• Title/Summary/Keyword: Jet injection

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The feasibility of needleless jet injection versus conventional needle local anesthesia during dental procedures: a systematic review

  • Alreem Ahmed, Alameeri;Hessa AlFandi, AlShamsi;Amel, Murad;Mariam Mahmoud, Alhammadi;Meznah Hamad, Alketbi;Arwa, AlHamwi;Natheer Hashim Al, Rawi;Sausan Al, Kawas;Marwan Mansoor, Mohammed;Shishir Ram, Shetty
    • Journal of the Korean Association of Oral and Maxillofacial Surgeons
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    • v.48 no.6
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    • pp.331-341
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    • 2022
  • This systematic review evaluates current evidence regarding the feasibility of using needleless jet injection instead of a conventional local anesthetic needle. EBSCO, ProQuest, PubMed, and Scopus databases were used to identify relevant literature published in English from 2005 to 2020. Ten studies were selected. Five of them were randomized clinical trials, 3 case-control studies, and 2 equivalence trials. Using the Critical Appraisal Skills Program checklist, 6 studies scored between 67% and 100%, and 4 studies scored between 34% and 66%. According to Jadad's scale, 2 studies were considered strong, and 8 studies were considered moderate in quality. The results of the 10 studies showed differences in patient preference for needleless jet injection. Needleless injection technique has been found to be particularly useful in uncooperative patients with anxiety and needle phobia. Needleless jet injection is not technique sensitive. However, with needleless jet anesthesia, most treatments require additional anesthesia. Conventional needle anesthesia is less costly, has a longer duration of action, and has better pain control during dental extraction. Needleless jet anesthesia has been shown to be moderately accepted by patients with a fear of needles, has a faster onset of action, and is an efficient alternative to conventional infiltration anesthesia technique.

The Effect of Combustion Chamber Shape on the Performance of Swirl Chamber in Diesel Engine (I) (와류실식 소형 디젤 기관의 연소실 형상이 기관 성능에 미치는 영향(I))

  • Ra, J.H.;Ahn, S.K.
    • Journal of Power System Engineering
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    • v.2 no.2
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    • pp.27-34
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    • 1998
  • The purpose of this study is to investigate the performance of swirl combustion chamber diesel engine by changing the jet passage area and its angle, the depth and shape of the piston top cavity(main chamber). The performance of diesel engine with newly changed swirl combustion chamber was tested through the experimental conditions as engine speed, load and injection timing etc. The test results were compared and analyzed. The rate of fuel consumption was affected significantly by the jet passage area at the high speed and load, by the depth of the piston top cavity at the low speed and load. The exhaust smoke density and exhaust gas temperature depended sensitively on variation of the injection timing rather than the shape of the combustion chamber within the experimental conditions.

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Study on the Surface Heat Transfer Around a Circular Secondary Jet in the Supersonic Flow (초음속 유동내 원형 2차분사 제트 주변에서의 표면 열전달 현상 연구)

  • Yi, Jong-Ju;Yu, Man-Sun;Cho, Hyung-Hee
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.2
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    • pp.47-53
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    • 2007
  • Convective heat transfer coefficient was measured around a circular secondary jet ejected into the supersonic flow field. The wall temperature measurement around a injection nozzle was conducted using infra-red camera. The constant heat flux is applied to the wall around a secondary nozzle. According to jet to freestream momentum ratio, the injection flow penetrates into the supersonic flow field. The measured temperature is used to calculate the convective heat transfer coefficient.

Simulation study on porosity disturbance of ultra-large-diameter jet borehole excavation based on water jet coal wetting and softening model

  • Guo, Yan L.;Liu, Hai B.;Chen, Jian;Guo, Li W.;Li, Hao M.
    • Geomechanics and Engineering
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    • v.30 no.2
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    • pp.153-167
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    • 2022
  • This study proposes a method to analyze the distribution of coal porosity disturbances after the excavation of ultra-large-diameter water jet boreholes using a coal wetting and softening model. The high-pressure jet is regarded as a short-term high-pressure water injection process. The water injection range is the coal softening range. The time when the reference point of the borehole wall is shocked by the high-pressure water column is equivalent to the time of high-pressure water injection of the coal wall. The influence of roadway excavation with support and borehole diameter on the ultra-large-diameter jet drilling excavation is also studied. The coal core around the borehole is used to measure the gas permeability for determining the porosity disturbance distribution of the coal in the sampling plane to verify the correctness of the simulation results. Results show that the excavation borehole is beneficial to the expansion of the roadway excavation disturbance, and the expansion distance of the roadway excavation disturbance has a quadratic relationship with the borehole diameter. Wetting and softening of the coal around the borehole wall will promote the uniform distribution of the overall porosity disturbance and reduce the amplitude of disturbance fluctuations.

An Experimental Study of Coanda Effect on the Flapped Control Surfaces (콴다효과를 응용한 플랩이 달린 고양력 날개장치에 대한 실험적 연구)

  • 안해성;김효철
    • Journal of the Society of Naval Architects of Korea
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    • v.40 no.5
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    • pp.10-16
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    • 2003
  • To investigate the jet effect on circulation control, a segment of model was prepared and inserted horizontally across the test section of the cavitation tunnel. The hydrodynamic forces acting on the model were measured under the 2 dimensional flow behavior. Circulation flow control requires higher flow rate of water jet than boundary layer control does. Jet injection is effective in increasing lift coefficient and the increments reach to 160% in a certain combination of parameters such as an angle of attack, jet flow rate and flap angle. The blown water jet not only reduces form drag but also thrust effect, which is sometimes greater than the form drag in specific conditions.

The Enhacned Atomization of Single Hole Nozzle by Cavitation at The Low Pressure Injection (저압 분사시 캐비테이션에 의한 단공 노즐의 미립화 향상)

  • Son, Jong-Won;Cha, Keun-Jong;Kim, Duck-Jool
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.952-957
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    • 2001
  • The objectives of this investigation were to obtain an excellent spray by cavitation under the low injection pressure. When cavitation occurs in the nozzle hole, the atomization of the liquid jet enhanced considerably. In this experiments, a acrylic nozzle made the gap and installed the bypass in the nozzle hole was used to enhance the atomization of the liquid jet at the low injection pressure. The liquid flow in the nozzle hole was photographed by a transmitted light using a micro flash. The spray angle was measured macroscope images of PMAS and the Sauter mean diameter was measured PDA system. To measure the pressure of the nozzle hole, pressure transducer was used. The results of this study indicated that enhanced atomization of the liquid jet at the low injection pressure was obtained by making the gap and installing the bypass at the single hole nozzle.

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Theoretical Model of Coaxial Twin-Fluid Spray In a Liquid Rocket Combustor (연소실 내 동축형 2-유체 분무의 이론적 모델)

  • 조용호;윤웅섭
    • Journal of the Korean Society of Propulsion Engineers
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    • v.6 no.2
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    • pp.37-44
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    • 2002
  • A theoretical study of spray and combustion characteristics due to coaxial twin-fluid injection is conducted to investigate the effects of liquid jet property, droplet size, contact length and liquid jet velocity. Model is properly validated with measurements and shows good agreement. Prediction of jet contact length, droplet size, liquid jet velocity reflects genuine features of coaxial injection in physical and practical aspects. Both the jet contact length and tile droplet size are reduced in a linear manner with an increase of injector diameter. Cross sectional area of liquid intact core is reduced with augmented jet splitting rate, thus the jet is accelerated to maintain the mass continuity and with an assistant of momentum diffusion by burnt gas.

Comparison of Supersonic Jet Characteristics between Hydrogen and Helium injected by Small-cone-angle Pintle-type Hydrogen Injector (수소 및 헬륨을 이용한 작은 원추각 핀틀형 수소인젝터의 초음속 제트 특성 비교)

  • Gyuhan Bae;Juwan Lim;Jaehyun Lee;Seoksu Moon
    • Journal of ILASS-Korea
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    • v.29 no.2
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    • pp.83-90
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    • 2024
  • Understanding the fundamental characteristics of supersonic hydrogen jets is important for the optimization of combustion in hydrogen engines. Previous studies have used helium as a surrogate gas to characterize the hydrogen jet characteristics due to potential explosion risks of hydrogen. It was based on the similarity of hydrogen and helium jet structures in supersonic conditions that has been confirmed using hole-type injectors and large-cone-angle pintle-type injectors. However, the validity of using helium as a surrogate gas has not been examined for recent small-cone-angle pintle-type injectors applied to direct-injection hydrogen engines, which form a supersonic hollow cone near the nozzle and experience the jet collapse downstream. Differences in the physical properties of hydrogen and helium could alter the jet development characteristics that need to be investigated and understood. This study compares supersonic jet structures of hydrogen and helium injected by a small-cone-angle (50°) pintle-type hydrogen injector and discusses their differences and related mechanisms. Jet penetration length and dispersion angle are measured using the Schlieren imaging method under engine-like injection conditions. As a result, the penetration length of hydrogen and helium jets showed a slight difference of less than 5%, and the dispersion angle showed a maximum of 10% difference according to the injection condition.

Study of Spray Droplet/Wall Interaction (분무액적과 벽의 상호작용에 대한 연구)

  • 양희천;유홍선;정연태
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.4
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    • pp.86-100
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    • 1998
  • The impingement of the fuel spray on the wall within the combustion chamber in compact high-pressure injection engines and on the intake port wall in port-fuel-inje- ction type engines is unavoidable. It is important to understand the characteristics of impinging spray because it influences on the rate of fuel evaporation and droplet distrib- ution etc. In this study, the numerical study for the characteristics of spray/wall interaction is performed to test the applicability and reliability of spray/wall impingement models. The impingement models used are stick model, reflect model, jet model and Watkins and Park's model. The head of wall-jet eminating radilly outward from the spray impingement site contains a vortex. Small droplets are deflected away from the wall by the stagnation flow field and the gas wall-jet flow. While the larger droplets with correspondingly higher momentum are impinged on the wall surface and them are moved along the wall and are rolled up by wall-jet vortex. Using the Watkins and Park's model the predicted results show the most reasonable trend. The rate of increase of spread and the height of the developing wall-spray is predicted to decrease with increased ambient pressure(gas density).

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