Objective： To explore the effect and mechanism of ginsenoside Rg3 （Shenyi Capsule, 参一胶囊） on the postoperative life span of patients with non-small cell lung cancer （NSCLC）. Methods： The prospective, randomiz...Objective： To explore the effect and mechanism of ginsenoside Rg3 （Shenyi Capsule, 参一胶囊） on the postoperative life span of patients with non-small cell lung cancer （NSCLC）. Methods： The prospective, randomized, controlled method was adopted. One hundred and thirty- three patients with NSCLC were randomly assigned to 3 groups： Shenyi Capsule group （43 cases）, combined therapy group （Shenyi Capsule plus chemotherapy, 46 cases）, and chemotherapy group （44 cases）. The survival rates, immune function and the correlation between vascular endothelial growth factor （VEGF） expression and clinical effect were analyzed in the three groups. Results： （1） The 1-year survival rate in the Shenyi group, the combined group and the chemotherapy group was 76.7% （33/43）, 82.6% （38/46）, and 79.5% （35/44）, respectively; the 2-year survival rate was 67.4% （29/43）, 71.7% （33/46）, and 70.5% （31/44）, respectively; and the 3-year survival rate was 46.5% （20/43）, 54.3% （25/46）, and 47.7% （21/44）, respectively. There was no significant difference among the 3 groups （P〉0.05）. （2） NK cells were increased to different degrees and the ratio of CD4/CD8 was normal in the Shenyi Capsule group and the combined group, while the ratio of CD4/CD8 was disproportional in the chemotherapy group. （3） In the chemotherapy group, the 3-year survival rate was lower in patients with positive expression of VEGF than in patients with negative expression （37.0% vs 64.7%, χ^2=17.9, P〈0.01）, but no significant statistical difference was shown in the other two groups （53.6% vs 55.6%, P〉0.05; 44.4% vs 50.0%, P〉0.05）. Conclusion： Shenyi Capsule, especially in combination with chemotherapy, can improve the life span of patients with NSCLC after operation. The mechanism might be correlated with improving the immune function and anti-tumor angiogenesis.展开更多
The reverse microemulsion system of Span 80-Tw ee n 80/liquid paraffin/acrylamide-H 2O was prepared, and the effects of n-b utanol,NaCl,Nc were studied with the conductivity method.The stability of re verse microemuls...The reverse microemulsion system of Span 80-Tw ee n 80/liquid paraffin/acrylamide-H 2O was prepared, and the effects of n-b utanol,NaCl,Nc were studied with the conductivity method.The stability of re verse microemulsion was reflected, and the information of its dynamic process wa s obtained by measuring its state changes continuously through testing its elect ronic conductivity by using electrochemistry.The results showed that the Span 80 -Tween 80/liquid paraffin/acrylamide-H 2O system was most stable when the HLB value approached 7.5, and its stability was enhanced when 5.0% (mass) NaCl or 10% (mass) Nc was added into this system.展开更多
The morphing technology of hypersonic vehicle improved the flight performance by changing aerodynamic characteristics with shape deformations,but the design of guidance and control system with morphing laws remained t...The morphing technology of hypersonic vehicle improved the flight performance by changing aerodynamic characteristics with shape deformations,but the design of guidance and control system with morphing laws remained to be explored.An Integrated of Guidance,Control and Morphing(IGCM)method for Hypersonic Morphing Vehicle(HMV)was developed in this paper.The IGCM method contributed to an effective solution of morphing characteristic to improve flight performance and reject the disturbance for guidance and control system caused by the morphing system for HMV in gliding phase.The IGCM models were established based on the motion models and aerodynamic models of the variable span vehicle.Then the IGCM method was designed by adaptive block dynamic surface back-stepping method with stability proof.The parallel controlled simulations’results showed the effectiveness in accomplishing the flight mission of IGCM method in glide phase with smaller terminal errors.The velocity loss of HMV was reduced by 32.8%which inferred less flight time and larger terminal flight velocity than invariable span vehicle.Under the condition of large deviations of aerodynamic parameters and atmospheric density,the robustness of IGCM method with variable span was verified.展开更多
In this work, a simulated aircraft fuel tank inerting system has been successfully estab- lished based on a model tank. Experiments were conducted to investigate the influences of different operating parameters on the...In this work, a simulated aircraft fuel tank inerting system has been successfully estab- lished based on a model tank. Experiments were conducted to investigate the influences of different operating parameters on the inerting effectiveness of the system, including flow rate of the inert gas （nitrogen-enriched air）, inert gas concentration, fuel load of the tank and different inerting approaches. The experimental results show that under the same operating conditions, the time span of a complete inerting process decreased as the flow rate of inert gas was increased; the time span using the inert gas with 5% oxygen concentration was much longer than that using pure nitrogen; when the fuel tank was inerted using the ullage washing approach, the time span increased as the fuel load was decreased; the ullage washing approach showed the best inerting performance when the time span of a complete inerting process was the evaluation criterion, but when the decrease of dissolved oxygen concentration in the fuel was also considered to characterize the inerting effective- ness, the approach of ullage washing and fuel scrubbing at the same time was the most effective.展开更多
文摘Objective： To explore the effect and mechanism of ginsenoside Rg3 （Shenyi Capsule, 参一胶囊） on the postoperative life span of patients with non-small cell lung cancer （NSCLC）. Methods： The prospective, randomized, controlled method was adopted. One hundred and thirty- three patients with NSCLC were randomly assigned to 3 groups： Shenyi Capsule group （43 cases）, combined therapy group （Shenyi Capsule plus chemotherapy, 46 cases）, and chemotherapy group （44 cases）. The survival rates, immune function and the correlation between vascular endothelial growth factor （VEGF） expression and clinical effect were analyzed in the three groups. Results： （1） The 1-year survival rate in the Shenyi group, the combined group and the chemotherapy group was 76.7% （33/43）, 82.6% （38/46）, and 79.5% （35/44）, respectively; the 2-year survival rate was 67.4% （29/43）, 71.7% （33/46）, and 70.5% （31/44）, respectively; and the 3-year survival rate was 46.5% （20/43）, 54.3% （25/46）, and 47.7% （21/44）, respectively. There was no significant difference among the 3 groups （P〉0.05）. （2） NK cells were increased to different degrees and the ratio of CD4/CD8 was normal in the Shenyi Capsule group and the combined group, while the ratio of CD4/CD8 was disproportional in the chemotherapy group. （3） In the chemotherapy group, the 3-year survival rate was lower in patients with positive expression of VEGF than in patients with negative expression （37.0% vs 64.7%, χ^2=17.9, P〈0.01）, but no significant statistical difference was shown in the other two groups （53.6% vs 55.6%, P〉0.05; 44.4% vs 50.0%, P〉0.05）. Conclusion： Shenyi Capsule, especially in combination with chemotherapy, can improve the life span of patients with NSCLC after operation. The mechanism might be correlated with improving the immune function and anti-tumor angiogenesis.
文摘The reverse microemulsion system of Span 80-Tw ee n 80/liquid paraffin/acrylamide-H 2O was prepared, and the effects of n-b utanol,NaCl,Nc were studied with the conductivity method.The stability of re verse microemulsion was reflected, and the information of its dynamic process wa s obtained by measuring its state changes continuously through testing its elect ronic conductivity by using electrochemistry.The results showed that the Span 80 -Tween 80/liquid paraffin/acrylamide-H 2O system was most stable when the HLB value approached 7.5, and its stability was enhanced when 5.0% (mass) NaCl or 10% (mass) Nc was added into this system.
文摘The morphing technology of hypersonic vehicle improved the flight performance by changing aerodynamic characteristics with shape deformations,but the design of guidance and control system with morphing laws remained to be explored.An Integrated of Guidance,Control and Morphing(IGCM)method for Hypersonic Morphing Vehicle(HMV)was developed in this paper.The IGCM method contributed to an effective solution of morphing characteristic to improve flight performance and reject the disturbance for guidance and control system caused by the morphing system for HMV in gliding phase.The IGCM models were established based on the motion models and aerodynamic models of the variable span vehicle.Then the IGCM method was designed by adaptive block dynamic surface back-stepping method with stability proof.The parallel controlled simulations’results showed the effectiveness in accomplishing the flight mission of IGCM method in glide phase with smaller terminal errors.The velocity loss of HMV was reduced by 32.8%which inferred less flight time and larger terminal flight velocity than invariable span vehicle.Under the condition of large deviations of aerodynamic parameters and atmospheric density,the robustness of IGCM method with variable span was verified.
文摘In this work, a simulated aircraft fuel tank inerting system has been successfully estab- lished based on a model tank. Experiments were conducted to investigate the influences of different operating parameters on the inerting effectiveness of the system, including flow rate of the inert gas （nitrogen-enriched air）, inert gas concentration, fuel load of the tank and different inerting approaches. The experimental results show that under the same operating conditions, the time span of a complete inerting process decreased as the flow rate of inert gas was increased; the time span using the inert gas with 5% oxygen concentration was much longer than that using pure nitrogen; when the fuel tank was inerted using the ullage washing approach, the time span increased as the fuel load was decreased; the ullage washing approach showed the best inerting performance when the time span of a complete inerting process was the evaluation criterion, but when the decrease of dissolved oxygen concentration in the fuel was also considered to characterize the inerting effective- ness, the approach of ullage washing and fuel scrubbing at the same time was the most effective.
