MICHAEL STANLEY CIESIELSKI, II
Pilots at Kirk Ave, Marple Township, PA

License number
Pennsylvania C1060263
Category
Airmen
Address
Address
2626 Kirk Ave, Marple Township, PA 19008

Professional information

Michael Ciesielski Photo 1

Vehicle Arresting Bed Systems

US Patent:
6726400, Apr 27, 2004
Filed:
May 19, 2000
Appl. No.:
09/574865
Inventors:
Richard D. Angley - Aston PA
Michael S. Ciesielski - Broomall PA
Christopher T. Dial - Lansdowne PA
Peter T. Mahal - Ardmore PA
Robert F. Cook - Chipley FL
Assignee:
Engineered Arresting Systems Corporation - Aston PA
International Classification:
E01C 500
US Classification:
404 27, 404 29, 404 71
Abstract:
Vehicle arresting beds, for installation at the ends of aircraft runways, are effective to safely decelerate aircraft entering the bed. The arresting bed is assembled of a large number of blocks of cellular concrete having predetermined compressive gradient strength, so that aircraft landing gear is subjected to drag forces effective to slow a variety of types of aircraft, while providing deceleration within a safe range of values. An arresting bed typically includes an entry region of a depth increasing from 9 to 24 inches formed of blocks having a first compressive gradient strength. A second region, which may be tapered into the first region and increase in depth to 30 inches, is formed of blocks having a greater compressive gradient strength. An aircraft thus experiences increasing drag forces while it travels through the bed, to provide an arresting capability suitable for a variety of aircraft. Arresting bed systems may include composite blocks including portions of cellular concrete of different strengths, reinforced blocks including a lower layer or grid of higher strength material, and cellular concrete block edge members surrounding a bed of aggregate or poured in place cellular concrete.


Michael Ciesielski Photo 2

Vehicle Arresting Unit Fabrication Methods

US Patent:
5902068, May 11, 1999
Filed:
Feb 7, 1997
Appl. No.:
8/796969
Inventors:
Richard D. Angley - Aston PA
Michael S. Ciesielski - Broomall PA
Christopher T. Dial - Lansdowne PA
Peter T. Mahal - Ardmore PA
Assignee:
Datron, Inc. - Garland TX
International Classification:
C04B7/02
US Classification:
404 34
Abstract:
Vehicle arresting blocks of cellular concrete are usable to safely slow travel of an object and may be used to construct an aircraft arresting bed at the end of an airport runway. For such purposes, cellular concrete blocks must be fabricated to exhibit compressive gradient strengths of predetermined values to provide sufficient, but not excessive, deceleration forces on an object. Material uniformity characteristics must be met to avoid unacceptable drag force variations, so that arresting blocks desirably exhibit a predetermined compressive gradient strength (e. g. , a 60/80 CGS) over a depth of penetration of 10 to 66 percent of block thickness. A 60/80 CGS will typically represent an average compressive strength of 70 pounds per square inch over such depth of penetration. Prior applications of cellular concrete typically involved meeting minimum strength values and the production methods did not meet uniformity or compressive gradient strength predictability as required for arresting blocks. Described methods include parameter, ingredient and process controls and ranges effective to enable fabrication of arresting blocks having dry densities and compressive gradient strengths which can be specified in order to provide limited deceleration of aircraft and other objects.


Michael Ciesielski Photo 3

Vehicle Arresting Bed Systems

US Patent:
5885025, Mar 23, 1999
Filed:
Feb 7, 1997
Appl. No.:
8/796970
Inventors:
Richard D. Angley - Aston PA
Michael S. Ciesielski - Broomall PA
Christopher T. Dial - Lansdowne PA
Peter T. Mahal - Ardmore PA
Robert F. Cook - Chipley FL
Assignee:
Datron Inc. - Garland TX
International Classification:
E01F 1500
US Classification:
404 27
Abstract:
Vehicle arresting beds, for installation at the ends of aircraft runways, are effective to safely decelerate aircraft entering the bed. The arresting bed is assembled of a large number of blocks of cellular concrete having predetermined compressive gradient strength, so that aircraft landing gear is subjected to drag forces effective to slow a variety of types of aircraft, while providing deceleration within a safe range of values. An arresting bed typically includes an entry region of a depth increasing from 9 to 24 inches formed of blocks having a first compressive gradient strength. A second region, which may be tapered into the first region and increase in depth to 30 inches, is formed of blocks having a greater compressive gradient strength. An aircraft thus experiences increasing drag forces while it travels through the bed, to provide an arresting capability suitable for a variety of aircraft. A protective hardcoat layer of cellular concrete of strength greater than the blocks overlays the blocks to enable service personnel to walk on the bed without damage.


Michael Ciesielski Photo 4

Arresting Material Test Apparatus And Methods

US Patent:
5789681, Aug 4, 1998
Filed:
Feb 7, 1997
Appl. No.:
8/796968
Inventors:
Richard D. Angley - Aston PA
Michael S. Ciesielski - Broomall PA
Christopher T. Dial - Lansdowne PA
Peter T. Mahal - Ardmore PA
Robert F. Cook - Chipley FL
Assignee:
Datron Inc. - Garland TX
International Classification:
G01N 300
US Classification:
73803
Abstract:
Arresting material test apparatus, test probes and test methods enable testing of compressive gradient strength of cellular concrete, and materials having similar characteristics, on a continuous basis from the surface of a section to a typical internal penetration depth of at least 60 percent of thickness. Previous testing of cellular concrete typically focused on testing to confirm a minimum structural strength prior to structural failure or shattering of a test sample. For an aircraft arresting bed, for example, cellular concrete must exhibit a compressive gradient strength in a relatively narrow precalculated range continuously from the surface to penetration depth equal to 60 to 80 percent of sample thickness. Precalculated and controlled compressive gradient strength is critical to enabling an aircraft to be safely stopped within a set distance, without giving rise to drag forces exceeding main landing gear structural limits. New test apparatus, test probes with post-compression build-up relief and test methods are described to enable such testing and recordation of data showing the gradient of compressive strength as it increases from the surface of a test sample to a predetermined depth of penetration.