scholarly journals Evaluation of Kaiser MX19-B and MX19-C Aluminum Honeycomb Landing Mat

1973 ◽  
Author(s):  
Gordon L. Carr ◽  
Dave A. Ellison
Keyword(s):  
Aluminum Honeycomb ◽  
Landing Mat

scholarly journals Case Study on Fire Resistance of Sandwiches for Means of Transport

Coatings ◽  
2021 ◽  
Vol 11 (2) ◽  
pp. 207
Author(s):  
Pavel Koštial ◽  
Zora Koštialová Jančíková ◽  
Robert Frischer
Keyword(s):  
Fire Resistance ◽  
Fire Protection ◽  
Public Transport ◽  
Hybrid Vehicles ◽  
Safety Requirements ◽  
Different Types ◽  
Aluminum Honeycomb ◽  
Heat Loads

These days there are undeniably unique materials that, however, must also meet demanding safety requirements. In the case of vehicles, these are undoubtedly excellent fire protection characteristics. The aim of the work is to experimentally verify the proposed material compositions for long-term heat loads and the effect of thickness, the number of laminating layers (prepregs) as well as structures with different types of cores (primarily honeycomb made of Nomex paper type T722 of different densities, aluminum honeycomb and PET foam) and composite coating based on a glass-reinforced phenolic matrix. The selected materials are suitable candidates for intelligent sandwich structures, usable especially for interior cladding applications in the industry for the production of means of public transport (e.g., train units, trams, buses, hybrid vehicles).

Axial crushing responses of aluminum honeycomb structures filled with elastomeric polyurethane foam

2021 ◽  
Vol 164 ◽  
pp. 107785
Author(s):  
Yousef Mohamadi ◽  
Hamed Ahmadi ◽  
Omid Razmkhah ◽  
Gholamhossein Liaghat
Keyword(s):  
Polyurethane Foam ◽  
Axial Crushing ◽  
Honeycomb Structures ◽  
Aluminum Honeycomb

The energy-absorbing properties of composite tube-reinforced aluminum honeycomb

2017 ◽  
Vol 176 ◽  
pp. 630-639 ◽  
Author(s):  
A. Al Antali ◽  
R. Umer ◽  
J. Zhou ◽  
W.J. Cantwell
Keyword(s):  
Composite Tube ◽  
Aluminum Honeycomb ◽  
Energy Absorbing

Compression tests on aluminum honeycomb and epoxy resin sandwich panels

2015 ◽  
Vol 4 (2) ◽  
pp. 157-163 ◽  
Author(s):  
Shuliang Cheng ◽  
Xuya Zhao ◽  
Bo Xiao ◽  
Yajun Xin
Keyword(s):  
Epoxy Resin ◽  
Sandwich Panels ◽  
Compression Tests ◽  
Aluminum Honeycomb

scholarly journals Ballistic Resistance of Honeycomb Sandwich Panels under In-Plane High-Velocity Impact

2013 ◽  
Vol 2013 ◽  
pp. 1-20 ◽  
Author(s):  
Chang Qi ◽  
Shu Yang ◽  
Dong Wang ◽  
Li-Jun Yang
Keyword(s):  
Structural Parameters ◽  
Sandwich Panels ◽  
Unit Cell ◽  
Dynamic Responses ◽  
Honeycomb Core ◽  
Ballistic Resistance ◽  
Honeycomb Sandwich ◽  
Aluminum Honeycomb ◽  
Parametric Studies ◽  
Nonmonotonic Effects

The dynamic responses of honeycomb sandwich panels (HSPs) subjected to in-plane projectile impact were studied by means of explicit nonlinear finite element simulations using LS-DYNA. The HSPs consisted of two identical aluminum alloy face-sheets and an aluminum honeycomb core featuring three types of unit cell configurations (regular, rectangular-shaped, and reentrant hexagons). The ballistic resistances of HSPs with the three core configurations were first analyzed. It was found that the HSP with the reentrant auxetic honeycomb core has the best ballistic resistance, due to the negative Poisson’s ratio effect of the core. Parametric studies were then carried out to clarify the influences of both macroscopic (face-sheet and core thicknesses, core relative density) and mesoscopic (unit cell angle and size) parameters on the ballistic responses of the auxetic HSPs. Numerical results show that the perforation resistant capabilities of the auxetic HSPs increase as the values of the macroscopic parameters increase. However, the mesoscopic parameters show nonmonotonic effects on the panels' ballistic capacities. The empirical equations for projectile residual velocities were formulated in terms of impact velocity and the structural parameters. It was also found that the blunter projectiles result in higher ballistic limits of the auxetic HSPs.

scholarly journals Mechanical design and analysis of a gripper for non-cooperative target capture in space

2018 ◽  
Vol 10 (11) ◽  
pp. 168781401881064 ◽  
Author(s):  
Yili Zheng ◽  
Guannan Lei ◽  
Mingwei Zhang ◽  
Qianbo Che
Keyword(s):  
Mechanical Design ◽  
Three Dimensional ◽  
Simulation Software ◽  
Microgravity Environment ◽  
Three Dimensional Modeling ◽  
Target Capture ◽  
Model Collision ◽  
Rigid Connection ◽  
Aluminum Honeycomb ◽  
Ground Test

Space grippers are the key devices for accomplishing space non-cooperative target capture, which has a great significance for satellite services and space debris removal. This article proposes a novel mechanical gripper device for the capture of aluminum honeycomb panels of non-cooperative satellites. The gripper was modeled and assembled in the three-dimensional modeling platform UGNX. The model was imported into the simulation software ADAMS. ADAMS is capable of analyzing the kinematic feasibility of the gripper model. Collision and penetrating power analysis of the mechanical claws into an aluminum honeycomb plate were carried out in LS-DYNA. Through non-vertical piercing experiment, the maximum approaching angle tolerance is 10°. The established rigid connection can withstand a destructive force greater than 1000 N. A prototype of the mechanical gripper is built. A ground test was carried out with this prototype, in which a test-platform simulated the space microgravity environment. The results certified that the prototype could reach the target at a relative speed of 0.5 m/s and then quickly complete the grabbing motion and establish a rigid connection. The experiment shows that this mechanical gripper can accomplish the task of repeatedly capturing the surface of non-cooperative space satellites.

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