Published October 1, 2017 | Version v1
Journal article

Application of Foldcore Sandwich Structures in Helicopter Subfloor Energy Absorption Structure

  • 1. Key Laboratory of Fundamental Science for National Defence-Advanced Design Technology of Flight Vehicles, Nanjing University of Aeronautics and Astronautics, 29 YuDao Street. Nanjing 210016 (China)

Description

The intersection element is an important part of the helicopter subfloor structure. The numerical simulation model of the intersection element is established and the crush simulation is conducted. The simulation results agree well with the experiment results. In order to improve the buffering capacity and energy-absorbing capacity, the intersection element is redesigned. The skin and the floor in the intersection element are replaced with foldcore sandwich structures. The new intersection element is studied using the same simulation method as the typical intersection element. The analysis result shows that foldcore can improve the buffering capacity and the energy-absorbing capacity, and reduce the structure mass. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/248/1/012033

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
248
Journal Issue
1
Journal Page Range
[7 p.]
ISSN
1757-899X

Conference

Title
2017 international conference on structural, mechanical and materials engineering
Acronym
ICSMME 2017
Dates
13-15 Jul 2017
Place
Seoul (Korea, Republic of)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
50053963
Subject category
S73: NUCLEAR PHYSICS AND RADIATION PHYSICS; S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
BUFFERS; CAPACITY; COMPUTERIZED SIMULATION; ENERGY ABSORPTION; EXPERIMENT RESULTS; FLOORS; HELICOPTERS; MASS
Descriptors DEC
ABSORPTION; AIRCRAFT; SIMULATION; SORPTION