青冈林土壤跳虫群落结构在落叶分解过程中的变化

1993年5月至1995年4月,用落叶代法研究青冈（Cyclobalanopsis glauca）落叶分解过程中跳虫的群落结构变化。用多样性指数、演替指数、相似系数分析跳虫在落叶分解过程中群落结构及其季节变化特点。青冈落叶分解经淋洗、养分固定 养分活化3个阶段,分解常数分别为k1=9.11,k2=2.57,k3=0.43（百分比／月）。跳中心在落叶分解过程中的集聚型分为3组：A组为落叶分解前期集聚的种类,B组为后期的种类,C组为中期或全过程的种类,分析讨论了落叶分解过程与跳虫功能群及群落结构变化的关系。     

三峡库区多年高水位运行对消落带狗牙根生长恢复的影响

为深入了解三峡库区多年高水位运行对消落带优势植物生长恢复的影响,分别于2008年和2017年定量调研了库区长寿段消落带狗牙根(Cynodon dactylon)种群的变化,探讨了库区高水位运行对消落带狗牙根萌发、生长和物质分配的影响。结果表明,多年的高水位运行导致不定芽形成和萌发显著被促进,形成更多的分株;高水位运行导致狗牙根分株的株高、茎宽和叶片数被显著抑制,而叶长和种群的总叶片数被显著促进,且随着消落带水位的降低叶长呈降低趋势,而叶宽和总叶片数呈增加趋势;高水位运行导致狗牙根种群匍匐茎和地下茎的茎长、茎节数和总茎长均被显著促进,且随着消落带水位降低匍匐茎茎长和茎节数呈显著的降低趋势,而地下茎茎长和茎节数呈增加趋势;高水位运行导致狗牙根地下茎储存的干质量呈增加趋势,而分株和匍匐茎的干质量呈降低趋势,而且在种群物质分配中地下茎所占的比例呈增大趋势,低水位狗牙根种群的分株和高水位种群的匍匐茎所占的比例也呈增加趋势。因此,狗牙根不仅具有很强的耐淹和生长恢复能力,也具有很强的拓殖能力,可以作为库区中低位消落带恢复和重建的主要原生物种。     

不同光质对烟草叶片组织结构及Rubisco羧化酶活性和rbc、rca基因表达的影响

通过对烟草植株覆盖白、红、黄、蓝、紫色滤膜获得不同光质,研究了烟草叶片在7～70d的生长发育期内,不同光质处理对烟叶组织结构特征、核酮糖1,5-二磷酸羧化酶/加氧酶（Rubisco）羧化酶活性、Rubisco基因（rbc）表达及其活化酶（Rca）基因（rca）表达的影响。结果表明,与黄膜处理下生长的烟叶相比,红、蓝、紫膜处理下生长的烟叶有较高的叶片厚度、栅栏组织厚度、海绵组织厚度、栅栏细胞密度和较小的组织空隙率。此外,红、蓝、紫膜处理的叶片有较高的Rubis-co羧化酶活性和净光合速率及较强的rbc和rca基因表达。实验结果表明不同光质对烟草叶片的组织结构特征有显著影响,光质可能通过影响Rubisco羧化酶活性进而影响叶片光合效率,而光质、叶片组织结构和光合效率之间存在某种程度的相互联系。     

金环蛇神经毒素与乙酰胆碱受体结合的特点

进一步纯化了前一工作中从广西省产金环蛇(Bungarus fasciatus)蛇毒分离的突触后毒素Ⅰ和Ⅱ。以超饱和剂量的毒素Ⅰ或Ⅱ先与从电鳐(Narcine maculata)电器官得到的乙酰胆碱受体(AChR)保温10min 或 lh,再加入~(125)Ⅰ-标记α-银环蛇毒素或~(125)Ⅰ-标记眼镜蛇毒素,继续保温10min 或 lh,由测定与 AChR 结合的放射性强度得知,如以未经毒素Ⅰ或Ⅱ预饱和的放射性强度为100%,则经与其一预饱和者的约为30%,即毒素Ⅰ或Ⅱ只竞争地阻遏了α-银环蛇毒素或眼镜蛇毒素与 AChR 结合能力的2/3左右。文中讨论了存在两种类型 AChR 的可能性。     

白及小分子热激蛋白BsHsp17.3基因的克隆与表达分析

为了探索人工栽培白及的适宜条件,该研究以湖北省十堰市野生白及为对象,采用同源克隆和3'RACE技术,从白及(Bletilla striata)中获得与热激蛋白合成有关的BsHsp17.3基因,并分析BsHsp17.3基因对不同胁迫的响应。结果表明:BsHsp17.3基因开放阅读框长度为453 bp,编码150个氨基酸;蛋白的分子量为17.42 kD,等电点为6.33。进化树分析表明BsHSP17.3蛋白与同为兰科的铁皮石斛进化关系较近,同在一分支上。半定量RT-PCR分析显示BsHsp17.3基因在白及根、叶、鳞茎及花组织中的表达具有特异性,且BsHsp17.3基因在叶中的表达量较高,在鳞茎及花中不表达。实时荧光定量PCR检测显示BsHsp17.3对非生物胁迫高温、低温具有明显应答反应,20%PEG模拟干旱胁迫不诱导该基因表达,推测该基因在白及防止倒苗过程中可能发挥一定作用。     

Low temperature induces oocytes p34^cdc2 synthesis and accumulation—the acquisition of competence to resume meiosis in toad oocytes

Full grown oocytes derived from Bufo Bufo gargarizans rearing at high temperature environment (24℃), never underwent GVBD after progesterone treatment.No p34^cdc2 Hl kinase activity was detected in the oocytes after progesterone stimulation or OA microinjection;Western blotting analysis showed that the level of p34^cdc2 and p33 in the oocytes are significantly lower than those in the oocytes derived from the hibernating toads (below 10℃).^35S-Met incorporation analysis showed that when the oocytes were incubated at 6℃,synthesis of about thirty defferent polypeptides was promoted or induced,including p34^cdc2 and some other p13^suc1-binding proteins.All these results indicated that a low temperature environment is essential for the oocytes of Bufo Bufo gargarizans to express and stord some cell cycle drivers and its regulators,and to gain the maturation competence.These results will also provide a nwe clue for explaining the molecular mechanisms why gametogenesis of some organisms depends on a relative low temperature and how to maintain the geographical distribution of some animals.     

毛蚊科九新种记述：双翅目：长角亚目

本文记述了双翅目毛蚊科3属9新种,其中棘毛蚊属3种:长喙棘毛蚊 Ditophus macrosiphonius sp.nov.,吉林棘毛蚊 D.jilinensis sp.nov.和膜棘毛蚊 D.membranaceus sp.nov.;叉毛蚊属2种:异角叉毛蚊 Penthetria aberrans sp.nov.和甘肃叉毛蚊 P.gansuensis sp.nov.;襀毛蚊属4种:裂襀毛蚁 Plecia dilacerabilis sp.nov.,峨眉襀毛蚊 P.emeiensis sp.nov.,钳襀毛蚊 P.forcipiformis sp.nov.和长叶襀毛蚊 P.longifolia sp.nov.。所有模式标本均保存在北京农业大学昆虫标本室。     

AUTOROTATION, SELF-STABILITY, AND STRUCTURE OF SINGLE-WINGED FRUITS AND SEEDS (SAMARAS) WITH COMPARATIVE REMARKS ON ANIMAL FLIGHT

• 1 A samara is a winged fruit or seed that autorotates when falling, thereby reducing the sinking speed of the diaspore and increasing the distance it may be transported by winds. Samaras have evolved independently in a large number of plants.
• 2 Aerodynamical, mechanical, and structural properties crucial for the inherent self-stability are analysed, and formulae for calculation of performance data are given.
• 3 The momentum theorem is applied to samaras to calculate induced air velocities. As a basis for blade element analysis, and for directional stability analysis, various velocity components are put together into resultant relative air velocities normal to the blade's span axis for a samara in vertical autorotation and also in autorotation with side-slip.
• 4 When falling, a samara is free to move in any sense, but in autorotation it possesses static and dynamic stability. Mainly qualitative aspects on static stability are pre sented. Simple experiments on flat plates at Reynolds numbers about 2000 as in samaras, showed that pitch stability prevails when the C. M. (centre of mass) is located 27–35 % of the chord behind the leading edge. The aerodynamic c.p. (centre of pressure) moves forward upon a decrease of the angle of attack, backward upon an increase. In samara blades the c.m. lies ca. one-third chord behind the leading edge, and hence the aerodynamic and centrifugal forces interact so as to give pitch stability, involving stability of the angles of attack and gliding angles.
• 5 Photographs show that the centre of rotation of the samara approximately coincides with its c.m.
• 6 The coning angle (blade angle to tip path plane) taken up by the samara is determined by opposing moments set up by the centrifugal and aerodynamic forces. It is essentially the centrifugal moment (being a tangent function of the coning angle, which is small) that changes upon a change of coning angle, until the centrifugal and aerodynamic moments cancel out at the equilibrium coning angle.
• 7 Directional stability is maintained by keeping the tip path plane horizontal whereby a vertical descent path relative to the ambient air is maintained. Tilting of the tip path plane results in side-slip. Side-slip leads to an increased relative air speed at the blade when advancing, a reduced speed when retreating. The correspondingly fluctuating aerodynamic force and the gyroscopic action of the samara lead to restoring moments that bring the tip path plane back to the horizontal.
• 8 Entrance into autorotation is due to interaction between aerodynamic forces, the force of gravity, and inertial forces (when the blade accelerates towards a trailing position behind the c.m. of the samara).
• 9 The mass distribution must be such that the c.m. lies 0–30 % of the span from one end. In Acer and Plcea samaras the C.M. lies 10–20% from one end, thereby making the disk area swept by the blade large and the sinking speed low.
• 10 The blade plan-form is discussed in relation to aerodynamics. The width is largest far out on the blade where the relative air velocities are large. The large width of the blade contributes to a high Re number and thus probably to a better L/D (lift/drag) ratio and a slower descent.
• 11 The concentration of vascular bundles at the leading edge of the blade and the tapering of the blade thickness towards the trailing edge are essential for a proper chord wise mass distribution.
• 12 Data are given for samaras of Acer and Plcea, and calculations of performance are made by means of the formulae given in the paper. Some figures for an Acer samara are: sinking speed 0.9 m/sec, tip path inclination 15°, average total force coefficient 1.7 (which is discussed), and a L/D ratio of the blade approximately 3.
• 13 The performances of samaras are compared with those of insects, birds, bats, a flat plate, and a parachute. They show the samara to be a relatively very efficient structure in braking the sinking speed of the diaspore.
• 14 In samaras the mass, aerodynamic, and torsion axes coincide, whereas in insect wings the torsicn axis often lies ahead of the other two. Location of the torsion axis in front of the aerodynamic axis in insects tends towards passive wing twisting and passive adjustment of the angles of attack relative to the incident air stream, the direction of which varies along the wing because of wing flapping.
• 15 Location of the mass axis behind the torsion axis may lead to unfavourable