2 to the axis of the support 2 is the same as the distance from the positioning pin hole on the rotor to the axis of the support 2.
The using process of the utility model is as follows:
the rotor is fixed in the support 2 by the positioning pin 8 penetrating through the positioning pin hole on the rotor, then the blade penetrates through the key slot on the mandrel 1, the mandrel 1 with the blade is placed into the support 2, the lower end of the mandrel 1 is assembled to the second section 5 of the inner hole 3, then the mandrel 1 is rotated to drive the blade to rotate together, whether the blade is interfered with the rotor or not is observed, if so, the blade is replaced, and the blade can be assembled into formal parts without interference.
The above embodiments are only used for illustrating the technical solutions of the present application, and not for limiting the same; although the present application has been described in detail with reference to the foregoing embodiments, it should be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equally replaced; such modifications and substitutions do not substantially depart from the spirit and scope of the embodiments of the present application, and are intended to be included within the scope of the present application.

Claims (9)

1. The preassembly tool is characterized by comprising a mandrel (1) and a support (2);
the support (2) is of a hollow revolving body structure, an inner hole (3) is formed in the support (2) along the axial direction, the inner hole (3) is divided into three sections from top to bottom, a first section (4) is in clearance fit with the outer diameter of a rotor, a second section (5) is in fit with the mandrel (1), and a third section (6) is a vent hole; the side wall of the mandrel (1) is radially provided with a key groove which penetrates through the mandrel (1) and is used for installing the blade.
2. The preassembly tool according to claim 1, characterized in that it further comprises an orientation pin (8);
the orientation pin (8) is a square pin and is used for matching with a pin hole (7) formed in the support (2) to install the rotor of the pump in the support (2).
3. The preassembly tool according to claim 1, characterized in that the first, second and third sections (4, 5, 6) of the bore (3) have a gradually increasing inner diameter.
4. The preassembly tool according to claim 1, characterized in that the bottom end fillet of the first section (4) of the inner bore (3) of the support (2) is not greater than R0.1.
5. A preassembly tool according to claim 1, characterized in that the seat (2) is of boss-like configuration, the first section (4) of the bore (3) being located in the projection of the boss.
6. The preassembly tool according to claim 2, characterized in that the pin hole (7) opens out on the end face of the first section (4) of the inner bore (3).
7. The preassembly tool according to claim 1, characterized in that a shoulder is provided between the second (5) and third (6) sections of the inner bore (3) of the support (2) for assembling the spindle (1).
8. The preassembly tool according to claim 1, characterized in that a pair of keyways is vertically arranged on the spindle (1), the keyways passing through the axis of the spindle (1).
9. The preassembly tool according to claim 1, characterized in that the distance from the pin hole (7) on the support (2) to the axis of the support (2) is the same as the distance from the locating pin hole on the rotor to the axis of the support (2).
CN202122281884.0U 2021-09-18 2021-09-18 Preassembling tool Active CN216464380U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122281884.0U CN216464380U (en) 2021-09-18 2021-09-18 Preassembling tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122281884.0U CN216464380U (en) 2021-09-18 2021-09-18 Preassembling tool

Publications (1)

Publication Number Publication Date
CN216464380U true CN216464380U (en) 2022-05-10

Family

ID=81436033

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202122281884.0U Active CN216464380U (en) 2021-09-18 2021-09-18 Preassembling tool

Country Status (1)

Country Link
CN (1) CN216464380U (en)

Similar Documents

Publication Publication Date Title
CN111927876A (en) Thrust air foil bearing
EP1795756A1 (en) Fixed vane of turbo molecular pump
EP2267868B1 (en) Rotor for permanent magnet electric machine
JP5606358B2 (en) Impeller, rotor provided with the same, and method for manufacturing impeller
JP2013047479A (en) Impeller and rotary machine with the same, and method for manufacturing impeller
US9664055B2 (en) Impeller and rotary machine provided with the same
JP2016077034A (en) Rotor with balancer weight, and motor
JPH03184726A (en) Method for manufacturing impeller or rotor having not less than one vanes for turbine pump application using electrical discharge machining and device manufactured thereby
US6554476B2 (en) Dynamic pressure bearing device and method of manufacturing the same
CN216464380U (en) Preassembling tool
JP2013139753A (en) Impeller, rotor comprising the same, and impeller manufacturing method
WO2017203917A1 (en) Rotating body and supercharger
CN109510419B (en) High-speed motor rotor
CN115528846A (en) High-rotation-speed motor and tool and machining process thereof
CN212296501U (en) Blade installation positioning tool and assembly thereof
CN216478012U (en) Shaft disc
CN218940893U (en) Rotary-changing rotor machining tool with limiting function
JP2019529765A (en) Axial turbine with diaphragm divided into two halves at horizontal interface
CN202940707U (en) Tool for motor rotor into shaft
WO2017094159A1 (en) Rotor of centrifugal compressor, centrifugal compressor, and method for manufacturing rotor of centrifugal compressor
CN218958641U (en) Mounting piece, stator and electric tool
CN211135653U (en) Rotor end face hole jig
CN219268592U (en) Shell of oil pump motor, oil pump motor and oil pump
CN218498925U (en) High-rotating-speed motor and tool thereof
CN220732462U (en) Novel structure of motor rotor

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant