RU2019131609A - METHOD FOR REPAIRING THROUGH HOLE IN AIRCRAFT GLAZING - Google Patents

METHOD FOR REPAIRING THROUGH HOLE IN AIRCRAFT GLAZING Download PDF

Info

Publication number
RU2019131609A
RU2019131609A RU2019131609A RU2019131609A RU2019131609A RU 2019131609 A RU2019131609 A RU 2019131609A RU 2019131609 A RU2019131609 A RU 2019131609A RU 2019131609 A RU2019131609 A RU 2019131609A RU 2019131609 A RU2019131609 A RU 2019131609A
Authority
RU
Russia
Prior art keywords
hole
aircraft glazing
repairing
overlay
composition
Prior art date
Application number
RU2019131609A
Other languages
Russian (ru)
Other versions
RU2751373C2 (en
RU2019131609A3 (en
Inventor
Анатолий Андреевич Крылов
Алексей Дмитриевич Пашко
Ирина Владимировна Леденева
Original Assignee
Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации
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 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации filed Critical Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации
Priority to RU2019131609A priority Critical patent/RU2751373C2/en
Publication of RU2019131609A publication Critical patent/RU2019131609A/en
Publication of RU2019131609A3 publication Critical patent/RU2019131609A3/ru
Application granted granted Critical
Publication of RU2751373C2 publication Critical patent/RU2751373C2/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/02—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021—Combinations of fibrous reinforcement and non-fibrous material
    • B29C70/025—Combinations of fibrous reinforcement and non-fibrous material with particular filler
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
    • B60S5/00—Servicing, maintaining, repairing, or refitting of vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)

Claims (1)

Способ ремонта сквозной пробоины в остеклении воздушного судна, включающий дефектацию с замером геометрических характеристик пробоины и определением концентраторов напряжения, обработку пробоины специальным инструментом до получения прямых линий обвода внутренних краев отверстия, отличающийся тем, что после обработки пробоины с внешней стороны остекления воздушного судна устанавливается и фиксируется, на металлизированную клейкую ленту, накладка, размеры которой больше диаметра обработанного отверстия, подготовленный специальный состав светового отверждения порционно размещается в обработанное отверстие со стороны, противоположной установленной накладке, порция состава, в количестве от 20% до 25% от толщины остекления воздушного судна, равномерно распределяется и выравнивается параллельно накладке и просвечивается с помощью ультрафиолетовой лампы с поляризационным эффектом (длина волны 450-500 нм) в течение от 3 до 5 минут, данная операция повторяется до момента полного заполнения отверстия составом.A method for repairing a through hole in an aircraft glazing, including flaw detection with measuring the geometric characteristics of the hole and determining stress concentrators, processing the hole with a special tool until straight lines bypassing the inner edges of the hole are obtained, characterized in that after processing the hole from the outside of the aircraft glazing, it is installed and fixed , on a metallized adhesive tape, an overlay, the dimensions of which are larger than the diameter of the machined hole, a prepared special light-curing compound is placed in portions into the machined hole from the side opposite to the installed overlay, a portion of the composition, in an amount from 20% to 25% of the aircraft glazing thickness, evenly distributed and aligned parallel to the patch and illuminated with an ultraviolet lamp with a polarizing effect (wavelength 450-500 nm) for 3 to 5 minutes, this operation is repeated until the answer is completely filled rstya composition.
RU2019131609A 2019-10-07 2019-10-07 Method of repairing a through breach in aircraft glazing RU2751373C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2019131609A RU2751373C2 (en) 2019-10-07 2019-10-07 Method of repairing a through breach in aircraft glazing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2019131609A RU2751373C2 (en) 2019-10-07 2019-10-07 Method of repairing a through breach in aircraft glazing

Publications (3)

Publication Number Publication Date
RU2019131609A true RU2019131609A (en) 2021-04-07
RU2019131609A3 RU2019131609A3 (en) 2021-04-07
RU2751373C2 RU2751373C2 (en) 2021-07-13

Family

ID=75345850

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2019131609A RU2751373C2 (en) 2019-10-07 2019-10-07 Method of repairing a through breach in aircraft glazing

Country Status (1)

Country Link
RU (1) RU2751373C2 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4995798A (en) * 1989-06-30 1991-02-26 Ameter Stephen L Apparatus for windshield repair
DE4019744C2 (en) * 1990-06-21 1994-05-26 Poly Id Ag Steckborn Device for repairing components made of plastic, in particular made of fiber composite materials
GB9526641D0 (en) * 1995-12-29 1996-02-28 Morris Huw T Glass sheet repair device
RU2131382C1 (en) * 1998-09-10 1999-06-10 Акционерное общество открытого типа "ОКБ Сухого" Method of repair of flying vehicle glazing members

Also Published As

Publication number Publication date
RU2751373C2 (en) 2021-07-13
RU2019131609A3 (en) 2021-04-07

Similar Documents

Publication Publication Date Title
ATE463964T1 (en) DEVICE AND METHOD FOR MEASURING PROPERTIES OF MULTISEGMENT FILTERS OR COMPOSITIONS OF FILTER SEGMENTS
EP3825945A4 (en) Method and device for performing credit evaluation on work publisher based on block chain
WO2008070722A3 (en) Methods and systems for identifying defect types on a wafer
BRPI0402556A (en) Methods to determine defect depth
WO2007005123A3 (en) Automated test case result analyzer
DE60332639D1 (en) USE OF BIOMARKERS FOR THE DETECTION OF EGG CANCER
DE502007001426D1 (en) Device for checking the accuracy of a circular path to be executed by a work spindle
WO2008115991A3 (en) A method and apparatus for estimating a property of a fluid downhole
ATE552489T1 (en) METHOD AND DEVICE FOR MONITORING AND DETECTING COATING DEFECTS IN AN UNDERGROUND OR WATER-LAYED PIPELINE
MX2017012856A (en) Method for determining the abrasion resistance of at least one wear layer arranged on a carrier plate.
RU2019131609A (en) METHOD FOR REPAIRING THROUGH HOLE IN AIRCRAFT GLAZING
WO2008084607A1 (en) Method for measuring immunochromato test piece
EP3951392A4 (en) Immunochromatographic analysis method, and test strip used in said immunochromatographic analysis method
MX2020007306A (en) Synergistic cancer treatment.
WO2007028005A3 (en) Biomarkers and methods for determining sensitivity to vascular endothelial growth factor receptor-2 modulators
WO2008033779A3 (en) Polarization imaging
RU180309U1 (en) DEVICE FOR EVALUATING ADHESIONAL PROPERTIES OF SEALANTS BY SHEAR
CO2023011971A2 (en) Methods for detecting neurofilament light chain in plasma and cerebrospinal fluid
MX2021010357A (en) Process for polysorbate quantification in a sample involving lc-ms with an internal standard.
EP0230182A1 (en) Process for monitoring cracks susceptible to be produced in structures subject to stress
EP2469250A3 (en) Method and apparatus for performing spectroscopy downhole within a wellbore
WO2020237221A9 (en) Methods of monitoring cell culture media
DE502007006770D1 (en) Method for connecting (wood) components
JP3208160U (en) Bolt inspection tool
CN112362623B (en) Physical and chemical adsorption method for identifying single-layer TMDs after laser radiation