PACS Structure Analysis1 PACS IBDR 27/28 Feb 2002 PACS Housing: Structure Analysis Dr. G. Wanderer CASE GmbH.

Slides:



Advertisements
Similar presentations
Reinforced Concrete Design-8
Advertisements

PACE Emerging Market Vehicle Suspension Design University of Cincinnati.
Unit 41 PSD Special Topics Vibrationdata Band-Splitting
Strength of Material-5 Torsion Dr. Attaullah Shah.
MAE 314 – Solid Mechanics Yun Jing
Aircraft Dynamic Response
GLAST LAT ProjectDOE/NASA Mechanical Systems Peer Review, March 27, 2003 Section Mechanical Systems Radiator Assy1 GLAST Large Area Telescope: Mechanical.
CM 197 Mechanics of Materials Chap 20: Connections
PACS IBDR 27/28 Feb 2002 Photoconductor Detector Arrays1 IBDR Hilmar Richter ANTEC-GmbH Germany Günter Bollmann, Peter Dinges, Otto Frenzl, Heidrun Köppen,
#1 212 Ketter Hall, North Campus, Buffalo, NY Fax: Tel: x 2400 Control of Structural Vibrations Lecture.
Lecture # 2 Allowable Stress Objective:
GLAST LAT ProjectDecember 2, 2003 R. Johnson Engineering Meeting 1 GLAST Large Area Telescope: Tracker Subsystem WBS Tracker EM Vibration Test Status.
Static and Fatigue Bolt Design
MODULE 12 RANDOM VIBRATION.
Bolted joint failure modes
Dynamic Mechanical Properties of Metals MADISON MINSK, ANANYA GARG, RACHEL NGAI, IAN CULHANE, ERIC SPEAR.
1 RF-Structures Mock-Up FEA Assembly Tooling V. Soldatov, F. Rossi, R. Raatikainen
Mechanics of Materials – MAE 243 (Section 002) Spring 2008 Dr. Konstantinos A. Sierros.
Chapter Five Vibration Analysis.
University of Palestine
TSU F.E ANALYSIS YAIR SOFFAIR. Ojective Dynamic Response Calculation Temperature Distribution LOS Retention due to Temperatures Design Recommendations.
1 衛星結構設計 祝飛鴻 10/13/  Design Considerations  Environmental Loads  Configuration Design  Structure Analysis  Design Verification  Contest Problem.
Verification by test and quality assurance
GLAST LAT ProjectDOE/NASA Mechanical Systems Peer Review, March 27, 2003 Section Mechanical Systems X-LAT Assy1 GLAST Large Area Telescope: Mechanical.
AAE450 Spring 2009 Finite Element Analysis (FEA) for Orbital Transfer Vehicle (OTV) Tim Rebold STRC [Tim Rebold] [STRC] [1]
Chapter Five Vibration Analysis.
Along-wind dynamic response
ME16A: CHAPTER FIVE DEFLECTION OF BEAMS. CHAPTER FIVE - DEFLECTION OF BEAMS P A yAyA B x v.
An-Najah National University Faculty of Engineering Civil Engineering Department Graduation Project Prepared by : 1- Areej Melhem 2- Jawad Ateyani 3-Rasha.
Overview of Mechanical Engineering for Non-MEs Part 2: Mechanics of Materials 6 Introduction – Concept of Stress.
Basic structural dynamics I Wind loading and structural response - Lecture 10 Dr. J.D. Holmes.
A Multi-Disciplinary Approach to Calculate Displacement Due to Random Vibration For A Space Based Focal Plane Anthony J. Davenport Senior Mechanical Engineer.
Machine Design I (MCE-C 203) Mechatronics Dept., Faculty of Engineering, Fayoum University Dr. Ahmed Salah Abou Taleb Lecturer, Mechanical Engineering.
Structural Analysis & Test in NABI Rt Main Activities of the FE Group Finite Element Estimation for Global & Local structures Software development.
Status report AHCAL Mechanics Karsten Gadow CALICE Collaboration Meeting KEK, Studies of AHCAL absorber structure stability.
1 衛星結構設計 祝飛鴻 5/25/  What are the main functions of structure subsystem?  Provide support all other subsystems and attach the spacecraft to launch.
THEMIS IDPU PDR I&T REQUIREMENTS- 1 UCB, October 16, 2003 I&T REQUIREMENTS Ellen Taylor University of California - Berkeley.
MODULE 08 MULTIDEGREE OF FREEDOM SYSTEMS. 2 Structure vibrating in a given mode can be considered as the Single Degree of Freedom (SDOF) system. Structure.
Silicon-to-Titanium Bond Preload Determination of the JWST NIRSpec Micro Shutter Subsystem FEMCI Workshop 2006 Eduardo Aguayo Jim Pontius.
1 KEK Hiroshi Yamaoka Vibration analysis of the ILD QD0-support system Oct, 2 nd '09 KEK H. Yamaoka - Results of Vibration analysis - Coherency measurement.
1 YamSat Bus Structures Analysis Tsai Ming-Hsien 蔡明憲 2005/03/24 YamSat.
Conclusions on Transverse Shearing Stress Calculations Maximum Value at Neutral Axis – IF CROSS- SECTION IS NOT NARROWER ELSEWHERE –Depends on Shape of.
Calculations for the bolted helium vessel February 2nd 2015 Norbert Kuder, EN/MME.
PACS IIDR 01/02 Mar 2001 PACS Thermal/Structure1 PACS FPFPU Thermal and Structure Analysis Dr. G. Wanderer CASE GmbH.
Date of download: 9/25/2017 Copyright © ASME. All rights reserved.
Mechanics of Solids (M2H321546)
DIGITAL SIGNAL PROCESSOR LNR-26 [LINEA RESEARCH]
Mechanics of Materials Dr. Konstantinos A. Sierros
MOVE2 Solar Panel Analysis
Introduction – Concept of Stress
Concept of Stress.
An-Najah National University
Characterization of C Pod
Characterization of NanoG
Characterization of Omega Pod
DVT 3-D Shaker System in House Ready for Testing
Eccentric Connections in Steel Structures
Earthquake Load Formulation using ASCE7-05
Femap Structural Analysis Toolkit (SATK)
Lecture 3: Vibration in Transport presented by David Shires
Theory of Simple Bending
Structure I Course Code: ARCH 208 Dr. Aeid A. Abdulrazeg
Structure I Course Code: ARCH 208 Dr. Aeid A. Abdulrazeg.
Vibration Basics and Shaker Selection
Strength of Material Torsion Dr. Attaullah Shah.
Vibration Basics and Shaker Selection
Experiment 13 Spring.
Concept of Stress.
CHAPTER SIX DEFLECTION OF BEAMS.
Presentation transcript:

PACS Structure Analysis1 PACS IBDR 27/28 Feb 2002 PACS Housing: Structure Analysis Dr. G. Wanderer CASE GmbH

PACS Structure Analysis2 PACS IBDR 27/28 Feb 2002 •Loads •Strength Analysis of Housing Parts –Housing –Pins and Bolts •Notching of Sine- and Random Qualification Loads •Suspension Analysis –Brackets –Pins and Bolts

PACS Structure Analysis3 PACS IBDR 27/28 Feb 2002 Dynamic and Static Loads Quasistatic: LC1 longitudinal 20g, lateral 2g LC2 lateral 14 g Sine Vibration longitudinal Hz 20g Hz 10g lateral Hz 14g Random Vibration Hz +6 dB/Oct Hz 0,05 g 2 /Hz Hz -6 dB/Oct

PACS Structure Analysis4 PACS IBDR 27/28 Feb 2002 Material The PACS Housing is build of AW 6061T6, Bolts and Pins are of Typ A4-70 (i. e. Steel AISI 316) Ref: MIL HDBK-5H, ESACRACK user´s manual

PACS Structure Analysis5 PACS IBDR 27/28 Feb 2002 Spectrometer Housing Spectrometer Housing is the highest loaded part except Suspension Stresses in Spectrometer Housing:

PACS Structure Analysis6 PACS IBDR 27/28 Feb 2002 Spectrometer Housing

PACS Structure Analysis7 PACS IBDR 27/28 Feb 2002 Pins And Bolts

PACS Structure Analysis8 PACS IBDR 27/28 Feb 2002 Notching of Vibration Loads Accelerometer- Positions with good correlation to I/F Forces

PACS Structure Analysis9 PACS IBDR 27/28 Feb 2002 Monitoring of I/F Loads I/F Loads for constant 1g Sine Reference Grid 13136

PACS Structure Analysis10 PACS IBDR 27/28 Feb 2002 Notch Procedure • an accelerometer is located on the FPU at a place that the measured values correspond to the interface loads • the notch calculation is based on the FE results scaled to the measured damping values for the major natural modes. • random vibration: – the equivalent force is calculated for each major natural mode by integrating the Force Power Spectral Density (PSD) around the mode – The 4-sigma response is limited to the static load level for each major natural mode. – The notch width shall be smaller than 1/3 octave around the natural frequency. – The slope of the notch shall be as steep as possible (more than 24dB/Oct, typical 50dB/Oct). • sine vibration: – the output is limited to the calculated static interface force in the frequency range 50 to 100 Hz

PACS Structure Analysis11 PACS IBDR 27/28 Feb Axis Suspension

PACS Structure Analysis12 PACS IBDR 27/28 Feb 2002 Forces in Suspensions

PACS Structure Analysis13 PACS IBDR 27/28 Feb axis Suspension •critical load path through pin of diameter 10mm (shear)   = F/(2*A) = 7975N/(2*78mm 2 ) = 50,8N/mm 2 •s = F*l/8W = 7975N*6mm / (8*98mm 3 ) = 60,9 N/mm 2 •sMises = 107 MPa