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honeycombing
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Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003037
EISBN: 978-1-62708-200-6
... Abstract Honeycomb is a product consisting of very thin sheets attached to form connecting cells. This article briefly explains the construction, core characteristics, properties, and testing methods of the honeycomb structures. It discusses the special processes carried out in customizing...
Abstract
Honeycomb is a product consisting of very thin sheets attached to form connecting cells. This article briefly explains the construction, core characteristics, properties, and testing methods of the honeycomb structures. It discusses the special processes carried out in customizing the shape of core to fit customer's specific needs. The article provides information on the basic concept of creating sandwich structures and its corresponding aspects like material selection, design guidelines, and structural efficiency.
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0009083
EISBN: 978-1-62708-177-1
... Abstract Honeycomb-cored sandwich panels increase part stiffness at a lower weight than monolithic composite materials. This article illustrates an area of a honeycomb-cored sandwich structure composite cross section that is viewed using transmitted polarized light. This area shows...
Abstract
Honeycomb-cored sandwich panels increase part stiffness at a lower weight than monolithic composite materials. This article illustrates an area of a honeycomb-cored sandwich structure composite cross section that is viewed using transmitted polarized light. This area shows the differences in the constituents and resin intermingling. The article discusses the factors that govern the honeycomb core movement and honeycomb core crush, with illustrations. Some common tests performed on honeycomb composites to characterize the skin-to-core bond strength are the climbing drum peel and flatwise tensile tests. The article concludes with a description on the reasons for core failure, which are analyzed after these tests.
Book: Machining
Series: ASM Handbook
Volume: 16
Publisher: ASM International
Published: 01 January 1989
DOI: 10.31399/asm.hb.v16.a0002194
EISBN: 978-1-62708-188-7
... Abstract This article presents general guidelines for machining metal matrix composites (MMC) and honeycomb structures. It provides guidelines for machining of specific MMCs, namely, aluminum-boron, aluminum-SiC, aluminum-Al 2 O 3 , and titanium-SiC MMCs. In addition, the article discusses...
Abstract
This article presents general guidelines for machining metal matrix composites (MMC) and honeycomb structures. It provides guidelines for machining of specific MMCs, namely, aluminum-boron, aluminum-SiC, aluminum-Al 2 O 3 , and titanium-SiC MMCs. In addition, the article discusses the various parameters influencing drilling of dissimilar-material laminates.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003375
EISBN: 978-1-62708-195-5
... Abstract Lightweight structural cores are used on aircrafts to reduce weight and increase payload and fight distance. This article discusses the classification of lightweight structural cores, namely, honeycomb, balsa, and foam. It reviews the four primary manufacturing methods used to produce...
Abstract
Lightweight structural cores are used on aircrafts to reduce weight and increase payload and fight distance. This article discusses the classification of lightweight structural cores, namely, honeycomb, balsa, and foam. It reviews the four primary manufacturing methods used to produce honeycomb: adhesive bonding and expansion, corrugation and adhesive bonding, corrugation and braze welding, and extrusion. The article describes cell configuration and properties of honeycomb. It discusses the factors influencing specification of structural cores, including materials, size, density, mechanical properties, environmental compatibility, formability, durability, and thermal behavior. The article provides information on the benefits and concepts of a sandwich panel containing lightweight structural cores.
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Published: 01 January 1989
Fig. 12 Expansion method of honeycomb core fabrication. This method consists of printing an adhesive on ribbon sheets, stacking the sheets, and curing the stack in a press at an elevated temperature to form a block of honeycomb.
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Published: 01 January 1989
Fig. 13 High-speed steel tools used for machining nonmetallic honeycomb structures. Left, circular milling cutter chip shredder to break up chips used for finish machining. Right, chip chaser type with notched bottom used for rough machining. Courtesy of Lockheed Aeronautical Systems Company
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Published: 01 December 2004
Fig. 12 Three pieces of honeycomb cut with a diamond wire saw. Note the absence of burrs and breakout. From left: titanium; section from helicopter rotor blade consisting of plastic, paper honeycomb, epoxy, stainless steel screws, and Kevlar; extruded ceramic honeycomb used in automotive
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in Fabrication of Near-Net Shape Cost-Effective Titanium Components by Use of Prealloyed Powder and Hot Isostatic Pressing
> Powder Metallurgy
Published: 30 September 2015
Fig. 12 Titanium 6Al-4V selectively net shape airframe honeycomb structure. All internal geometry of the honeycomb is net shape; the outside and height is subject to final machining.
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Published: 01 January 1994
Fig. 1 Impregnated catalyst washcoated on a substrate honeycomb
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Published: 01 December 2004
Fig. 13 Cross sections of honeycomb node areas showing the number of phenolic resin dip coats. (a) Transmitted light, 100× objective. (b) Void in the node area. Transmitted-light phase contrast, 100× objective
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in Sample Preparation and Mounting for Fiber-Reinforced Composites[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 2 Glass fiber honeycomb composite part submitted for failure analysis. The coordinates were established with a tape measure and a felt-tip permanent-ink marker. The starting point is the lower left corner, numbering “1” to “15” vertically (next to holes) and “A” through “E” horizontally
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in Special Sample Preparation and Polishing for Fiber-Reinforced Composites[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 1 Mounted titanium honeycomb specimen. Note the cuts introduced into the titanium honeycomb to facilitate resin impregnation.
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in Viewing Composite Specimens Using Reflected Light Microscopy[1]
> Metallography and Microstructures
Published: 01 December 2004
Fig. 1 Carbon fiber composite/honeycomb chamfer area. Bright-field illumination, 5× objective. 4 × 5 in. 14-picture (Polaroid) micrograph montage
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Published: 01 December 2004
Fig. 12 Montage of a chamfer area in a honeycomb composite part made with carbon fabric prepreg skins. Bright-field illumination, 5× objective. A magnified view of an area having a void is also shown.
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Published: 01 December 2004
Fig. 9 Glass fabric prepreg honeycomb core composite with voids throughout the structure. Bright-field illumination, 5× objective
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Published: 01 December 2004
Fig. 1 Honeycomb sandwich structure composite cross section (∼1 μm ultrathin section) showing differences in the constituents and resin intermingling. Transmitted crossed polarized light with a 530 nm compensator plate. This micrograph and the insets are expanded to 200× magnification. (A–C
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Published: 01 December 2004
Fig. 2 Ultrathin section of an area of a honeycomb sandwich composite structure showing the effects of core movement during manufacturing and the resulting deformation and separation of the prepreg plies. (a) Transmitted crossed polarized light, 20× objective. (b and c) Transmitted polarized
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Published: 01 December 2004
Fig. 3 Ultrathin section of areas of the honeycomb sandwich composite structure where resin was found to span the separated prepreg plies after core movement. (a) Transmitted light, phase contrast, 40× objective. (b and c) Transmitted light, phase contrast, 20× objective
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