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Miroslaw A Ostaszewski

age ~64

from Louisville, CO

Also known as:
  • Miroslaw Antoni Ostaszewski
  • Joanna Ostaszewski
  • Miroslaw Antoni I

Miroslaw Ostaszewski Phones & Addresses

  • Louisville, CO
  • Steamboat Springs, CO
  • Frisco, CO
  • Bayonne, NJ
  • Fort Collins, CO
  • Louisville, CO
  • Orlando, FL
  • Boulder, CO

Work

  • Company:
    Seagate technology
    Mar 1995 to Jan 2001
  • Position:
    Senior staff engineer

Education

  • Degree:
    Masters, Master of Engineering
  • School / High School:
    Stevens Institute of Technology
    1982 to 1984
  • Specialities:
    Engineering, Mechanical Engineering

Skills

Space Systems • Aerospace • Simulations • Engineering Management • Sensors • Aerospace Engineering • Satellite • Systems Engineering • Systems Design

Industries

Aviation & Aerospace

Us Patents

  • Reactionless Scanning And Positioning System

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  • US Patent:
    52836827, Feb 1, 1994
  • Filed:
    Oct 6, 1992
  • Appl. No.:
    7/957420
  • Inventors:
    Miroslaw A. Ostaszewski - Boulder CO
  • Assignee:
    Ball Corporation - Muncie IN
  • International Classification:
    G02B 2608
  • US Classification:
    359198
  • Abstract:
    A reactionless scanning and positioning system is disclosed which includes a mirror scanning assembly coupled to a reaction mass having a rotational moment of inertia equal and opposite to that of the mirror assembly, so that the system is effectively reactionless. The overall mechanical design of the scanning system is optimized to require minimum power consumption by the actuators used to drive the scanning assembly. The scanning assembly is mounted on flexible pivots having a torsional stiffness which provides a mechanically resonant frequency such that a minimum amount of power is required to angularly position the mirror. A position encoder disc is used in both coarse positioning mode and in a relatively fast scanning mode to determine the position of the mirror. In the present invention, the position of the mirror is accurately determinable in a fast scanning mode due to the novel mounting of the mirror with respect to the position encoder disc.
  • Reactionless Scan Mechanism

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  • US Patent:
    52770761, Jan 11, 1994
  • Filed:
    Jun 8, 1992
  • Appl. No.:
    7/894889
  • Inventors:
    Miroslaw Ostaszewski - Boulder CO
  • Assignee:
    Ball Corporation - Muncie IN
  • International Classification:
    F16H 2144
  • US Classification:
    74 96
  • Abstract:
    Pivotal platform apparatus (10) includes a frame member (12), a platform member (14) being pivotally attached to the frame member and having a first rotational inertia, and a reaction member (20) being pivotally attached to the frame member and having a second rotational inertia. A pair of crossed taut elements (40a and 40b) provide means for transmitting reverse rotation pivotal movement between the platform member and the reaction member so that the inertia of the reaction member balances the reaction of the platform member to provide a reactionless scan mechanism. A pair of motors (26a and 26b), each having pole pieces (30a and 30b) attached to the reaction member, and each having motor coils (28a and 28b) attached to the frame member, provide means for rotationally positioning the reaction member.
  • Suspension System Having Two Degrees Of Rotational Freedom

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  • US Patent:
    55292771, Jun 25, 1996
  • Filed:
    Sep 20, 1994
  • Appl. No.:
    8/309039
  • Inventors:
    Miroslaw A. Ostaszewski - Louisville CO
  • Assignee:
    Ball Corporation - Muncie IN
  • International Classification:
    F16M 1300
  • US Classification:
    248603
  • Abstract:
    A system is described which utilizes two perpendicular four-bar linkages coupled by a common plate to provide a translational-free flexible suspension having two rotational degrees of freedom about a desired point. One of the four-bar linkages is secured to a stationary "ground" structure, and the other linkage is attached to the object to be supported, such as a mirror. In one embodiment, two links of each of the two four-bar linkages are constructed from spring steel flexure elements which are rigid in all directions except about the rotational axis. The flexure elements thus comprise "revolute joints". Because the flexure elements function as spring hinges, no friction is encountered when the suspension is displaced or "pivoted".
  • Systems And Methods For Limiting Rotation Of A Supported Object

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  • US Patent:
    20220290800, Sep 15, 2022
  • Filed:
    Feb 18, 2022
  • Appl. No.:
    17/675024
  • Inventors:
    - Boulder CO, US
    Miroslaw A. Ostaszewski - Louisville CO, US
    Grady Egan - Frederick CO, US
    Lathan Collins - Denver CO, US
  • Assignee:
    Ball Aerospace & Technologies Corp. - Boulder CO
  • International Classification:
    F16M 11/12
    F16F 15/04
    F16C 11/12
    F16C 11/10
  • Abstract:
    Systems and methods for limiting rotation of a supported object about an axis of rotation are provided. A system as disclosed includes a stop system that engages at a selected amount of rotation about an axis of rotation to provide a balanced force countering further rotation. The stop system includes one or more pairs of stop mechanisms, with one stop mechanism in a pair disposed to act from a first side of the axis of rotation, and a second stop mechanism in the pair disposed to act from a second side of the axis of rotation. Each stop mechanism can include stops that engage a flexure at a selected amount of rotation.
  • Cross Flexure Suspension

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  • US Patent:
    20180196257, Jul 12, 2018
  • Filed:
    Jan 3, 2018
  • Appl. No.:
    15/861372
  • Inventors:
    - Boulder CO, US
    Miroslaw A. Ostaszewski - Louisville CO, US
  • International Classification:
    G02B 26/10
    A47G 1/24
    A47G 1/02
    F16M 11/10
    F16F 15/04
    F16M 11/20
    G02B 26/08
  • Abstract:
    Suspension system structures and methods are provided. A system as disclosed allows for rotation of a supported object in two axes, with very little translational movement of the supported object. The system can include a base mounting structure that is joined to an intermediate or connecting structure by a first set of flexure blades. The connecting structure is in turn joined to a supported element structure by a second set of flexure blades. The first set of flexure blades can include four blades that intersect along a line that is coincident with an X axis of rotation, and the second set of flexure blades can include four blades that intersect along a line that is coincident with the Y axis of rotation. The components of the suspension system can comprise a monolithic structure that is formed from a single piece of material.

Resumes

Miroslaw Ostaszewski Photo 1

Staff Consultant

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Location:
139 south Tanager Ct, Louisville, CO
Industry:
Aviation & Aerospace
Work:
Seagate Technology Mar 1995 - Jan 2001
Senior Staff Engineer

Ball Aerospace Mar 1995 - Jan 2001
Staff Consultant

Coherent Technologies May 1994 - Mar 1995
Senior Design Engineer

Ball Aerospace Nov 1988 - May 1994
Senior Design Engineer
Education:
Stevens Institute of Technology 1982 - 1984
Masters, Master of Engineering, Engineering, Mechanical Engineering
Stevens Institute of Technology 1978 - 1982
Bachelor of Engineering, Bachelors, Mechanical Engineering
Skills:
Space Systems
Aerospace
Simulations
Engineering Management
Sensors
Aerospace Engineering
Satellite
Systems Engineering
Systems Design

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