Adjustable internal support restraint device for roundness control of cabin component

Patent metadata

Field	Value
Publication number	US-2021362880-A1
Application number	US-202117167079-A
Country	US
Kind code	A1
Filing date	Feb 4, 2021
Priority date	May 25, 2020
Publication date	Nov 25, 2021
Grant date	—

Abstract

Disclosed is an adjustable internal support restraint device for roundness control of a cabin component. The present disclosure solves the problem that the existing cabin components are prone to roundness distortion in a heat treatment process. The adjustable internal support restraint device includes a central limiting column and at least two circumferential ejecting correcting assemblies that are coaxially mounted on the central limiting column in a sleeving manner. Each circumferential ejecting correcting assembly includes a mounting piece and a plurality of ejector blocks. The mounting piece is mounted on the central limiting column in a sleeving manner. The plurality of the ejector blocks are annularly arranged outside the mounting piece and are in threaded connection with the mounting piece. One side surface, close to the inner cavity profile of a cabin, of each ejector block and the inner cavity profile of the cabin are arranged according to the shapes.

First claim

1 . An adjustable internal support restraint device for roundness control of a cabin component, comprising a central limiting column and at least two circumferential ejecting correcting assemblies that are coaxially mounted on the central limiting column in a sleeving manner, wherein each circumferential ejecting correcting assembly includes a mounting piece and a plurality of ejector blocks; the mounting piece is mounted on the central limiting column in a sleeving manner; the plurality of the ejector blocks are annularly arranged outside the mounting piece and are in threaded connection with the mounting piece; one side surface, close to the inner cavity profile of a cabin, of each ejector block and the inner cavity profile of the cabin are arranged according to the shapes.

2 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 1 , wherein the mounting piece comprises a mounting ring and a plurality of support arms that are uniformly and fixedly mounted on an outer wall of the mounting ring; the number of the support arms is the same as that of the ejector blocks in each circumferential ejecting correcting assembly; the plurality of the ejector blocks are in threaded connection with the plurality of the support arms in one-to-one correspondence.

3 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 2 , wherein the support arm comprises a cylindrical section and a threaded section that are fixedly connected end to end and are formed integrally; one end of the cylindrical section is fixedly connected to the mounting ring; the ejector block is in threaded connection with the threaded section; the threaded section, between one end of the ejector block and the other end of the cylindrical section, is in threaded connection with an eyelet bolt.

4 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 2 , wherein the mounting ring is in clearance fit with the central limiting column.

5 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 3 , wherein the mounting ring is in clearance fit with the central limiting column.

6 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 4 , wherein when the inner cavity profile of the cabin is a cambered surface, the ejector block is in full arc length or half arc length fit with the inner cavity profile of the cabin.

7 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 5 , wherein when the inner cavity profile of the cabin is a cambered surface, the ejector block is in full arc length or half arc length fit with the inner cavity profile of the cabin.

8 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 1 , wherein the cross section of one side surface, close to the inner cavity profile of the cabin, of the ejector block is wave-shaped or square wave-shaped.

9 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 2 , wherein the cross section of one side surface, close to the inner cavity profile of the cabin, of the ejector block is wave-shaped or square wave-shaped.

10 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 3 , wherein the cross section of one side surface, close to the inner cavity profile of the cabin, of the ejector block is wave-shaped or square wave-shaped.

11 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 6 , wherein the cross section of one side surface, close to the inner cavity profile of the cabin, of the ejector block is wave-shaped or square wave-shaped.

12 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 7 , wherein the cross section of one side surface, close to the inner cavity profile of the cabin, of the ejector block is wave-shaped or square wave-shaped.

13 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 8 , wherein the number of the support arms is four, and the four support arms are arranged pairwise in opposite directions in a manner of ejecting each other.

14 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 2 , wherein the number of the circumferential ejecting correcting assemblies is three.

15 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 3 , wherein the number of the circumferential ejecting correcting assemblies is three.

16 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 6 , wherein the number of the circumferential ejecting correcting assemblies is three.

17 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 7 , wherein the number of the circumferential ejecting correcting assemblies is three.

18 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 14 , wherein the central limiting column is a hollow cylinder.

19 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 15 , wherein the central limiting column is a hollow cylinder.

20 . The adjustable internal support restraint device for roundness control of a cabin component according to claim 16 , wherein the central limiting column is a hollow cylinder.

Assignees

• Harbin Inst Technology

Inventors

• Jiang Jiantang
• Jiang Hao
• Yuan Yong
• Shao Wenzhu
• Zhen Liang

Classifications

• B21D3/14

  Recontouring · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B21D7/03

  Apparatus with means to keep the profile in shape · CPC title

• B64G1/22

  Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles · CPC title

• B21D3/00

  Straightening or restoring form of metal rods, metal tubes, metal profiles, or specific articles made therefrom, whether or not in combination with sheet metal parts (straightening of well casings in situ E21B; {straightening rails or rail joints E01B31/08}) · CPC title