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Transition metal bonding strength

A second insight regarding bond strengths can be gained by comparing the enthalpies of atomization of Cr = 95, Mo = 157, and W = 203 kcalmol. Metal-metal bond strengths in dimeric complexes also increase when going from Cr to Mo to W. To date, information appears to support this trend for all transition metals. [Pg.1143]

The transition metal homoleptic complexes containing alkyl ligands are kinetically and thermally less stable than analogous compounds of the main group metals. For some time, it was believed that this is a result of the diminished strength of the carbon-transition metal bond. However, thermodynamic studies showed that the M —C(sp ) bond energy for the transition metals and the main group metals is the same (Table 4.2). [Pg.201]

The dependence of substitution rates on metal-metal bond strengths emerges from good correlations between the activation enthalpy of reaction of [M2(CO)io1 (M = Mn, Tc, or Re), [MnRe(CO)io], and [Mn(CO)4L]2 [L = PPh3 or P(OPh)3] with oxygen, with corresponding force constants for the metal-metal bond vibration and with hv for the a transition, which involves orbitals from metal-metal interaction. ... [Pg.366]

Sequences such as the above allow the formulation of rate laws but do not reveal molecular details such as the nature of the transition states involved. Molecular orbital analyses can help, as in Ref. 270 it is expected, for example, that increased strength of the metal—CO bond means decreased C=0 bond strength, which should facilitate process XVIII-55. The complexity of the situation is indicated in Fig. XVIII-24, however, which shows catalytic activity to go through a maximum with increasing heat of chemisorption of CO. Temperature-programmed reaction studies show the presence of more than one kind of site [99,1(K),283], and ESDIAD data show both the location and the orientation of adsorbed CO (on Pt) to vary with coverage [284]. [Pg.732]

Vessel heads can be made from explosion-bonded clads, either by conventional cold- or by hot-forming techniques. The latter involves thermal exposure and is equivalent in effect to a heat treatment. The backing metal properties, bond continuity, and bond strength are guaranteed to the same specifications as the composite from which the head is formed. AppHcations such as chemical-process vessels and transition joints represent approximately 90% of the industrial use of explosion cladding. [Pg.150]

Adhesive strength is evaluated at room temperature as well as at the extreme temperatures of —65°F and 180°F. Aircraft structure can reach —65°F at cruise altitudes and 180°F on the ground in a hot, sunny location. The types of toughened epoxies commonly used for metal bond adhesives have glass transition temperatures not much greater than 200°F, so properties fall off drastically at higher temperatures. [Pg.1147]

Table 3. Bond lengths (A), bond dissociation energies (kcal/mol), a- and n-bond strengths (kcal/mol), charges on phosphorus (e), and orbital energies (eV) for first row transition metal complexes ML =PH ... Table 3. Bond lengths (A), bond dissociation energies (kcal/mol), a- and n-bond strengths (kcal/mol), charges on phosphorus (e), and orbital energies (eV) for first row transition metal complexes ML =PH ...
Apart from the hardness and softness, two reactivity-related features need to be pointed out. First, iron salts (like most transition metal salts) can operate as bifunctional Lewis acids activating either (or both) carbon-carbon multiple bonds via 71-binding or (and) heteroatoms via a-complexes. However, a lower oxidation state of the catalyst increases the relative strength of coordination to the carbon-carbon multiple bonds (Scheme 1). [Pg.3]


See other pages where Transition metal bonding strength is mentioned: [Pg.194]    [Pg.194]    [Pg.119]    [Pg.268]    [Pg.119]    [Pg.166]    [Pg.854]    [Pg.97]    [Pg.66]    [Pg.90]    [Pg.142]    [Pg.1159]    [Pg.97]    [Pg.315]    [Pg.316]    [Pg.841]    [Pg.73]    [Pg.148]    [Pg.631]    [Pg.1142]    [Pg.1158]    [Pg.163]    [Pg.631]    [Pg.110]    [Pg.38]    [Pg.69]    [Pg.2777]    [Pg.59]    [Pg.411]    [Pg.127]    [Pg.22]    [Pg.115]    [Pg.262]    [Pg.808]    [Pg.305]    [Pg.203]    [Pg.108]    [Pg.30]    [Pg.42]    [Pg.48]    [Pg.55]    [Pg.63]    [Pg.153]    [Pg.274]   


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