204 resultados para Neural Tube Defects

em Chinese Academy of Sciences Institutional Repositories Grid Portal


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神经管闭合缺陷(NTDs)是一种严重的先天畸形疾病,在新生儿中有千分之一的发病率.神经管融合前后,多种组织参与形态发生运动.神经管一经融合,神经嵴细胞就会向背侧中线方向产生单极突出并向此方向迁移形成神经管的顶部.与此同时,神经管从腹侧开始发生辐射状切入以实现单层化.在此,我们在非洲爪蟾的移植体中机械阻断神经管的闭合以检测其细胞运动及随后的图式形成.结果显示神经管闭合缺陷的移植体不能形成单层化的神经管,并且神经嵴细胞滞留在侧面区域不能向背侧中线迁移,而对神经前体标记基因的检测显示神经管的背腹图式形成并未受到影响.以上结果表明神经管的融合对于辐射状切入和神经嵴细胞向背侧中线方向的迁移过程是必需的,而对于神经管的沿背腹轴方向的图式形成是非必需的.

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Gene duplication is thought to provide raw material for functional divergence and innovation. Fish-specific dmrt2b has been identified as a duplicated gene of the dmrt2a/terra in fish genomes, but its function has remained unclear. Here we reveal that Dmrt2b knockdown zebrafish embryos display a downward tail curvature and have U-shaped somites. Then, we demonstrate that Dmrt2b contributes to a divergent function in somitogenesis through Hedgehog pathway, because Dmrt2b knockdown reduces target gene expression of Hedgehog signaling, and also impairs slow muscle development and neural tube patterning through Hedgehog signaling. Moreover, the Dmrt2b morphants display defects in heart and visceral organ asymmetry, and, some lateral-plate mesoderm (LPM) markers expressed in left side are randomized. Together, these data indicate that fish-specific duplicated dmrt2b contributes to a divergent function in somitogenesis through Hedgehog pathway and maintains the common function for left-right asymmetry establishment.

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神经嵴(neural crest)是一类脊椎动物特有的多潜能迁移细胞。这一类细胞历经“表皮—间充质”转换(EMT),与神经管背侧的其它细胞分离,经由不同路线迁移,定位于胚胎外周各处,后分化为不同的细胞类型包括外周神经系统、颅面骨骼系统及色素细胞等。神经嵴的发育是一个多途径多步骤的过程,受多种信号通路及转录因子调控。这些调控因子相互调节形成精密网络,可被划分为三个主要层次类群:分泌性信号分子(BMP、Wnt、FGF、Delta)、神经板边界特异基因(Msx、Pax3/7、 Zic1、Dlx3/5)、神经嵴特异基因(Snail/Slug、AP-2、FoxD3、Twist、Id、cMyc、Sox9/10)。本文第一章主要概述不同组织来源的各种分泌信号在神经嵴诱导中的作用以及他们之间的整合调控。 Nkx6家族蛋白是一类进化上保守的转录因子,在脊椎动物中枢神经系统(CNS)的图式形成和胰腺的发育中有重要作用。在第二章,我们描述了非洲爪蟾中Nkx6家族基因的克隆及其表达图式。与小鼠和鸡中的同源基因类似,爪蟾的Nkx6家族基因在胚胎发育过程中主要表达于中枢神经系统和前部内胚层组织。其中Nkx6.1和Nkx6.2在神经胚期神经板表达重合,晚期都表达于后脑和脊髓的腹侧。Nkx6.3从卵裂期到神经胚早期都表达于非神经外胚层,而尾芽期表达于后脑后部和腮弓。在内胚层中,Nkx6.2在尾芽期表达于底索。在蝌蚪期,Nkx6家族的三个基因分别表达于前部内胚层的衍生物,包括胰腺、胃、食道和肺。 Nkx6.3是最近发现的Nkx6家族新成员,它在爪蟾中的表达与Nkx6.1和Nkx6.2有了较大分歧。在第三章,我们通过功能获得及功能缺失实验来探讨Nkx6.3在爪蟾早期发育中的功能。我们发现原肠期前过量或抑制Nkx6.3表达都会影响胚胎原肠运动的正常进行。我们通过动物帽延伸实验证明Nkx6.3参与了细胞运动。半定量RT-PCR结果显示,Nkx6.3可以调控一些粘附分子的表达。以上结果说明Nkx6.3通过调控粘附分子的转录而参与细胞运动的调控。我们还发神经嵴(neural crest)是一类脊椎动物特有的多潜能迁移细胞。这一类细胞历经“表皮—间充质”转换(EMT),与神经管背侧的其它细胞分离,经由不同路线迁移,定位于胚胎外周各处,后分化为不同的细胞类型包括外周神经系统、颅面骨骼系统及色素细胞等。神经嵴的发育是一个多途径多步骤的过程,受多种信号通路及转录因子调控。这些调控因子相互调节形成精密网络,可被划分为三个主要层次类群:分泌性信号分子(BMP、Wnt、FGF、Delta)、神经板边界特异基因(Msx、Pax3/7、 Zic1、Dlx3/5)、神经嵴特异基因(Snail/Slug、AP-2、FoxD3、Twist、Id、cMyc、Sox9/10)。本文第一章主要概述不同组织来源的各种分泌信号在神经嵴诱导中的作用以及他们之间的整合调控。 Nkx6家族蛋白是一类进化上保守的转录因子,在脊椎动物中枢神经系统(CNS)的图式形成和胰腺的发育中有重要作用。在第二章,我们描述了非洲爪蟾中Nkx6家族基因的克隆及其表达图式。与小鼠和鸡中的同源基因类似,爪蟾的Nkx6家族基因在胚胎发育过程中主要表达于中枢神经系统和前部内胚层组织。其中Nkx6.1和Nkx6.2在神经胚期神经板表达重合,晚期都表达于后脑和脊髓的腹侧。Nkx6.3从卵裂期到神经胚早期都表达于非神经外胚层,而尾芽期表达于后脑后部和腮弓。在内胚层中,Nkx6.2在尾芽期表达于底索。在蝌蚪期,Nkx6家族的三个基因分别表达于前部内胚层的衍生物,包括胰腺、胃、食道和肺。 Nkx6.3是最近发现的Nkx6家族新成员,它在爪蟾中的表达与Nkx6.1和Nkx6.2有了较大分歧。在第三章,我们通过功能获得及功能缺失实验来探讨Nkx6.3在爪蟾早期发育中的功能。我们发现原肠期前过量或抑制Nkx6.3表达都会影响胚胎原肠运动的正常进行。我们通过动物帽延伸实验证明Nkx6.3参与了细胞运动。半定量RT-PCR结果显示,Nkx6.3可以调控一些粘附分子的表达。以上结果说明Nkx6.3通过调控粘附分子的转录而参与细胞运动的调控。我们还发现,在爪蟾胚胎中Nkx6.3的过表达或抑制表达都导致神经嵴标记基因表达降低。进一步研究发现,32细胞期在不同部位注射Nkx6.3 mRNA可以异位诱导或抑制Slug的表达。动物帽实验显示,Nkx6.3单独过表达可以诱导神经嵴发生,而迄今为止转录因子中只有Snail1具有这一单独诱导能力。在爪蟾胚胎及动物帽中,过表达Nkx6.3都可以诱导Fgf8、Wnt8而抑制BMP4的转录,而且Nkx6.3对这些分泌因子的调控方式是不同的。4细胞期过表达Nkx6.3的胚胎,在促进Fgf8和Wnt8而抑制BMP4的同时,却抑制神经板边界特异基因Msx1、Pax3和神经嵴特异基因Slug的表达,说明Nkx6.3对神经嵴的诱导调控在神经板边界基因层次还存在抑制作用。32细胞过表达Nkx6.3会细胞自主性抑制以及细胞非自主诱导Msx1、Pax3、Slug的表达。Nkx6.3异位诱导Dlx5却抑制Dlx3的表达,说明Dlx5可能是Nkx6.3负调控的直接靶基因。由此,我们提出Nkx6.3的神经嵴诱导调控分为两个层次:分泌信号分子水平的正调控和神经板边界决定水平的负调控。在脊椎动物的神经发生过程中,神经管背腹不同层次形成不同的神经元。这些神经元细胞的命运由背腹起源的多种形态发生素决定。形态发生素通过浓度梯度确定了一组转录因子在神经管背腹不同层次的特异表达,这些基因的组合调控决定了神经前体细胞的命运。然而,这些转录因子是如何解读形态发生素梯度信号的还不是很清楚。第四章,我们通过对神经管腹侧特异表达的转录因子的调控区进行预测,确定了可能调控这些基因表达的保守区段。此外,我们改进了爪蟾转基因操作,并用这一技术确证了Nkx6.2的调控区域。Dbx1、Nkx2.2及Pax6的转录调控区已在小鼠或爪蟾中报道过。由此我们得到了两对在神经管背腹图式中相互作用的转录因子的调控区域:Nkx6.2和Dbx1、Nkx2.2和Pax6。通过对Nkx6.2和Dbx1的调控保守区的转录因子结合位点的预测,我们发现这四个基因以及Wnt信号之间存在大量的相互调控。然而在这两个基因的调控区,我们没有发现Gli的调控位点,暗示这两个基因可能不受Shh的直接调控。我们还克隆了Dbx家族的两个基因,并检测了它们的时空特异性表达,发现Dbx2是母源性表达的,而Dbx1是合子型基因。这两个基因的表达图式相似,都在神经板中线两侧成线状表达,尾芽期在神经管中部表达。过表达Dbx2抑制神经元的初级分化,说明它可能与Dbx1一样具有维持神经板细胞未分化状态的功能。Dbx2的过表达还抑制Nkx6.2及Dbx1的表达,说明它们可能一起参与了神经管腹侧图式的调控。

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Amphioxus Bblhx3 was identified as a LIM-homeobox gene expressed in gastrulae. Structural analysis suggested that it is a member of lhx3 but not of lhx1 gene group. Whole mount in situ hybridization revealed, that expression of Bblhx3 was initiated at the early gastrula stage and continued at least until 10-day larvae. Expression of Bblhx3 first appeared in the vegetal and future dorsal area in initial gastrulae and became restricted to the endoderm during gastrulation. In neurulae and early larvae, Bblhx3 was expressed in the developing neural tube, the notochord and preoral pit lineage. In 10-day larvae, Bblhx3 was expressed only in the preoral pit. This expression pattern is apparently distinct from that of vertebrate lhx3 genes that are not expressed during gastrulation. (C) 2002 Elsevier Science Ireland Ltd. All rights reserved.

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A full length amphioxus cDNA, encoding a novel phosducin-like protein (Amphi-PhLP), was identified for the first time from the gut cDNA library of Branchiostoma belcheri. It is comprised of 1 550 bp and an open reading frame (ORF) of 241 amino acids, with a predicted molecular mass of approximately 28 kDa. In situ hybridization histochemistry revealed a tissue-specific expression pattern of Amphi-PhLP with the high levels in the ovary, and at a lower level in the hind gut and testis, hepatic caecum, gill, endostyle, and epipharyngeal groove, while it was absent in the muscle, neural tube and notochord. In the Chinese Hamster Ovary (CHO) cells transfected with the expression plasmid pEGFP-N1/Amphi-PhLP, the fusion protein was targeted in the cytoplasm of CHO cells, suggesting that Amphi-PhLP is a cytosolic protein. This work may provide a framework for further understanding of the physiological function of Amphi-PhLP in B. belcheri.

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The multi-layers feedforward neural network is used for inversion of material constants of fluid-saturated porous media. The direct analysis of fluid-saturated porous media is carried out with the boundary element method. The dynamic displacement responses obtained from direct analysis for prescribed material parameters constitute the sample sets training neural network. By virtue of the effective L-M training algorithm and the Tikhonov regularization method as well as the GCV method for an appropriate selection of regularization parameter, the inverse mapping from dynamic displacement responses to material constants is performed. Numerical examples demonstrate the validity of the neural network method.

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The ionization kinetics of sodium diluted in argon is studied in a shock tube, in which the test gas mixture is ionized by a reflected shock wave and subsequently quenched by a strong rarefaction wave. A Langmuir electrostatic probe is used to monitor the variation of the ion number density at the reflection shock wave region. The working state of the probe is in the near fi-ee fall region and a correction for reduction of the probe current due to elastic scattering in the probe sheath is introduced. At the temperature range of 800 to 2600 K and in the ambience of argon gas, the three-body recombination rate coefficient of the sodium ion with electron is determined: 3.43 x 10(-14)T(-3.77) cm(6).s(-1).

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针对氢/空气混合物,通过实验研究了其预混火焰在半开口管道中的火焰传播加速现象,结果表明,火焰传播状态随着氢气当量比的变化而发生改变。当氢/空气混合物被点燃后,由于障碍物的扰动,火焰在管道中不断加速传播,并最终到达一准稳态传播。在氢气当量比0.31附近时,火焰速度发生跃变。当氢气当量比足够大时,火焰传播由爆燃态转变为爆轰态。在本实验条件下,爆燃转准爆轰的临界条件是d/Lambda>=2.6(d是圆环形障碍物内径,人是爆轰格胞尺度)。障碍物阻塞比的变化对最大火焰速度和压力提升的影响不明显。

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在应用激光技术加工复杂曲面时,通常以采样点集为插值点来建立曲面函数,然后实现曲面上任意坐标点的精确定位。人工神经网络的BP算法能实现函数插值,但计算精度偏低,往往达不到插值精确要求,造成较大的加工误差。提出人工神经网络的共轭梯度最优化插值新算法,并通过实例仿真,证明了这种曲面精确定位方法的可行性,从而为激光加工的三维精确定位提供了一种良好解决方案。这种方法已经应用在实际中。

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An experimental study and a numerical simulation were conducted to investigate the mechanical and thermodynamic processes involved in the interaction between shock waves and low density foam. The experiment was done in a stainless shock tube (80mm in inner diameter, 10mm in wall thickness and 5360mm in length). The velocities of the incident and reflected compression waves in the foam were measured by using piezo-ceramic pressure sensors. The end-wall peak pressure behind the reflected wave in the foam was measured by using a crystal piezoelectric sensor. It is suggested that the high end-wall pressure may be caused by a rapid contact between the foam and the end-wall surface. Both open-cell and closed-cell foams with different length and density were tested. Through comparing the numerical and experimental end-wall pressure, the permeability coefficients a and 0 are quantitatively determined.

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在一端封闭、一端开口的火焰传播管中均匀布置障碍物,研究了障碍物结构对管道中预混火焰传播的影 响。结果表明,由于障碍物的扰动,火焰不断加速,在阻塞比相同的条件下,最终的火焰稳态速度与障碍物的形状 和间距基本无关,其中障碍物间距仅仅影响火焰的加速速率,在障碍物间距约等于火焰传播管内径( W/ D≈1. 0) 时,平均火焰速度达到最大值,火焰到达稳态传播的距离最短。同时,本文用一维简化模型模拟了火焰在障碍物管 道中的加速过程,计算结果与实验测试结果在定性上比较吻合,说明在管内火焰速度较低的情况下,用一维可压缩 流动近似处理能初步揭示管内火焰的加速机制。

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The performance of combustion driver ignited by multi-spark plugs distributed along axial direction has been analysed and tested. An improved ignition method with three circumferential equidistributed ignitors at main diaphragm has been presented, by which the produced incident shock waves have higher repeatability, and better steadiness in the pressure, temperature and velocity fields of flow behind the incident shock, and thus meets the requirements of aerodynamic experiment. The attachment of a damping section at the end of the driver can eliminate the high reflection pressure produced by detonation wave, and the backward detonation driver can be employed to generate high enthalpy and high density test flow. The incident shock wave produced by this method is well repeated and with weak attenuation. The reflection wave caused by the contracted section at the main diaphragm will weaken the unfavorable effect of rarefaction wave behind the detonation wave, which indicates that the forward detonation driver can be applied in the practice. For incident shock wave of identical strength, the initial pressure of the forward detonation driver is about 1 order of magnitude lower than that of backward detonation.

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Defects induced by plastic deformation in electrodeposited, fully dense nanocrystalline (nc) Ni with an average grain size of 25 nm have been characterized by means of high resolution transmission electron microscopy. The nc Ni was deformed under uniaxial tension at liquid-nitrogen temperature. Trapped full dislocations were observed in the grain interior and near the grain boundaries. In particular, these dislocations preferred to exist in the form of dipoles. Deformation twinning was confirmed in nc grains and the most proficient mechanism is the heterogeneous nucleation via emission of partial dislocations from the grain boundaries.

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A numerical study on wave dynamic processes occurring in muzzle blast flows, which are created by a supersonic projectile released from the open-end of a shock tube into ambient air, is described in this paper. The Euler equations, assuming axisymmetric flows, are solved by using a dispersion-controlled scheme implemented with moving boundary conditions. Three test cases are simulated for examining friction effects on the muzzle flow. From numerical simulations, the wave dynamic processes, including two blast waves, two jet flows, the bow shock wave and their interactions in the muzzle blasts, are demonstrated and discussed in detail. The study shows that the major wave dynamic processes developing in the muzzle flow remain similar when the friction varies, but some wave processes, such as shock-shock interactions, shock-jet interactions and the contact surface instability, get more intensive, which result in more complex muzzle blast flows.

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The high-speed combustible gas ignited by a hot gas jet, which is induced by shock focusing, was experimentally investigated. By use of the separation mode of shock tube, the test section of a single shock tube is split into two parts, which provide the high-speed flow of combustible gas and pilot flame of hot gas jet, respectively. In the interface of two parts of test sections the flame of jet was formed and spread to the high-speed combustible gas. Two kinds of the ignitions, 3-D “line-flame ignition” and 2-D “plane-flame ignition”, were investigated. In the condition of 3-D “lineflame ignition” of combustion, thicker hot gas jet than pure air jet, was observed in schlieren photos. In the condition of 2-D “plane-flame ignition” of combustion, the delay time of ignition and the angle of flame front in schlieren photos were measured, from which the velocity of flame propagation in the high-speed combustible gas is estimated in the range of 30–90 m/s and the delay time of ignition is estimated in the range of 0.12–0.29 ms.