JPS6448671A - Production of honeycomb structure - Google Patents

Production of honeycomb structure

Info

Publication number
JPS6448671A
JPS6448671A JP20614987A JP20614987A JPS6448671A JP S6448671 A JPS6448671 A JP S6448671A JP 20614987 A JP20614987 A JP 20614987A JP 20614987 A JP20614987 A JP 20614987A JP S6448671 A JPS6448671 A JP S6448671A
Authority
JP
Japan
Prior art keywords
filler metal
brazing filler
thermal spraying
film layer
amorphous
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.)
Pending
Application number
JP20614987A
Other languages
Japanese (ja)
Inventor
Tetsuo Toyoda
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.)
Showa Aircraft Industry Co Ltd
Original Assignee
Showa Aircraft Industry 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 Showa Aircraft Industry Co Ltd filed Critical Showa Aircraft Industry Co Ltd
Priority to JP20614987A priority Critical patent/JPS6448671A/en
Publication of JPS6448671A publication Critical patent/JPS6448671A/en
Pending legal-status Critical Current

Links

Landscapes

  • Laminated Bodies (AREA)

Abstract

PURPOSE:To eliminate the need for a temporary fixing and to thin the thickness of a brazing filler metal as well with the joining part being compact without any defect by thermally spraying the powder of an amorphous brazing filler metal at high speed and yet high heating by a plasma thermal spraying device and executing brazing by forming the coating layer thereof. CONSTITUTION:At a thermal spraying stage, the powder of an amorphous brazing filler metal A is thermally sprayed on a flat or corrugated sheet 2 or 3 by the thermal spraying gun 4 of a plasma thermal spraying device 1. At the following film layer forming stage the film layer of the amorphous brazing filler metal A is formed on the specified part of such the sheet 2 or 3. Since the film layer of the amorphous brazing filler metal A is formed by high speed and high heat thermal spray like this, the temporary fixing is unnecessary, no org. solvent, etc., are contaminated, its thickness can be made thinner than that of a thin plate 2 or 3 and the adhesive force to the plate 2 or 3 is strong.
JP20614987A 1987-08-18 1987-08-18 Production of honeycomb structure Pending JPS6448671A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20614987A JPS6448671A (en) 1987-08-18 1987-08-18 Production of honeycomb structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20614987A JPS6448671A (en) 1987-08-18 1987-08-18 Production of honeycomb structure

Publications (1)

Publication Number Publication Date
JPS6448671A true JPS6448671A (en) 1989-02-23

Family

ID=16518605

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20614987A Pending JPS6448671A (en) 1987-08-18 1987-08-18 Production of honeycomb structure

Country Status (1)

Country Link
JP (1) JPS6448671A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5024368A (en) * 1989-08-01 1991-06-18 British Aerospace Stopping-off method for use with diffusion bonding
US5084361A (en) * 1990-04-17 1992-01-28 Showa Aircraft Industry Co., Ltd. Heat resistant structure
US5316997A (en) * 1989-08-04 1994-05-31 Showa Aircraft Industry Co., Ltd. Heat resisting structure

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5024368A (en) * 1989-08-01 1991-06-18 British Aerospace Stopping-off method for use with diffusion bonding
US5316997A (en) * 1989-08-04 1994-05-31 Showa Aircraft Industry Co., Ltd. Heat resisting structure
US5084361A (en) * 1990-04-17 1992-01-28 Showa Aircraft Industry Co., Ltd. Heat resistant structure

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