Fatigue Degradation of the Structure of Parachute Systems

• Autorzy: Szafran K. , Kramarski I.

Identyfikatory

DOI

10.2478/fas-2018-0009

• Języki publikacji: EN

Abstrakty

EN

Parachute systems are in widespread use in aviation. Up to now, parachutes are the most uncertain air vehicles because of their complex and unsteady opening characteristics, changes in geometry up to 30% and vulnerability from unsteady atmospheric turbulence. Fatigue is a problem that the designers of long living parachute systems need to cope with. Authors demonstrate complexity of parachute exploitation and means to lower opening forces and extend service life without influencing safety.

Słowa kluczowe

EN

parachute systems; fatigue degradation; aviation safety system

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Fatigue of Aircraft Structures
• Rocznik: 2018
• Tom: Iss. 10
• Strony: 93--103
• Opis fizyczny: Bibliogr. 11 poz., rys., wykr.

Twórcy

autor

Szafran K.

• Institute of Aviation, Warsaw, Poland

autor

Kramarski I.

• HORNET, Nowy Dwór Mazowiecki, Poland

Bibliografia

• [1] Peterson, C. W., Strickland, J. H., Higuchi, H, 1996 “The Fluid Dynamics of Parachute Inflation, Annual Review of Fluid Mechanics, Volume 28 (1) - Jan 1.
• [2] Szafran K., Kramarski I. 2015 “Safety of Navigation on the Approaches to the Ports of the Republic of Poland on the Basis of the Radar System on the Aerostat Platform”. Trans Nav the International Journal on Marine Navigation and Safety of Sea Transportation. ISSN 2083-6473 vol. 9 nr 1 pp. 131-136.
• [3] http://blog.performancedesigns.com/know-your-lines-part-3-when-do-you-need-a-reline/
• [4] Nelsen, J. M., Computational fluid dynamic studies of a solid and ribbon 12-gore parachute canopy in subsonic and supersonic flow. 13th AIAA Aerodynamic Decelerator Systems Technology Conference, AIAA Paper 95-1558
• [5] Parachute Handling vs Porosity (https://www.hpac.ca/pub/?pid=158)
• [6] PIA Position On A 180 Day Repack Cycle http://www.pia.com/piapubs/pia_position_on_a_180_day_repack.htm
• [7] Knacke, T., W., Parachute Recovery Systems Design Manual, 1991
• [8] SIGMA Tandem System Owner’s Manual (http://unitedparachutetechnologies.com/PDF/Support/Manual/Manual_Sigma_MAN-013.pdf?Name=Value)
• [9] Szafran K., Pągowski Z. T. & Kramarski I. 2015 „Badania symulacyjne elementów konstrukcyjnych modułowego napędu platformy badawczej”. Trans Comp 2015, TTS - ISSN 1232-3829 12/2015 pp. 234-241
• [10] Kasyanov V. A., Szafran K., Goncharenko A., Shipitiak T. „Entropy Paradigm in the theory of Hierarchical Active Systems. Elements of Conflict Theory”. Transaction of the Institute of Aviation. № 5-6 (232-233). - pp. 115-128. 2013
• [11] Szafran K., Kończak J., M. Mieteń 2017„Impact of the decision on transport systems’ reliability in emergency situations”. DOI: 10.5604/01.3001.0010.7230, JOURNAL OF SCIENCE OF THE MILITARY ACADEMY OF LAND FORCES. Volume 49 Number 4(186)

Uwagi

PL

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2019).