MOUNTING TOOL AND METHOD OF MOUNTING FASTENING PINS Russian patent published in 2024 - IPC B25B27/02 B23P19/02 

Abstract RU 2818541 C1

FIELD: engine building.

SUBSTANCE: invention relates to engine assembly, in particular to a tool for installation of a fixing pin and a method of installation. Fixing pin (20) installation tool (100) for fixing the turbine rotor balancing weight comprises tubular housing (110), pressure pin (120) and sliding nut (140), wherein inside tubular housing (110) there is cavity (111) for fixing pins (20), and the surface of tubular housing (110) is made with first slot (112) and the second slot located opposite each other and connected to said cavity (111), wherein two ends of tubular housing (110) have, respectively, first opening (113) and second opening (114), which are connected to cavity (111), and fixing pins (20) are able to enter cavity (111) through first hole (113) and exit from cavity through second hole (114), pressure pin (120) is movable in tubular housing (110) along first slot (112) and second slot, and both ends of pressure pin (120) protrude from the surface of tubular housing (110), and sliding nut (140) is connected to tubular body (110) and is configured to actuate pressure pin (120) towards second hole (114), wherein said tool (100) also comprises pressure cover (130) located on the surface of tubular housing (110), and sliding nut (140) is made with possibility to actuate pressure pin (120) by means of pressure cover (130) for its movement to second hole (114), and on pressure cover (130) there is fixing groove (131) corresponding to pressure pin (120), wherein tubular body (110) also comprises tapered section (115), and inner diameter of at least part of cavity (111) on tapered section (115) is less than diameter of fixing pin (20).

EFFECT: reduced probability of locking pin falling out, increased safety and efficiency of assembly, as well as reduced complexity of installation.

6 cl, 6 dwg

Similar patents RU2818541C1

Title Year Author Number
FASTENING TOOL, BOLT SETTING DEVICE AND METHOD OF ASSEMBLING HIGH-PRESSURE COMPRESSOR ROTOR 2021
  • Hu Yiting
  • Mu Wenxing
  • Pan Fei
  • Zhou Yuqian
RU2817162C1
AIRCRAFT ENGINE COMPRESSOR AND DESIGN FOR FIXING POSITION OF ADJUSTABLE STATOR BLADE 2021
  • Wang Jiaguang
  • Zhu Bin
  • Zhang Miaomiao
  • Gao Haomai
  • Cao Chuanjun
RU2810172C1
NOZZLE WITH BLADE PROFILE TUBE FOR GAS TURBINE 2017
  • Lyu, Jianbo
  • Luo, Hualing
  • Hu, Shuzhen
  • Pan, Xiande
  • Liu, Guofeng
RU2729589C1
CONNECTOR AND CONNECTING DEVICE WITH THERMAL MISMATCH PROTECTION 2020
  • Guo, Hongbao
  • Li, Kaiyuan
  • Hong, Zhiliang
RU2781032C1
BLADE PLATFORM, BLADED ROW, IMPELLER DISK AND GAS TURBINE ENGINE 2021
  • Wu Zhiqing
  • Lu Xiaofeng
  • Yan Dongqing
  • Jiang Ben
  • Li Jibao
  • Yin Zeyong
  • Liu Hao
RU2796182C1
METHOD OF NON-DESTRUCTIVE TESTING FOR LOF-TYPE DEFECTS, STANDARD PART FOR TESTING AND METHOD OF ITS PRODUCTION 2020
  • Li, Yali
  • Lei, Liming
  • Fu, Jun
  • He, Yanli
  • Zheng, Yinlan
RU2808971C1
METHOD FOR PREPARING PREFABRICATED DEFECTS IN FORM OF CRACKS IN ADDITIVE MANUFACTURING OF METAL PARTS AND PREFABRICATED PART MANUFACTURED BY THIS METHOD 2020
  • Fu, Jun
  • Lei, Liming
  • Li, Yali
  • Zhou, Xinmin
  • Fu, Xin
RU2808296C1
METHOD FOR PREPARING PREVIOUSLY MANUFACTURED DEFECTS IN FORM OF GAS PORE, METHOD FOR PREPARING PREVIOUSLY MANUFACTURED PART WITH SUCH DEFECTS IN ADDITIVE MANUFACTURING OF METAL PARTS AND SUCH PREVIOUSLY MANUFACTURED PART 2020
  • Lei, Liming
  • Fu, Jun
  • Li, Yali
  • Zhou, Xinmin
  • Fu, Xin
RU2806071C1
METHOD OF NON-DESTRUCTIVE TESTING FOR CRACK-TYPE DEFECTS, STANDARD PART FOR TESTING AND METHOD OF ITS PRODUCTION 2020
  • Li, Yali
  • Lei, Liming
  • Chen, Xiaohui
  • Fu, Jun
  • Chang, Fei
RU2808972C1
MODELLING METHOD FOR AIRCRAFT ENGINE FAN ASSEMBLY 2019
  • Yang, Xiaohe
  • Pei, Xiaomeng
  • Liu, Shiwen
RU2794994C2

RU 2 818 541 C1

Authors

Hu Yiting

Ren Jiahai

Kou Lingqin

Zhou Yuqian

Dates

2024-05-02Published

2021-07-09Filed