<oologkalJoumal ofthe Linnean Socieg (2000), 130: 499-510. With 3 figures @ b cl doi: 10.1006/zjls.1999.0238, available online at http://www.idealibrary.com on Incidence and mechanical significance of pneumatization in the long bones of birds J. CUB0 AND A. CASINOS FLS* Department $Animal Biology (Vutebrates), Universip of Barcelona, 08028 Barcelona, Spain Received August 1998; accepted&r publication October 1999 The incidence of pneumatization in avian long bones was studied, by direct observation, in a large sample of species. Only proximal bones (humerus and femur) presented pneurnatization in the sample studied. The incidence obtained was related to the variation of the maximum cortical thickness and mechanical properties, such as bending strength and flexural Young’s modulus. Cortical thickness, bending strength and flexural Young’s modulus were sigtllficantly lower in pneumatized bones than in marrow-filled bones. Furthermore, some congruence was found between pneumatization and systematic groups when compared. In this sense, Charadriformes was the only order studied with total absence of long bone pneurnatization. Results on cortical thickness appear to be in agreement with modelling predictions previously made and with results obtained on other groups of flying vertebrates. The possible selective advantage of reduction in cortical thickness in relation to flying is suggested. 0 2000 The Linnean Soriety of London ADDITIONAL KEY WORDS:-ortical - systematics. thickness - strength - Young’s modulus - bending CONTENTS Introduction . . . . Material and methods Results . . . . . Discussion . . . . Acknowledgements . References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 499 500 503 506 509 509 INTRODUCTION It now seems clear that merely hollow bones (no tissue filling the marrow cavities; see, for example, Kardong, 1998) are a generalized theropod condition (Fastovsky & Weishampel, 1996). However, only modern birds possess bone pneumatization, * Corresponding author E-mail: [email protected] + 0024-4082/00/ 120499 12 $35.00/0 499 0 2000 The Linnean Society of London 500 J. CUB0 AND A. CASINOS that is bones with pneumatic foramina: openings in the wall of the bone for the air sacs to enter the internal bone cavities. No Mesozoic dinosaur nor any Cretaceous bird has them (Fastovsky & Weishampel, 1996). At the same time, the traditional generalized assumption that, due to penumatization, the avian skeleton is lighter than the mammalian skeleton, is questionable (Prange et al., 1979). In fact some skeletal structures-such as the humerus, ulna-radius, tibiotarsus and fibula-display larger masses in birds than in mammals (Cubo & Casinos, 1994). Unfortunately, data on the incidence of pneumatization in the avian skeleton are rather scarce and always partial (Bellairs & Jenkin, 1960; Portmann, 1950; Winkler, 1985).Although Portmann (1950)accepted that pneumatization may relate to the supposed lightness of the avian skeleton, he showed there does not appear a strict relationship between degree of pneumatization and flight ability. For example, he pointed out that both gulls (flying birds) and kiwi (running bird) lack pneumatization, and if in Aepyornis the femur is pneumatized, in Dinomis it is not, despite the fact that both are running birds. According to the review carried out by Winkler (1985), the only general rule seems to be that the postcranial skeletons of diving birds (e.g. Spheniscidae) appear to be less pneumatized and, furthermore, within the same systematic group, skeletons of large species appear to be more highly pneumatized than those of smaller species. In addition, for a limited sample, Currey (1984) and Currey & Alexander (1985) found that cortical thickness, measured as the ratio of the internal to the external diameter in the sagittal direction, is lower in pneumatized bones than in marrowfilled bones. Finally, Alexander (1982), Currey (1984) and Currey & Alexander (1985) modelled the optimal thickness of the walls of pneumatized and marrowfilled bones, with regards to their mechanical properties. However, as far as we know, to date no empirical data on the mechanical significance of pneumatization vs. marrow-filled bones have been published. The aim of the present research was to study the incidence of pneumatization in avian long bones and the mechanical consequences of the pneumatization process, quantified by means of maximum cortical thickness, bending strength and flexural Young’s modulus. MATERIAL AND METHODS The long bones (humerus, radius, ulna, femur, tibiotarsus and tarsometatarsus) of 35 adult specimens, belonging to 24 species, were studied (Table 1).The systematic scheme of Cracraft (1981) was followed. Bones were fresh material, obtained from recently dead animals of known body mass and were kept wet during experiments. Of methods suggested by Hogg (1980) to recognize pneumatized bones, direct examination was considered the most useful, since broken bones, resulting from mechanical tests (see below) were available. A microscope was used to make more accurate direct observations. The criterion adopted to establish that a bone was pneumatized was the total absence of marrow in the diaphyses; epiphyses were not analysed. In the whole sample studied, diaphyses were marrow-filled or hollow: no ambiguous state was found. At the same time, within a given bone of a particular species, the hollow or marrow-filling condition was constant. After breaking, the sections of the bones, at the only fracture point, were ground down until smooth cross-sections were obtained. PNEUMATIZATION IN AVIAN BONES 50 1 TABLE1 . List of the species studied. Numerals in parentheses following species names indicate the number of individuals studied. Abbreviations: F =femur; H =humerus; R = radius; U =ulna; Ta = tarsometarsus; Ti= tibiotarsus. 1 =bone with marrow; O=pneumatized bones; - presence or absence of marrow was not checked. Body masses of the specimens studied are given between parentheses. H U R F Ti Order Galliforrnes P h i a n u s colchicus (2) (1 023 g, 826 g) 0 I 1 0 I Order Gruiforrnes Otis ktrax(1) (271 g) 0 I 1 0 Ta Order Falconiformes Accipi& gentilis ( I ) (1 024 g) Accipiler nisuc (2) ( I 6 1 g, I63 g) Asia otus (2) (262 g, 203 g) Buteo buko ( I ) (497 g) Cirm cianeus ( I ) (295 g) Falco columbarius ( I ) (10 I g) Fako tinnunculus (3) ( 168 g, I35 g, 1 10 g) Olus scops (3) (77 g, 63 g, 69 g) 7ylo alba (2) (233 g, 275 g) Order Charadriiformes Aka torda ( I ) (489 g) Burhinus oedicnemus ( I ) (207 g) Caldrk alpina ( I ) (49 g) Celocheldon nilotica ( I ) ( 157 g) Lam ndibunduc (2) (2I2 g, 159 g) S h a alblfmns ( I ) (39g) S h a h i m n d o ( 1 ) (1199) Order Colurnbiformes Columba palumbus ( I ) (401 g) I 0 1 0 - 0 I Order Piciformes Picus &id& (3) ( I 30 g, 158 g, I58 g) 0 I Order Coraciiformes Memps apim& ( I ) (57 g) 0 I Order Psittaciformes &op~iti~amonachus (1 ) ( I 33 g) Njmphicw hollandicw ( I ) (58 g) Order Passeriforrnes Oriolus ori0lus ( I ) (48 g) I 1 1 I 1 1 1 1 I 1 0 1 Bending strength and flexural Young’s modulus (tangential modulus) were calculated by means of three-point bending tests carried out with an INSTRON 85 l l machine (Fig. 1). Bones were loaded along the sagittal axis, at the mid-point of the length, until breaking, with an actuator speed of 0.5 mm/min. A 10 kN load cell was used. For each bone, stiffness (slope of force-extension curve), and maximum load were obtained directly from the machine, by means of the specific software, with appropriate assumptions and modifications. See, for example, Spatz et al. (1996) for a similar methodology. Cross sections (see above) were analysed with a Hitachi video camera, mounted on a microscope, to calculate internal and external diameters and second moment of area of each bone. See Cub0 & Casinos (1998) for more details on the method. For the second moment of area, the classical formula 502 J. CUB0 AND A. CASINOS Figure 1. Schematic arrangement for the three-point bending tests used in the present research. See text for more details. Figure 2. Scheme of the cross-section of a hypothetical bone. Shadow zone corresponds to cortical internal area. Abbreviations: B, breadth of the bone; & (thick bar), breadth of the thin layer; radius; R, external radius; W, width of the bone; xx, neutral axis;y, distance from the thin layer to the neutral axis; z, width of the thin layer. See text for details. m, was used, where .t-Sy is a thin layer of the cross-sectional surface area placed at a distancey from the neutral axis (Alexander, 1983) (Fig. 2). Second moment of area was calculated for the sagittal direction in which the bone was loaded. Using these data, the bending strength and the flexural Young modulus were calculated using the following formulae (Jackson, 1992): PNEUMATIZATION IN AVIAN BONES 503 o=- 3 P,,*S 2*B*d E= (F/x)*S3 48*Z (3) where o is the bending strength, E the flexural Young's modulus, P,, the maximum load, S the span used, B and D the breadth and the width of the specimen, respectively, F/x the stiffness and I the second moment of area (Figs 1 and 2). The K parameter, the ratio of the internal to the external diameter, measures the thickness of the cortical bone normalized to diameter for comparison of bones of different size (Currey & Alexander, 1985) (Fig. 2). The minimum K parameter and its orientation were calculated on each bone by using the IMAT program (Cubo & Casinos, 1998).The orientation of the minimum K was reported by means of angles expressed in degrees, considering the antero-posterior a x i s as 0". This orientation ranges from -90" to 90". Negative values were transformed into positive values in order to determine deviations in the orientation of the minimum K from the sagittal axis. Variations of bending strength, flexural Young's modulus and minimum K parameter were analysed separately on marrow-filled and pneumatized (gas-filled) bones. Marrow-filled and pneumatized femora were also studied separately to test for differences between pneumatized and non-pneumatized patterns in a given type of bone. This protocol could not be followed with humeri because of the small size of the sample. See Results where the special treatment given to femora and humeri in relation to other long bones is described. Standard deviation, mean, and 95% mean confidence interval were calculated. At the same time the variation of the orientation of the minimum K was also analysed by means of circular descriptive statistics (Zar, 1984).Mean angles, their 95Y ' o' confidence limits and circular standard deviations were calculated for the total sample as well as for marrow-filled and pneumatized bones. Finally, assuming the allometric equation y =a*? (4) bending strength and flexural Young's modulus were regressed to body mass, separately for marrow-filled and pneumatized bones. Model I of regression was used, in accordance with previous work (Biewener, 1982). RESULTS Table 1 shows the incidence of pneumatization in the sample studied. Globally, distal long bones (ulna, radius, tibiotarsus and tarsometatarsus) did not show pneumatization. Only humeri and femora were pneumatized, although with very different percentages, since while 70% of the humeri studied were pneumatized, only 39% of the femora studied had no marrow. In relation to a possible congruence between the incidence of pneumatization and systematics, some patterns arose, despite limited sample sizes. Charadriiformes (7 species and 8 specimens studied) J. CUB0 AND A. CASINOS 504 TABLE 2. Variation in maximum cortical thickness, expressed by means of the K parameter, bending strength (a)and flexural Young's modulus Q between marrow-filled and gas-filled bones studied. In each case, the femur subsample studied is indicated. Size of the sample (n), standard deviation, mean, and mean confidence interval, are shown. Other abbreviations: GPa =gigapascals; MPa = megapascals K n SD Mean Mean confidence interval Marrow-filled Total Femur 123 18 0.11 0.05 0.65 0.74 0.63, 0.67 0.72, 0.76 Gas-filled Total Femur 30 9 0.04 0.03 0.77 0.80 0.76, 0.79 0.78, 0.82 Total Femur I22 18 51.20 26.79 200.19 153.87 191.02, 209.36 140.54, 167.20 Total Femur 30 9 36.92 23.93 139.03 124.88 125.25, 152.81 106.49, 143.27 Total Femur 1 I5 18 7.65 5.35 14.73 11.09 13.32, 16.14 8.43, 13.75 Total Femur 30 9 4.10 4.16 7.67 6.88 6.14, 9.20 3.68, 10.08 u (MPa) Marrow-filled Gas-filled E (GPa) Marrow-filled Gas-filled was the only order with complete absence of pneumatization in long bones, in accordance with the previous observation of gulls by Portmann (1950) (see above). On the other hand, in Falconiformes (9 species and 16 specimens studied) all humeri were pneumatized, whereas the femora differed in two families: in Accipitridae marrow was absent from all the femora; in Strigidae marrow was always present. The limited sample size of the other orders studied made similar separate analyses inadequate. Table 2 shows results on the minimum K parameter, which means maximum cortical thickness. The statistical analysis carried out for the whole sample showed that confidence intervals of the means do not overlap at all: pneumatized bones were significantly thinner than marrow-filled bones. These results are graphically shown in Figure 3. A parallel result was obtained when sub-samples corresponding to femora were compared. However, the confidence intervals of the means corresponding to both pneumatized and marrow-filled humeri overlapped, possibly because of the reduced sizes of the respective sub-samples. No difference was found in the orientation of the maximum cortical thickness (minimum K) (Table 3). In both cases, the circular mean confidence intervals for the whole sample included 45", which means an orientation equidistant from both sagittal and transverse diameters. Table 2 also shows the results obtained from mechanical parameters tested, namely bending strength and flexural Young's modulus. Considering the whole sample, the confidence intervals of the means show that marrow-filled bones are stronger and stiffer than pneumatized bones, i.e. bending strength and Young's modulus are significantly lower when marrow is absent. However, when the subsample of femora is analysed, confidence intervals of the means overlap. PNEUMATIZATION IN AVIAN BONES "0 505 0.2 0.4 0.6 0.8 1 0.2 0.4 0.6 0.8 1 4 2 0 ; 0 K parameter Figure 3. Graphic representation of the distribution of the K parameter in the marrow-filled (A) and pneumatized bones (B). Number of species and K parameter are indicated in y-axis and x-axis, respectively. TABLE 3. Variation in the orientation of minimum K (Kq. See text for details. Abbreviations as in Table 2 Ke Total Marrow-filled Gas-filled n Circular SD circular mean circular mean confidence interval I54 I23 30 24.9 27.7 24.9 45.3 43. I 48.7 42.3, 48.3 39.6, 46.6 39.7, 57.7 In can be assumed that mechanical properties like strength and stiffness are specific to the materials and independent of body mass (Currey, 1984). Previous results on long bone strength (Biewener, 1982) seem to confirm this assumption. Nevertheless, the statistical analysis of the mechanical results obtained with our sample, showed that bending strength is correlated with body mass in the case of J. CUB0 AND A. CASINOS 506 TABLE 4. Results of the correlations of bending streqgth (a) and flexural Young's modulus (4to body mass for marrow-filled and gas-filled bones studied. Equations and confidence intervals for a (y-interception) and b (slope) are indicated. Correlation coefficients are indicated by r. For other abbreviations, see previous tables Model I Mechanical n properties (Pa) to Body mass (9) equation cr (MPa) Marrow-filled Gas-filled 122 30 0.081 0.556 y=220.680* x A -0.026 y=334.492* X " -0.170 E (GPa) Marrow-filled 115 30 0.224 0.175 y=29.218* x " -0.161 y=13.060* x " -0.137 Gas-filled ' r a confidence interval b confidence interval 164.247, 296.503 -0.083, 0.032 195.287, 572.925 -0.269, -0.072 14.773, 57.789 2.560, 66.640 -0.292, -0.030 -0.436, 0.162 pneumatized bones (r=0.556, for 28 degrees of freedom, for R0.05) (Table 4). The same result was found for the flexural Young's modulus of the marrow-filled bones. In both cases slopes were negative, different from 0, since this value is excluded by the slope confidence interval, which means that both parameters decrease with body mass. DISCUSSION Long bones are tubular structures, which means they have values of K greater than 0. It is interesting to consider the saving in mass produced by having tubular bones. Pauwels (1980) and Currey & Alexander (1985) estimated values of 8% and 13% respectively for the maximum saving in mass by having tubular bones. Since limb bones must be accelerated and decelerated during locomotion and lightness favours flying ability, this saving in mass is thought to be important and positively selected. At the same time bones must resist stresses acting on them. Therefore; it can be assumed that an optimal cortical thickness, or optimal K, exists. Alexander (1982), Currey (1984) and Currey & Alexander (1985) made predictions for this optimal K. They found different values regarding Merent mechanical requirements, depending on whether bones were pneumatized or marrow-fled. The following considerations should be borne in mind when comparing the mean minimum K values obtained in this study with the predictions of Currey & Alexander (1985): (1) Marrow-fdled bones studied have a mean minimum K value of 0.65. These results are very similar to the optimum value of K predicted by Alexander (1982) (0.6) and Currey & Alexander (1985)(0.67), assuming marrow density is 930 kg*mP3 and bone density is 2 100 kg*m-3. According to the predictions of their model, bones with this K would be selected for minimum mass and be strong enough not to yield or fail to fatigue. At the same t i e , Currey & Alexander (1985) modelled an optimum K of 0.75 for a stiff enough bone in bending. This value is very close to that obtained in the present study with the partial sample of marrow-fled femora (0.74). Currey & Alexander's mean calculated for sagittal K in birds was about 0.7, which is intermediate between the optima for strength and stiffness. (2) Mean minimum K values obtained for pneumatized bones and for the pneumatized femora subsample were 0.77 and 0.85 respectively. Low values of PNEUMATIZATION IN AVIAN BONES 507 cortical thickness are thought to be a compromise between yield strength requirements vs. local buckling prevention. Our present results are also similar to those obtained by Currey & Alexander (1985; sagittal K range 0.69-0.86) and lower than the optima K predicted by Alexander (1982) and Currey & Alexander (1985) (K =0.93). Indeed, Currey and Alexander (1985) suggested that it is almost impossible for a bird bone to have a K value higher than those observed for pneumatized bones. Otherwise, it would be impossible to withstand traumas in this area. (3) Currey & Alexander (1985) suggested that perhaps distal limb bones may tend to have lower values of K either in terrestrial mammals or flying birds. This assumption seems correct for flying birds, according to our results: the only proximal bone studied, the femur, always has K values higher than the total sample. (4) Currey & Alexander (1985) anticipated that in both terrestrial mammals and flying birds larger animals would show a tendency to have lower values of K (higher values of cortical thickness) than related smaller animals. This expectation seems to be in agreement with a previous result of Cubo & Casinos (1998), showing that cortical area scales with positive allometry in the avian hind limb bones. However, when minimum K from either hind limb bones or the total sample of birds of the present study were regressed against body mass, results showed that K was independent of body mass, since the correlation coefficients were 0.088 and 0.068, respectively. We have shown that the mean minimum K is significantly lower in marrow-filled than pneumatized bones and that mean minimum K is also significantly lower in the marrow-filled than in the pneumatized femora subsample (Table 2). Does this morphological difference have some mechanical significance?Mean bending strength and mean flexural Young’s modulus are significantly higher for marrow-filed bones than for pneumatized bones. Sub-samples corresponding to femora follow the same pattern, but differences are not significant (Table 2). We wonder whether with a greater number of femora results might be different, taking into account the results obtained on cortical thickness reported above. Therefore, our findings indicate that cortical thickness may be relevant for bone strength and stfiess. The question is whether the presence of marrow, with a density approximately half that of the bone (Alexander, 1982),is also relevant to the mechanical behaviour of the bone. In their model Currey & Alexander (1985) assumed that marrow merely contributed to the mass of the bone, but other authors (see, for example, Kafka, 1983) claim marrow may be important to increase bone strength. In this situation, we wonder whether the variation found in mechanical parameters is a direct effect of the presence or absence of marrow or independent of it. As far as we know, no study is available on the variation of strength and/or stiffness in avian bone. However, Bou et al. (1991) carried out extensive research on bending moments at breaking in avian long bones. Within the sample used (about 100 specimens for bending) variation of maximum and minimum values of moments for animals with the same body mass was twice as high or more, independent of whether bones were pneumatized or not. Therefore, the null hypothesis to be tested is whether the differences in strength found in the present research can induce variations in bending moments at breaking within the range found by Bou et al. (1991). According to Alexander (1983) 508 J. CUB0 AND A. CASINOS where o is bone strength (as calculated in the present research), M, is the breaking moment in bending, ys the maximum perpendicular distance from the neutral axis to the outline, as in (l), and I, the second moment of area, with all the parameters being considered relative to the sagittal axis. Therefore, assuming either marrowfilled or pneumatized bones to have elliptical cross sections: o= M.*yI (l-Kq*Tn* r;"*rl Given a mean value of strength in marrow-filled bones of 200 MPa and a K value of 0.65 (Table 2), Similarly, for the pneumatized bones (means, Table 2, again). CT= 139 MPa and K=0.77; see In principle, we can assume that for the same body mass there is no geometric difference between marrow-filled bones and pneumatized bones, with the only exception of K. Therefore, calling C the quotient between the geometric parameters 4 we arrive at the following expressions: @rMs O M , 139=------1-0.773- 0.54 Therefore, M, = 200*0.73-- 14.6/c C M, = 139*0.54 =7 5 / c C This means that, for the same body mass, the breaking moment in bending for marrow-filled bones should be almost double that of pneumatized bones, a range PNEUMATIZATION IN AVIAN BONES 509 of variation very similar to that found by Bou et al. (1991). According to this, it seems there is no necessity to invoke a hydraulic strengthening effect (Kafka, 1983): differences in cortical thickness alone could be sufficient to explain the higher strength of marrow-filled bones. When results for Young’s modulus are considered, conclusions are not very different: bending breaking moments of marrow-filled bones ought to be 2.5 times higher than those of pneumatized bones, which, given the results of Bou et al. (1991), is to be expected. Swartz et al. (1992) showed that cortical thickness of forelimb bones of bats falls within the range of previous values of K calculated for birds and pterosaurs by Currey & Alexander (1 985). Therefore, the reduction of cortical thickness would be a convergence of the three large groups of flying vertebrates (pterosaurs, birds and bats). If according to the present analysis, hollow bones are less resistant in bending and less stiff than marrow-filled bones, a question arises: what could be the selective advantage of hollow bones? Swartz et al. (1992) argue that resistance to torsional stresses, originated by downstroke movements in wings, can be important for flying animals. Torsional stress is a direct function of the polar moment (J(Young, 1989) and according to Swartz et al. (1992) this parameter would be maximized by circular cross-sectional geometry of maximum outer diameter. So, hollow bone design would involve a sacrifice of bending strength in order to obtain high values of torsional strength, taking also into account that, as indicated above and previously (Cubo & Casinos, 1994), the reduction of skeletal mass does not seem very important. Indeed, the torsional effect in flying has been also advocated recently (Cubo & Casinos, 1998) to explain the disagreement between the directions of maximum bending loads and maximum second moment of area in the avian humerus. ACKNOWLEDGEMENTS The Servei de Proteccio i Gestib de la Fauna (Generalitat de Catalunya) generously provided the specimens used in this study. Alejandro de Giorgio (Serveis CientificoTkcnics, Universitat de Barcelona) prepared the IMAT program, following the specifications of the authors. P. Zioupos (University of York) commented on the paper; Robin Rycroft (Servei d’Assessorament LinGistic, Universitat de Barcelona) corrected it for language. The editorial efforts of Marvalee H. Wake are much appreciated. Thanks are also due to two anonymous referees. The project was funded by DGICYT, grant no. PB 914282. REFERENCES Alexander RMcN. 1982. Optima fir animals. London: Arnold. Alexander RMcN. 1983. Animal mechanics. 2nd. edn. Oxford: Blackwell. Bellairs Ad’A, Jenkin CR. 1960. The skeleton of birds. In: Marshall AJ, ed. Biology and Comparative Physiology @Birds, vol. 1. New York Academic Press, 241-300. Biewener AA. 1982. Bone strength in small mammals and bipedal birds: do safety factors change with body size? Journal of Experimental B w l o ~98: 289-301. Bou Jy Olmos M, Casinos A. 1991. Strengths of the limb bones of birds and small mammals in bending and twisting. Annales des S&nces Naturelles, <oolo@ 12: 197-207. CracraftJ. 1981. Toward a phylogenetic classification of the recent birds of the world (Class Aves). The Auk 98: 681-714. 510 J. C U B 0 AND A. CASINOS Cub0 J, Casinos A. 1994. Scaling of skeletal mass in birds. BeigianJoumal of<oology 124: 127-137. 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