Essays about: "chocklaster"

Found 3 essays containing the word chocklaster.

  1. 1. Requirements and Analysis of an Overload Protection Mechanism for an Electromechanical Linear Actuator

    University essay from KTH/Maskinkonstruktion (Inst.)

    Author : Mats Vesterberg; [2022]
    Keywords : EMA; Electromechanical Actuator; Linear Actuator; Shock load; Protection mechanism; Elektromekaniska ställdon; Linjära ställdon; Shocklaster; Överlastskydd;

    Abstract : Cascade Drives specializes in high-performance electromechanical linear actuators (EMA). The company has developed a range of linear rack and pinion actuators based on a patented load distribution technique that allows multiple pinions to interact with a single gear rack. READ MORE

  3. 2. Efficiency verification of an electromechanical linear actuator

    University essay from KTH/Skolan för industriell teknik och management (ITM)

    Author : Ingela Råberg; [2021]
    Keywords : Efficiency; Linear actuator; Modelling; Romax; Linjärt ställdon; Modellering; Romax; Verkningsgrad;

    Abstract : Cascade Drives has developed an electromechanical linear actuator with a patented feature which allows for load sharing between multiple pinions interacting on the same rack. This arrangement has proven resilient for shock loads, and allows for compact gearbox designs with very high load rating. READ MORE

  4. 3. Finite Element Analysis of Stresses in the MIST CubeSat due to Dynamic Loads During Launch

    University essay from KTH/Lättkonstruktioner

    Author : Carl Järmyr Eriksson; [2021]
    Keywords : Satellite; CubeSat; Nanosatellite; Dynamic Loads; Launch Loads; Finite Element Analysis; FEA; Quasi-static Acceleration; Modal Analysis; Random Vibration; Shock Loads; satellit; CubeSat; nanosatellit; dynamiska laster; uppskjutningslaster; finita elementmetoden; FEM; kvasistatisk acceleration; modalanalys; stokastiska vibrationer; chocklaster;

    Abstract : A finite element model of the CubeSat MIST was created, in order to assess the stresses that occur in the satellite in response to loads during its launch. Due to size limits of thesoftware used, simplifications had to be made to the geometry of the model. READ MORE