MIT OpenCourseWare http://ocw.mit.edu 2.72 Elements of Mechanical Design Spring 2009 For information about citing these materials or our Terms of Use, visit: http://ocw.mit.edu/terms. 2.72 Elements of Mechanical Design Lecture 05: Structures Schedule and reading assignment Quizzes Quiz – None Topics Finish fatigue Finish HTMs in structures Reading assignment None Quiz next time on HTMs © Martin Culpepper, All rights reserved 2 Matrix Review What is a Matrix? A matrix is an easy way to represent a system of linear equations Linear algebra is the set of rules that governs matrix and vector operations ⎡ b1 ⎤ ⎢b ⎥ ⎣ 2⎦ “Vector” ⎡ a1 ⎢a ⎣ 3 a2 ⎤ ⎥ a4 ⎦ “Matrix” © Martin Culpepper, All rights reserved 4 Matrix Addition/Subtraction You can only add or subtract matrices of the same dimension Operations are carried out entry by entry ⎡ a1 ⎢a ⎣ 3 a2 ⎤ ⎡ b1 +⎢ ⎥ a4 ⎦ ⎣b3 (2 x 2) ⎡ a1 ⎢a ⎣ 3 b2 ⎤ ⎡ a1 + b1 =⎢ ⎥ b4 ⎦ ⎣a3 + b3 (2 x 2) a2 ⎤ ⎡b1 b2 ⎤ ⎡ a1 − b1 −⎢ =⎢ ⎥ ⎥ a4 ⎦ ⎣ b3 b4 ⎦ ⎣ a3 − b3 (2 x 2) © Martin Culpepper, All rights reserved (2 x 2) a2 + b2 ⎤ ⎥ a4 + b4 ⎦ (2 x 2) a2 − b2 ⎤ ⎥ a4 − b4 ⎦ (2 x 2) 5 Matrix Multiplication An m x n matrix times an n x p matrix produces an m x p matrix ⎡ a1 ⎢a ⎣ 3 a2 ⎤ ⎡ b1 ⎥ ⎢ a4 ⎦ ⎣b3 (2 x 2) b2 ⎤ ⎡ a1b1 + a2b3 =⎢ ⎥ b4 ⎦ ⎣ a3b1 + a4b3 (2 x 2) © Martin Culpepper, All rights reserved a1b2 + a2b4 ⎤ ⎥ a3b2 + a4b4 ⎦ (2 x 2) 6 Matrix Properties Notation: A, B, C = matrix , c = scalar Cumulative Law: A+B=B+A Distributive Law: c(A + B) = cA + cB C(A + B) = CA + CB Associative Law: A + (B – C) = (A + B) – C A(BC) = (AB)C NOTE that AB does not equal BA !!!!!!! © Martin Culpepper, All rights reserved 7 Matrix Division To divide in linear algebra we multiply each side by an inverse matrix: AB = C A-1AB = A-1C B = A-1C Inverse matrix properties: A-1A = AA-1 = I (The identity matrix) (AB)-1 = B-1A-1 © Martin Culpepper, All rights reserved 8 Structures Machines structures Structure = backbone = affects everything Satisfies a multiplicity of needs Enforcing geometric relationships (position/orientation) Material flow and access Reference frame Requires first consideration and serves to link modules: Joints (bolted/welded/etc…) Bearings Shafts Parts Tools Sensors Actuators © Martin Culpepper, All rights reserved Image removed due to copyright restrictions. Please see http://www.clarkmachinetools.com/2003_1.jpg 10 Key issues with structural design Machine concepts Topology Material properties Image removed due to copyright restrictions. Please see http://www.fortune-cnc.com/uploads/images/1600ge_series.jpg Principles Thermomechanical Elastomechanics Kinematics Vibration Key tools that help Stick figures Parametric system/part error model © Martin Culpepper, All rights reserved Visualization of the: Load path Vibration modes Thermal growth 11 Modeling: stick figures Image removed due to copyright restrictions. Please see http://americanmachinetools.com/images/diagram-lathe.jpg 3 1 2 © Martin Culpepper, All rights reserved 12 Modeling: stick figures 1. Stick figures These types of models are idealizations of the physical behavior. The designer must KNOW: 2. Beam bending 3. System bend. (a) if beam bending assumptions are valid (b) how to interpret and use the results o this type of these models 3 1 2 © Martin Culpepper, All rights reserved y z x 13 Modeling: stick figures F © Martin Culpepper, All rights reserved 14 Transformation Matrices Translational Transformation Matrix Translational Transformation Matrix Y P=(A+L P=(A, B)1, B+L2)=(A’, B’) Y’ B L1 X A L2 A’ X’ B’ 1 © Martin Culpepper, All rights reserved = 1 0 L1 A 0 1 L2 B 0 0 1 1 16 Translational Transformation Matrix General 2D transformation matrix © Martin Culpepper, All rights reserved 1 0 ΔX 0 1 ΔY 0 0 1 1 0 L1 0 1 L2 0 0 1 17 Rotational Transformation Matrix Rotational Transformation Matrix Y Y’ P=(A, B) P=(A’, B’) B’ X’ B Ө Ө Ө X A’ A © Martin Culpepper, All rights reserved 18 Rotational Transformation Matrix Rotational Transformation Matrix Y Y’ P=(A’, B’) X’ B Ө Ө Ө X A A’ = A cosӨ + B sin Ө © Martin Culpepper, All rights reserved 19 Rotational Transformation Matrix Y Y’ P=(A’, B’) X’ B Ө Ө Ө X A A’ = A cosӨ + B sin Ө B’ = -A sinӨ + B cos Ө © Martin Culpepper, All rights reserved 20 Rotational Transformation Matrix Rotational Transformation Matrix Y Y’ P=(A’, B’) B’ X’ B Ө Ө X A’ cosӨ sinӨ 0 A B’ = -sinӨ A’ = A cosӨ + B sin Ө 1 0 B’ = -A sinӨ + B cos Ө cosӨ 0 B 0 1 1 A © Martin Culpepper, All rights reserved A’ 21 Rotational Transformation Matrix Rotational Transformation Matrix Y (+Ө) Counter Clockwise Y’ General 2D rotational matrix: X’ Ө cosӨ sinӨ 0 -sinӨ cosӨ 0 0 0 1 Ө X Y Y’ (-Ө) Clockwise -sinӨ 0 cosӨ Ө sinӨsinӨ cosӨ cosӨ 0 Ө X -sinӨ 0 0 cosӨ 0 0 0 0 1 1 X’ © Martin Culpepper, All rights reserved 22 Homogeneous Transformation Matrix General 2D HTM translational and rotational matrix: © Martin Culpepper, All rights reserved cosӨ sinӨ Δx -sinӨ cosӨ Δy 0 0 1 23 HTM Applications Simple Beam Example Simple Beam Example: B Y’ A Y X’ X F L © Martin Culpepper, All rights reserved 25 Simple Beam Example Simple Beam Example: A B Y X Y’ Ө D F X’ L © Martin Culpepper, All rights reserved 26 Useful Equations ForceForce-deflection Deflection Equations d d= F d Ө FL EA FL3 d= 3EI FL2 Ө= 2EI F d Ө M © Martin Culpepper, All rights reserved ML2 d= 2EI ML Ө= EI 27 Simple Beam Example Simple Beam Example: A B Y Y’ X Ө D X’ L A B L cosӨ H B D = A = sinӨ 1 © Martin Culpepper, All rights reserved 0 -sinӨ L 0 cosӨ D 0 0 1 1 FL3 D= 3EI FL2 Ө= 2EI 28 Drill Press Example Simple Beam Example: Find the HTM from a to b: L b c b H a D a F F d L e Ha = b Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved A 1 0 0 0 1 -(D-δ) 0 0 1 Ad E 29 Useful Equations ForceForce-deflection Deflection Equations d d= F d Ө FL EA FL3 d= 3EI FL2 Ө= 2EI F d Ө M © Martin Culpepper, All rights reserved ML2 d= 2EI ML Ө= EI 30 Drill Press Example Simple Beam Example: Find the HTM from a to b: L b c b H a D a F F d L e Ha = b Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved E Ad A 1 0 0 0 1 -(D-δ) 0 0 1 δ= FD EAd 31 Drill Press Example Simple Beam Example: Find the HTM from b to c: L c b H a D c b F F d L e Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved c Hb = cosӨ -sinӨ L sinӨ cosӨ δ 0 0 1 A Ad E 32 Useful Equations ForceForce-deflection Deflection Equations d d= F d Ө FL EA FL3 d= 3EI FL2 Ө= 2EI F d Ө M © Martin Culpepper, All rights reserved ML2 d= 2EI ML Ө= EI 33 Drill Press Example Simple Beam Example: Find the HTM from b to c: L c b H a D c b F F d L e Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved E Ad c Hb = cosӨ -sinӨ L sinӨ cosӨ δ 0 0 1 A FL3 δ= 3EI FL2 Ө= 2EI 34 Drill Press Example Simple Beam Example: Find the HTM from c to d: L c c b H a F FL D F d L e Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved Ad A d Hc = d cosӨ -sinӨ -δ1 sinӨ cosӨ H+δ2 0 0 1 E 35 Useful Equations ForceForce-deflection Deflection Equations d d= F d Ө FL EA FL3 d= 3EI FL2 Ө= 2EI F d Ө M © Martin Culpepper, All rights reserved ML2 d= 2EI ML Ө= EI 36 Drill Press Example Simple Beam Example: Find the HTM from c to d: L c c b H a F FL D F d L e Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved E A d Hc = d Ad FLH Ө= EI cosӨ -sinӨ -δ1 sinӨ cosӨ H+δ2 0 0 1 FLH2 δ1 = 2EI FH δ2 = EA 37 Drill Press Example Simple Beam Example: Find the HTM from d to e: L c b H a D d F FL F d L e Hd = e Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved e Ad A 1 0 -L 0 1 0 0 0 1 E 38 Drill Press Example Simple Beam Example: Find the HTM from a to e: L c H a F d L H a = e Hd d Hc c Hb b Ha e b D Find the vector aVe from e to a: 0 e aV Cross-Sectional Area of large sections = Cross-Sectional Area of Drill Bit = Young’s Modulus of Material = © Martin Culpepper, All rights reserved A e = Ha e 0 1 Ad E 39 Method building system’s HTM Simplefor Beam Example: • Identify key nodes around the system’s structural loop • Create HTMs for each member between each node • Multiply the member’s HTMs in the correct order © Martin Culpepper, All rights reserved 40 More on HTMs 3D HTMs For x-axis rotation For y-axis rotation For z-axis rotation 0 ⎡1 ⎢0 cos θ x ⎢ ⎢0 − sin θ x ⎢ 0 ⎣0 ⎡cos θ y ⎢ 0 ⎢ ⎢ sin θ y ⎢ ⎣ 0 ⎡ cos θ z ⎢− sin θ z ⎢ ⎢ 0 ⎢ ⎣ 0 © Martin Culpepper, All rights reserved 0 sin θ x cos θ x 0 0 − sin θ y 1 0 0 0 cos θ y 0 sin θ z cos θ z 0 0 X ⎤ Y ⎥⎥ Z ⎥ ⎥ 1⎦ X⎤ Y ⎥⎥ Z⎥ ⎥ 1⎦ For small Ө: cos(Ө)~1 & sin(Ө)~ Ө 0 X⎤ 0 Y ⎥⎥ 1 Z⎥ ⎥ 0 1⎦ 42 HTM Rotation •Remember order of multiplication matters: 180 deg flip 90 deg right 90 deg right 180 deg flip •To combine a translation and rotation, again multiply the HTM matrices together •Note that the order of the rotation and translation matrices does matter, so makes sure the answer makes sense!!! © Martin Culpepper, All rights reserved 43