首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Investigations of gas and particle dynamics in first generation needle-free drug delivery devices
Authors:NJ Quinlan  MAF Kendall  BJ Bellhouse  RW Ainsworth
Institution:(1) PowderJect Centre for Gene and Drug Delivery Research, University of Oxford, Oxford OX2 6PE, UK , GB;(2) Department of Engineering Science, University of Oxford, Oxford OX1 3PJ, UK , GB
Abstract:Abstract. Transdermal powdered drug delivery involves the propulsion of solid drug particles into the skin by means of high-speed gas-particle flow. The fluid dynamics of this technology have been investigated in devices consisting of a convergent-divergent nozzle located downstream of a bursting membrane, which serves both to initiate gas flow (functioning as the diaphragm of a shock tube) and to retain the drug particles before actuation. Pressure surveys of flow in devices with contoured nozzles of relatively low exit-to-throat area ratio and a conical nozzle of higher area ratio have indicated a starting process of approximately 200 s typical duration, followed by a quasi-steady supersonic flow. The velocity of drug particles exiting the contoured nozzles was measured at up to 1050 m/s, indicating that particle acceleration took place primarily in the quasi-steady flow. In the conical nozzle, which had larger exit area ratio, the quasi-steady nozzle flow was found to be overexpanded, resulting in a shock system within the nozzle. Particles were typically delivered by these nozzles at 400 m/s, suggesting that the starting process and the quasi-steady shock processed flow are both responsible for acceleration of the particle payload. The larger exit area of the conical nozzle tested enables drug delivery over a larger target disc, which may be advantageous. Received 12 March 2000 / Accepted 8 June 2000
Keywords:: Needle-free drug delivery  Transdermal powdered drug delivery  Powder injection  Biolistics  Supersonic nozzle            Shock tube  Doppler global velocimetry
本文献已被 SpringerLink 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号