Examples for the use of winLIFE

Examples from the automotive industry show the wide range of applications for winLIFE:

  • Automotive engineering
  • Aircraft construction
  • Wind energy technology
  • Welding engineering
  • Universities

Automotive Industry

Many winLIFE users come from the automotive industry. Two examples from the powertrain and axle sectors illustrate this:

Powertrain

Clutches, torque converters, retarders, gearbox housings, shafts, planetary gears, torsion dampers, trucks and agricultural vehicles.

Measurements were carried out on real tracks to capture real-world conditions. A race track, the Nürburgring, was measured in detail and used as a basis for durability tests, particularly for the powertrain and automatic transmission.

7-speed automatic transmission from Mercedes-Benz AG

The load spectrum measured at the Nürburgring for a Mercedes S 500 with the 7-speed automatic transmission illustrated is shown in the following figure.

Dwell times of torques and speeds at the transmission output for a 7-speed automatic transmission on the Nürburgring with winLIFE (source: Mercedes-Benz AG)
Amplitude frequency as a result of the winLIFE classification of the threshold stress of a gearwheel of a simulation and for comparison test rig tests with different control (DV, DW) of the test rig

AXLE SUSPENSIONS

winLIFE is used in the development of military vehicles. Chassis, axles and springs were calculated with winLIFE. During the road test, measurements were taken on different road categories to determine the particularities caused by road unevenness.

Fennek military vehicle, calculated with winLIFE

FE model of a rim with unit loads for vertical force and wheel hub, which was used as the basis for calculating the fatigue life of the Fennek wheel hub under the influence of the load data measured in the road test (3 forces, 3 moments) using the rotating superposition

Wheel with wheel hub of the "Fennek" and the wheel hub analysed in the fatigue life calculation
Result of the calculation for the wheel hub of the "Fennnek" on different road surfaces and with different driving manoeuvres

Aircraft Applications

Manoeuvring aircraft at an airport is more economical when done by a tow truck. The tow tractor pulls the aircraft with a rod on the front landing gear. The question arose as to what loads would occur compared to normal flight operations and whether this could lead to a fatigue problem.

Strain gauges were attached to the landing gear and measured during manoeuvring and landing. A comparative fatigue life calculation showed the damage caused by the landing and manoeuvring processes and allowed an assessment to be made.

Aircraft used for the measurements
Landing gear with strain gauges

 

As a result, it was possible to assess the relationship between the damage caused by the landing and the manoeuvring with the tow tractor. These processes on the ground can now be taken into account in the overall load on the landing gear.

Wind Turbines

When designing a wind turbine, the fatigue life must be verified using mathematical methods. Wind turbines are designed to last for decades and must be able to withstand strongly changing weather conditions. The towers, rotor hub and components of the wind turbine are calculated in this way.

Offshore turbines, which are located off the coast and are exposed to extreme conditions such as waves, wind and salt water, are subject to even stricter requirements.

To make the work of wind turbine manufacturers easier, calculation rules are integrated, e.g. for generating S-N curves in accordance with the regulations of Germanischer Lloyd. The following figure shows a wind turbine planet carrier calculated with FEMAP and winLIFE.

Planet carrier of an offshore wind turbine (top FE model), bottom results of the fatigue life calculation with 122 load sequences, scaled to a fatigue life of 20 years.

 

The following figure shows results for a gearbox-housing from Zollern Company, which was calculated with ANSYS and winLIFE (damage is shown).

Zollern gearbox housing for fatigue life calculation with ANSYS and winLIFE

Weld Seam Calculation

Hot-Spot Search (Example from Shipbuilding)

The main feature of this method is that, in the case of welded sheets made up of plate elements, the elements are found largely automatically at the plate joints, where the welds are usually located. The element stresses projected perpendicular to the weld notch are used for the fatigue life calculation. As only one element is used for the fatigue life prediction, the weld notch stress is not realistically captured and the prediction quality is poorer than the structural stress concept. However, this method also finds the critical points of a structure. If necessary, the hotspots found can then be recalculated using the structural stress concept to improve the prediction quality.

non-deformed structure without load
Loaded structure including deformation
Result of the weld seam calculation using the hotspot method (amount of damage)
Result of the weld seam calculation according to the structural stress concept (amount of damage)

NOTCH STRESS CONCEPT R1 (SEMITRAILER AXLE)

The welded joint of the rear axle of a semi-trailer was calculated using FEMAP (Fig.). The substructure method was used, in which the relatively coarsely modelled overall model was calculated first. The welds were then "cut out" and modelled very finely according to the specifications of the r1 concept (Figure).

A fatigue life calculation was then performed for the weld only, based on the acting load spectrum. This enabled the critical crack locations to be identified in accordance with the test results and a fatigue life estimate to be calculated and compared for the conditions on the test track and for a real customer collective. The results were very helpful in the development of this axle.

Rear axle of a Kögel semi-trailer, calculated with winLIFE according to the R1 concept
Lines of equal damage on the weld seam
Visualisation of the fatigue life calculation results in winLIFE

STRUCTURAL STRESS CONCEPT (EXAMPLE: UNIMOG TRAILER COUPLING)

The weld seams for the ball head hitch shown are to be calculated according to the structural stress concept. In this example, only the fillet welds on the left-hand side between the U-profile and the rectangular profile are considered, see Fig. 1-1.

Ball head hitch geometry

 

The model is mainly composed of tetrahedral elements. The areas of the weld seams to be analysed are meshed with hexahedral elements. For the structural stress concept with linear extrapolation, defined distances of the node rows from the fillet weld are maintained, as shown by the nodes marked in yellow in the figure.

The distance of node line 1 is 0.4 x plate thickness from the weld seam and the distance of node line 2 is 1 x plate thickness from the weld seam. Therefore, with a plate thickness of the rectangular profile of 7.1 mm, node line 1 is 2.84 mm and node line 2 is 7.1 mm from the fillet weld.

Node line at the fillet weld for the structure stress concept

 

The ball head is subjected to two load cases, which are initially displayed separately. In the following fatigue life calculation in winLIFE, these two load cases act simultaneously.

The ends of the U-profiles are fixed in the area of the holes.

Load Case No.

Type of Load

Load

1

Lateral load

 

Tensile force in y-direction Fy = 20000 N

 

2

Vertical and horizontal load

Tensile force in x direction Fx = 21700 N
and
thrust in z direction of Fz = -12000 N

 

Trailer hitch under lateral load (load case 1)
Trailer hitch under vertical and horizontal loads (load case no. 2)

 

The degree of utilisation is shown in the following figure. A fatigue factor of 0.178 means that 17.8% of the fatigue limit has been used.

Degree of utilisation of the fillet weld

Combination of MBS and FEM Simulation for an Excavator Arm

To analyse the fatigue life of an excavator arm, a multi-body dynamics simulation (Recurdyn) was carried out in combination with a finite element simulation. The results of the time-dependent stresses were imported from Recurdyn and used in winLIFE for the damage accumulation calculation.

Excavator with meshed arm for simulation

 

A stress-time function was determined for each node of the structure and the number of repetitions until cracking was calculated.
The variation of the acceleration during operation showed the influence of the operating conditions on the fatigue life.

Equivalent stress history for the most damaged node

Universities

winLIFE has been used in teaching and research at several universities and colleges for many years. In order to meet the requirements of a larger number of installations, a special university version has been developed. The easy handling of winLIFE enables students to quickly and independently familiarise themselves with the software. The necessary functionality is provided to clearly explain the essential calculation concepts.

The documentation, including examples, is suitable to fully understand the results, so that the student also understands in detail what he or she is working on.

The university version consists of a full version for the supervisor with a separate single user hardlock. An additional network licence for 10 users allows a slightly restricted use of winLIFE BASIC, which is completely sufficient for academic questions.

Image: Interactive stress-strain path simulation. The load step and the resulting stress-strain path are displayed in an image and can be interactively specified by the user. In this way, the laws of material memory can be understood in a playful way
Animation of the Neuber rule and its variants. The Neuber hyperbola is displayed from the starting point. By moving the mouse, the starting point is moved and the lines are animated in real time
To understand the state of stress and strain, Mohr's circle can be visualised for each time step. A deeper understanding and analysis of the problem is possible
Multiaxial yield with the Mroz model. This visualisation can be used to animate the flow of a load-time function (max. 2000 steps)