Estimating Optimized Stress Bounds in Early Stage Design of Compliant Mechanisms

2017 ◽  
Vol 139 (6) ◽  
Author(s):  
Sree Kalyan Patiballa ◽  
Girish Krishnan

Design synthesis of distributed compliant mechanisms is often a two-stage process involving (a) conceptual topology synthesis and a subsequent (b) refinement stage to meet strength and manufacturing specifications. The usefulness of a solution is ascertained only after the sequential completion of these two steps that are, in general, computationally intensive. This paper presents a strategy to rapidly estimate final operating stresses even before the actual refinement process. This strategy is based on the uniform stress distribution metric, and a functional characterization of the different members that constitute the compliant mechanism topology. Furthermore, this paper uses the underlying mechanics of stress bound estimation to propose two rule of thumb guidelines for insightful selection of topologies and systematically modifying them for an application. The selection of the best conceptual solution in the early stage design avoids refinement of topologies that inherently may not meet the stress constraints. This paper presents two examples that illustrate these guidelines through the selection and refinement of topologies for a planar compliant gripper application.

Author(s):  
Sreekalyan Patiballa ◽  
John Francis Shanley ◽  
Girish Krishnan

Synthesis of distributed compliant mechanisms is often a two-stage process involving (a) conceptual topology synthesis, and a subsequent (b) refinement stage to meet stress and manufacturing specifications. The usefulness of a solution is ascertained only after the sequential completion of these two steps, which are in general computationally intensive. This paper presents a strategy to rapidly estimate final operating stresses even before the actual refinement process. This strategy is based on the uniform stress distribution metric, and a functional characterization of the different members that constitute the compliant mechanism topology. It enables selecting the best conceptual solution for further optimization, thus maximally avoiding refinement of topologies that inherently may not meet the stress constraints. Furthermore this strategy enables modifying topologies at the early design stage to meet final stress specifications, thus greatly accelerating the overall synthesis process.


2015 ◽  
Author(s):  
Igor Mizine ◽  
Charles Rogers ◽  
Bruce D. Wintersteen

The objective of the ship design synthesis process is to derive a ship’s physical and performance characteristics based on mission requirements and selected technology and configuration options. To accomplish this objective an effective compromise must be achieved between the many competing requirements and constraints that form the available design space. The engineering disciplines that are addressed during the design synthesis process include; mission systems and cargo requirements, hull form geometry, hull subdivision, deckhouse geometry and subdivision, structures, appendages, resistance, propulsors, machinery arrangements, weight estimates, required arrangeable area and volume, intact stability and seakeeping. The hull form is a critical component of the design synthesis process. The hull is subdivided with decks and bulkheads to establish the compartment configuration (to the watertight compartment level) within the hull and to determine if the required mission capabilities and systems can be accommodated. The hull form is the principal boundary for the structural design. Required appendages must be integrated with the hull form. The propulsor design (propellers, waterjets, etc.) depends on resistance and the water flow around the hull form. The hull form significantly drives the propulsion power required and significantly impacts the location of the principle machinery equipment within the hull. While the weight estimates draw directly from the structural design and machinery equipment and other known data (mission systems), many of the other weight groups are estimated by algorithms. These algorithms are very dependent on hull volume and the distribution of that volume within the hull. Hull hydrostatics, stability and seakeeping are all very dependent on the hull form. The investigation of hull form variations during early stage design has long been limited by the capabilities present in the available design tools and their supporting framework. While some excellent hulls have been designed in parallel or preceding the overall ship design process, the limitations in design tools and their integration have often left the design process with a significant unknown as to whether the selected hull form is truly the best configuration for the ship and its mission. The hull form has a significant influence on almost every subsystem and discipline involved in ship design, not just hydrodynamics The routine Navy practice during early stage design has been to perform analysis based on a single baseline hull form point design, which is usually derived from dimensional scaling of existing designs or prototypes. This practice limits analysis of the hull form related characteristics and performance in concert with other tradeoffs and analysis of the disciplines that are very much influenced by the hull form. In some cases, this approach has perpetuated the undesirable characteristics of the selected starting hull form. In many, if not most recent designs, the limitations of our design process capabilities have produced less than optimal hull form configurations, especially in view of the operational profile, which determines the life cycle cost. In addition, late design improvements in hull form such as stern flaps or bulb changes result in the ship exceeding the design requirements that drive cost into the ship, i.e. larger engines installed then required to meet the ship’s KPP for speed. The paper explains how it is possible to overcome this limitation and how to restructure the ship design processes to facilitate effective investigation of hull form variations as part of the design synthesis process. The development of the hull form along with the overall development of the ship design configuration can be effectively integrated during the early Mizine Hull Form Exploration in the Early Stage of Design 2 stages of design when sufficient flexibility remains to enable the most effective design across all disciplines. This paper addresses the process, tools, and methodologies the authors have been developing and applying for several ship design projects to enable the effective development of the hull form and the investigation of hull form variations and their impact on the overall ship effectiveness. The approach used to facilitate the effective integration of the range of design and analysis tools necessary to support the process is described. The methodologies and theories used to investigate the potential range of hull form alternatives and assess their relative performance are presented. Examples of analyses done for actual design projects are provided, along with lessons-learned and recommendations for further refinements and improvements to the processes presented.


Author(s):  
Venkatasubramanian Kalpathy Venkiteswaran ◽  
Hai-Jun Su

The use of pseudo-rigid-body models in the analysis and design of compliant mechanisms has opened up the possibility of using various types of flexible elements within the same framework. In this paper, an idea for combining initially curved and straight beams within compliant mechanisms is developed to create a set of equations that can be easily used to analyze various designs and topologies. A pseudo-rigid-body model with three revolute joints is derived to approximate the behavior of initially-curved compliant beams, to go with another model previously presented for straight beams. The general kinematic and static equations for a single-loop mechanism are shown. Finally, this setup is used for the early-stage design of a compliant constant force mechanism to illustrate its application and comparisons with Finite Element Analysis for validation.


2021 ◽  
Vol 1 ◽  
pp. 11-20
Author(s):  
Owen Freeman Gebler ◽  
Mark Goudswaard ◽  
Ben Hicks ◽  
David Jones ◽  
Aydin Nassehi ◽  
...  

AbstractPhysical prototyping during early stage design typically represents an iterative process. Commonly, a single prototype will be used throughout the process, with its form being modified as the design evolves. If the form of the prototype is not captured as each iteration occurs understanding how specific design changes impact upon the satisfaction of requirements is challenging, particularly retrospectively.In this paper two different systems for digitising physical artefacts, structured light scanning (SLS) and photogrammetry (PG), are investigated as means for capturing iterations of physical prototypes. First, a series of test artefacts are presented and procedures for operating each system are developed. Next, artefacts are digitised using both SLS and PG and resulting models are compared against a master model of each artefact. Results indicate that both systems are able to reconstruct the majority of each artefact's geometry within 0.1mm of the master, however, overall SLS demonstrated superior performance, both in terms of completion time and model quality. Additionally, the quality of PG models was far more influenced by the effort and expertise of the user compared to SLS.


Procedia CIRP ◽  
2015 ◽  
Vol 28 ◽  
pp. 125-130 ◽  
Author(s):  
M. Colledani ◽  
L. Bolognese ◽  
D. Ceglarek ◽  
F. Franchini ◽  
C. Marine ◽  
...  

Author(s):  
Girish Krishnan ◽  
Charles Kim ◽  
Sridhar Kota

Visualizing load flow aids in conceptual design synthesis of machine components. In this paper, we present a mathematical framework to visualize load flow in compliant mechanisms and structures. This framework uses the concept of transferred forces to quantify load flow from input to the output of a compliant mechanism. The key contribution of this paper is the identification a fundamental building block known as the Load-Transmitter Constraint (LTC) set, which enables load flow in a particular direction. The transferred force in each LTC set is shown to be independent of successive LTC sets that are attached to it. This enables a continuous visualization of load flow from the input to the output. Furthermore, we mathematically relate the load flow with the deformation behavior of the mechanism. We can thus explain the deformation behavior of a number of compliant mechanisms from literature by identifying its LTC sets to visualize load flow. This method can also be used to visualize load flow in optimal stiff structure topologies. The insight obtained from this visualization tool facilitates a systematic building block based design methodology for compliant mechanisms and structural topologies.


1988 ◽  
Vol 25 (04) ◽  
pp. 239-252
Author(s):  
G. Robed Lamb

Even though in 1987 there were only a dozen SWATH (smali-waterplane-area twin-hull) craft and ships afloat around the world, word of their markedly superior seakeeping performance is spreading rapidly. The number of SWATH vessels is likely to double within five years. As in many other areas of technology, the United States and Japan are the acknowledged leaders in the development and practical application of the SWATH concept. This paper reviews the characteristics of existing SWATH craft and ships from the standpoint of the stated seakeeping objective. Hull form differences between four SWATH craft and ships, including the Navy's SSP Kairnalino, are analyzed and interpreted. Important considerations for the early-stage design of a SWATH ship are discussed. Differences in the range of feasible hull form geometries for coastal areas and unrestricted ocean operations, and for low-speed versus moderately high-speed applications, are pointed out.


2021 ◽  
Author(s):  
Jonathan M. Smyth ◽  
Robert J. Miller

Abstract This paper proposes a new duty-based Smith Chart as part of an improved method of selecting the geometric topology of compressors (axial, mixed or radial) in the earliest stage of design. The method has a number of advantages over previous methods: it is based on the non-dimensional flow and the non-dimensional work, which aligns with the aerodynamic function of the compressor and is therefore more intuitive than specific speed and specific diameter. It is based on a large number of consistently designed compressor rotors which have been computationally predicted using RANS CFD. Most importantly, it provides the designer not only with a choice of topology but also with the complete meridional geometry of the compressor, its blade design and the number of blades. This fidelity of geometry at the very early stage of design allows the designer to undertake a true systems design optimization (noise, manufacturing, packaging constraints and cost). This has the major advantage of significantly reducing early stage design times and costs and allows the designer to explore completely new products more quickly.


Sign in / Sign up

Export Citation Format

Share Document