Unlock instant, AI-driven research and patent intelligence for your innovation.

Repair compound for repairing composite material and method for repairing composite material using the repair compound

A technology of composite materials and repairing materials, which is applied in the field of repairing composite materials and can solve problems such as unsuitability and cumbersome repairing process steps.

Active Publication Date: 2017-12-26
AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH
View PDF6 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, US5985433, like US 4358480, also has the disadvantages of cumbersome repair process steps, a large amount of small molecular substances, and is not suitable for on-orbit repair in space.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Repair compound for repairing composite material and method for repairing composite material using the repair compound
  • Repair compound for repairing composite material and method for repairing composite material using the repair compound
  • Repair compound for repairing composite material and method for repairing composite material using the repair compound

Examples

Experimental program
Comparison scheme
Effect test

preparation example Construction

[0026] The present invention has no special limitation on the preparation of the first composition, for example, a hydroxyl-terminated silicone rubber prepolymer and a first inorganic filler such as hollow glass microspheres, pulverized rigid heat insulation tile scraps and hydrophobic gas phase II Silica is prepared by grinding in a mortar for 10 to 60 minutes to fully mix the ingredients.

[0027] The present invention has no special limitation on the preparation of the second composition, for example, the inorganic filler such as hollow glass microspheres and rigid heat insulation tile scrap pulverization and crosslinking agent such as orthosilicic acid Ethyl ester and a catalyst such as dibutyltin dilaurate are placed in a mortar and ground for 30 to 60 minutes so that the ingredients are fully mixed and evenly prepared.

[0028] The room temperature curing silicone rubber continuous phase used in the method of the present invention comprises a hydroxyl-terminated silicone...

preparation example 1

[0034] Preparation of a first composition in a repair compound for repairing rigid thermal insulation tiles

[0035] Weigh 50g of hydroxyl-terminated polydimethylsiloxane with a viscosity of 12000cst, 15g of hollow glass microspheres, 10g of crushed rigid insulation tile scraps, and 5.5g of hydrophobic fumed silica, and place them in a research chamber with a volume of 250mL. Grinding in a bowl for 10 minutes, so that the above-mentioned ingredients are fully mixed and uniform, and the first composition of the repair material is obtained.

[0036] Preparation of a second composition in a repair compound for repairing rigid thermal insulation tiles

[0037] Weigh 15g of hollow glass microspheres, 10g of crushed rigid insulation tile scraps, 5g of ethyl orthosilicate and 0.5g of dibutyltin dilaurate, place them in a mortar with a volume of 250mL, grind for 30 minutes, and make the above The ingredients are mixed thoroughly to form a second composition of repair compound.

[00...

preparation example 2 to 10

[0041] Except for the contents shown in the following table, it was carried out substantially in the same manner as Preparation Example 1.

[0042] After testing, the density of each repairing material thus prepared before curing is 0.35-0.55g / cm 3 , the density after curing is 0.45~0.65g / cm 3 .

[0043]

[0044] Repair example 1

[0045] Such as figure 1 As shown in (a), a 150mm × 150mm × 25mm rigid thermal insulation tile with a surface compounded with a high emissivity coating is installed on a titanium alloy metal load-bearing structural substrate through a strain isolation pad and room temperature curing silicone rubber. The surface of the heat insulation tile has an irregular pit-like damage with a maximum diameter of 30mm and a depth of 20mm. This part is processed into a regular cylindrical pit with a diameter of 30mm and a depth of 20mm by a CNC tool, and then a piece with a diameter of 29.8mm is processed. 18mm rigid heat insulation tile column, the side and b...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

PropertyMeasurementUnit
densityaaaaaaaaaa
densityaaaaaaaaaa
Login to View More

Abstract

The invention relates to a repair material for repairing a composite material and a method for repairing the composite material with the repair material. The repair material is prepared from a room temperature cured silicone rubber continuous phase and inorganic filler, wherein the room temperature cured silicone rubber continuous phase contains a hydroxyl-terminated silicone rubber prepolymer, a crosslinking agent and a catalyst. The invention further provides the method for repairing the composite material, such as rigid thermal protection tiles, with the repair material. With the adoption of the repair material, a low-density and high-strength material can be formed in a repaired composite material matrix, and the rigid thermal protection tiles for an aircraft can be repaired both in orbit and on the ground.

Description

technical field [0001] The invention belongs to the technical field of composite material repair, and more specifically, the invention relates to a composite material repair material and a repair method. Background technique [0002] Composite materials, such as rigid thermal insulation tiles, as large-area thermal protection materials for the outer surface of aircraft, have many advantages such as light weight, reusability, high temperature resistance, and good heat insulation effect. However, the impact resistance of rigid thermal insulation tiles is poor, and rigid thermal insulation tiles may be damaged when the aircraft is installed on the ground, transported, launched, orbited or re-entered the atmosphere. Therefore, how to repair the damaged rigid thermal insulation tile is one of the important auxiliary technologies in the engineering application process of the large area thermal protection system of rigid thermal insulation tile. [0003] When the rigid insulation ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): C08L83/06C08K7/28C08K3/36C08K5/5415C08K3/38C08K5/5419B64C1/00
CPCB64C1/00B64C2001/0072C08K3/36C08K3/38C08K5/5415C08K5/5419C08K7/28C08L83/06
Inventor 鲁胜裴雨辰张凡郭慧吴宪刘斌赵英民
Owner AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH