# Synthesis, Characterization, and Thermokinetic Analysis of New Epoxy Sugar Derivative

Authors: Selinay Y. Erişkin; Fatma Ç. Telli; Yeliz Yıldırım; Yeşim Salman
Journal: Journal of Chemistry
 (2014)

---

## Abstract

The synthesis of 5,6-O-isopropylidene-1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (compound1) and 5,6-O-isopropylidene-1,2-O-(R)-trichloroethylidene-3-O-(2′,3′-epoxypropan-1′-yl)-α-D-glucofuranose (compound2) was carried out. The synthesized compounds1 and2 were characterized by nuclear magnetic resonance (1H-NMR), Fourier transform infrared spectroscopy (FTIR), and thermogravimetric analysis (TG). The FTIR and 1H NMR spectra showed that the epoxy group in compound2 was attached by means of a nucleophilic substitution reaction. The activation energies for thermal degradation of compounds1 and2 were calculated from their TG data by using the Kissinger-Akahira-Sunose (KAS) and Tang methods.


---

## Body

## 1. Introduction

Epoxides are versatile intermediates in organic synthesis. Not only are these compounds easily prepared from a variety of starting materials, but also the inherent polarity and strain of their three-membered ring make them susceptible to reaction with a large number of reagents: electrophiles, nucleophiles, acids, bases, reducing agents, and some oxidizing agents [1].Chiral oxiranes are very important building blocks for the synthesis of enantiomerically pure complex molecules of biologically active compounds [1–3]. Carbohydrates contain several functional groups and stereogenic centres in one molecular unit, which allows the use of carbohydrates as tools in stereochemical differentiations, as starting materials in ex-chiral pool syntheses of interesting enantiopure compounds [4], as chiral templates in asymmetric transformations [5], and as chiral auxiliaries in stereoselective synthesis [6, 7].Oxiranes are key intermediates in the asymmetric synthesis of chiral 1,2-difunctionalized compounds of biological and pharmacological interest, such asα-hydroxy-β-amino acids derived from isoserine, which are important members of the β-amino acid family. Isoserine derivatives constitute an essential fragment in natural products of high therapeutic value [3], such as Taxol (an anticancer agent), whose side chain is N-acyl-(2R,3S)-phenylisoserine; bestatin (a dipeptide modifier of the immune response), in which one of the amino acids is (2S,3R)-2-hydroxy-3-amino-3-phenylbutyric acid, and the kinostatins (potent inhibitors of the HIV-1 protease), in which one of the constituent amino acids is (2S,3S)-2-hydroxy-3-amino-3-phenylbutyric acid.The aim of this study was to investigate the possibility of producing sugar compound (2) which might be used as a monomer for the synthesis of certain polymers. Glucose is an abundant and sustainable natural product. The chloralose derivative of glucose is also prepared easily with choral and acid catalysts such as H2SO4 [8]. It is not possible to make an epoxy derivative of α-chloralose without using the protecting group (5,6-O-isopropylidene). 1,2-O-(R)-Trichloroethylidene-α-D-glucofuranose was further acetalized with 2,2-dimethoxypropane (2,2-DMP) to give the 5,6-O-isopropylidene derivative (compound1) [9]. This sugar derivative has only one free hydroxyl group which can be etherified. After inserting a leaving group, it can also be used in a substitution reaction. Etherification of the C-3 hydroxyl group is not easy because of the low reactivity, due to steric effects of the protecting groups. Reaction with epichlorohydrin was carried out with 5,6-O-isopropyliden-1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (1) Figure 5. This derivative was used as a starting material which has a free C-3 hydroxyl group to react with epichlorohydrin at room temperature under basic conditions. Tetrabutylammonium bromide was used as a phase-transfer catalyst in this reaction. The structures and the stereochemistry of all of the compounds (1 and2) were determined using spectroscopic techniques.


### 1.1. Kinetic Analysis [10–12]

Thermogravimetric analysis can be used for determining the degradation kinetics of a lot of compounds. In general, the thermal degradation reaction of a solid compound can be shown as(1)
A
solid
⟶
B
solid
+
C
gas
,
where A is the starting material and Bsolid and Cgas are the solid residue and the gaseous products, respectively.The thermal degradation kinetics of the compounds is generally expressed by the following typical kinetic equation:(2)
r
=
d
α
d
t
=
k
(
T
)
×
f
(
α
)
,
where T is the absolute temperature (K); α is the conversion per unit time (t); and f
(
α
) is the conversion function which represents the reaction model. The degree of conversion (
α
) is calculated by (3), where m
o, m
t, and m
f are the weights of sample before degradation at time t and after complete degradation, respectively:
(3)
α
=
m
o
-
m
t
m
o
-
m
f
.
k is the reaction constant which can be expressed by the Arrhenius equation:
(4)
k
(
T
)
=
A
o
e
-
(
E
/
R
T
)
,
where A is called the preexponential factor, E is the activation energy, and R is the gas constant.By combining (2) and (4), the following equation is obtained:
(5)
d
α
d
t
=
A
o
e
-
(
E
/
R
T
)
×
f
(
α
)
.
According to the kinetic theory for the nonisothermal decomposition reactions, the fractional conversion α is expressed as a function of temperature which depends on the time of heating. Thus, the heating rate (β) can be described as
(6)
β
=
d
T
d
t
.
As a result, (5) can be modified as follows:
(7)
d
α
d
T
=
(
1
β
)
A
o
e
-
(
E
/
R
T
)
×
f
(
α
)
.
Equations (5) and (7) are the basis for the many equations derived to evaluate thermal analysis data.


### 1.2. Kissinger-Akahira-Sunose (KAS) Method [13, 14]

The KAS method is based on the following equation:(8)
ln
⁡
(
β
T
2
)
=
ln
⁡
A
R
E
g
(
α
)
-
(
E
R
T
)
,
where the plots of ln
⁡
(
β
/
T
2
) versus 1000
/
T for the several α values give straight lines with the slope of -
E
/
R which give the corresponding E values.


### 1.3. Tang Method [15]

The Tang method is based on the following equation:(9)
ln
⁡
(
β
T
1.894661
)
=
ln
⁡
A
E
R
g
(
α
)
+
3.635041
-
1.894661
ln
⁡
E
-
(
1.001450
E
R
T
)
.
Here, the plot of ln
⁡
(
β
/
T
1.894661
) versus 1000
/
T can give E from the slope.


## 1.1. Kinetic Analysis [10–12]

Thermogravimetric analysis can be used for determining the degradation kinetics of a lot of compounds. In general, the thermal degradation reaction of a solid compound can be shown as(1)
A
solid
⟶
B
solid
+
C
gas
,
where A is the starting material and Bsolid and Cgas are the solid residue and the gaseous products, respectively.The thermal degradation kinetics of the compounds is generally expressed by the following typical kinetic equation:(2)
r
=
d
α
d
t
=
k
(
T
)
×
f
(
α
)
,
where T is the absolute temperature (K); α is the conversion per unit time (t); and f
(
α
) is the conversion function which represents the reaction model. The degree of conversion (
α
) is calculated by (3), where m
o, m
t, and m
f are the weights of sample before degradation at time t and after complete degradation, respectively:
(3)
α
=
m
o
-
m
t
m
o
-
m
f
.
k is the reaction constant which can be expressed by the Arrhenius equation:
(4)
k
(
T
)
=
A
o
e
-
(
E
/
R
T
)
,
where A is called the preexponential factor, E is the activation energy, and R is the gas constant.By combining (2) and (4), the following equation is obtained:
(5)
d
α
d
t
=
A
o
e
-
(
E
/
R
T
)
×
f
(
α
)
.
According to the kinetic theory for the nonisothermal decomposition reactions, the fractional conversion α is expressed as a function of temperature which depends on the time of heating. Thus, the heating rate (β) can be described as
(6)
β
=
d
T
d
t
.
As a result, (5) can be modified as follows:
(7)
d
α
d
T
=
(
1
β
)
A
o
e
-
(
E
/
R
T
)
×
f
(
α
)
.
Equations (5) and (7) are the basis for the many equations derived to evaluate thermal analysis data.


## 1.2. Kissinger-Akahira-Sunose (KAS) Method [13, 14]

The KAS method is based on the following equation:(8)
ln
⁡
(
β
T
2
)
=
ln
⁡
A
R
E
g
(
α
)
-
(
E
R
T
)
,
where the plots of ln
⁡
(
β
/
T
2
) versus 1000
/
T for the several α values give straight lines with the slope of -
E
/
R which give the corresponding E values.


## 1.3. Tang Method [15]

The Tang method is based on the following equation:(9)
ln
⁡
(
β
T
1.894661
)
=
ln
⁡
A
E
R
g
(
α
)
+
3.635041
-
1.894661
ln
⁡
E
-
(
1.001450
E
R
T
)
.
Here, the plot of ln
⁡
(
β
/
T
1.894661
) versus 1000
/
T can give E from the slope.


## 2. Results and Discussion

The FTIR spectra of compounds1 and2 are shown in Figure 1. The peak assignments in the FTIR spectrum of compound1 are as follows: C–H in CH3 and C–H in CH2 at 2800–3000 cm−1; C(CH3)3 in isopropylidene protective group at 1374 cm−1; C–O–C peak in the sugar ring at 1150 cm−1; and C–Cl peaks of trichloroethylidene protective group at 827 and 811 cm−1. Finally, the absorption band at 3473 cm−1 corresponds to the presence of the C–3 OH group.Figure 1
The FTIR spectrums of compounds1 and2.The FTIR spectrum of compound2was as follows: C–H in CH3 and C–H in CH2 at 2800–3000 cm−1; C(CH3)3 in isopropylidene protective group at 1372 cm−1; C–O–C peak in the sugar ring at 1100 cm−1; and C–Cl peaks of trichloroethylidene protective group at 832 and 812 cm−1. Instead of the hydroxyl peak observed in the FTIR spectrum of compound1, an ether (C–O–C) peak at 1068 cm−1 is observed in the FTIR spectrum of compound2.In the1H NMR spectra of compound2, the anomeric H-1 proton usually appears at a low field and is a very characteristic and distinct signal. Two doublets are observed in this 1H NMR spectrum. One is the H-1 doublet at δ 6.05 and another is the H-2 doublet at δ 4.74. The coupling constant between H-1 and H-2 is 4.0 Hz which is typical for an α-D-furanose derivative. Due to the twisted conformation of the furanose rings, the dihedral angle between the H-2 and H-3 protons is usually 90° and, hence, in the spectra of compound2, the coupling constant between H-2 and H-3 is 0 Hz. The H-5 proton gives a complex multiplet at δ 4.65. One of the epoxy group signals is H-1′ which is resolved into a double doublet (dd) at δ 3.92 with a coupling constant between H-1′ and H-2′ of 6.4 Hz. H-2′ signal is observed as a multiplet at δ 3.13. The H-3′ signals are resolved giving a dd signal at δ 2.80 with a coupling constant between H-1′ and H-2′ of 11.6 Hz. The isopropylidene methyl groups resonate at δ 1.39 and 1.33. Finally, the trichloroethylidene acetal proton (HCCl3) gives a signal at δ 5.28.


### 2.1. Thermogravimetric Analysis of the Compounds (1 and 2)

Figures2(a) and 2(b) show the TG and DTG thermograms of compound1 and compound2 under nitrogen atmosphere over a temperature range from 30 to 600°C with a heating rate of 10°C min−1, respectively. The derivative of the thermogram with respect to temperature, also known as a differential thermogram or a DTG, shows the maximum rate of compound decomposition (T
max
⁡). The initial (T
i) and maximum (T
max
⁡) degradation temperatures related to the thermograms are summarized in Table 1.Table 1
Initial (T
i) and maximum (T
max
⁡) degradation temperatures for the thermal degradation of the compounds.
Compound number
T
i (°C)
T
max
⁡ (°C)
1
154
276
2
152
248(a) Typical TG curves for compounds1 and2 in N2atmosphere at 10°C min−1. (b) Typical DTG curves for compounds1 and2 in N2atmosphere at 10°C min−1.
(a)
(b)As far as thermal degradation of compounds is concerned, only one degradation stage was observed. TheT
max
⁡ of compound1 was about 276°C while that of compound2 was 248°C. Thus, these results show that the thermal stability of compound1 was approximately 28°C higher than that of compound2. Obviously, it is the epoxy unit, the critical component of the compound, which decreases the thermal stability. In order to obtain detailed information related to the thermal stability of the compounds, the activation energy of the degradation was calculated using the KAS and Tang methods. The KAS and Tang methods were used to analyze the TG data of the compounds because they were independent of any thermal degradation mechanism.


### 2.2. Thermal Degradation Kinetics of the Compounds (1 and 2)

Compounds1 and2 were heated thermogravimetrically under various heating rates such as 5, 10, 15, and 20°C min−1 in a temperature range of 30 to 600°C to determine their thermal degradation activation energies. The TG curves obtained for compounds1 and2 are shown in Figures 3(a) and 3(b), respectively. The individual degradation behavior of each compound was analogous at all heating rates as seen from the figure. The activation energies for the compounds were estimated by the KAS and Tang methods.(a) The TG thermograms of compound1 in argon atmosphere at different heating rates (5, 10, 15, and 20°C min−1). (b) The TG thermograms of compound2 in argon atmosphere at different heating rates (5, 10, 15, and 20°C min−1).
(a)
(b)The average activation energies for compounds1 and2 were found to be 96 and 69 kJ mol−1, respectively, by means of the KAS method. By comparison, the average activation energies when calculated by the Tang method for compounds1 and2 were 113 and 87 kJ mol−1, respectively. The activation energies determined by the KAS and Tang methods indicate that the thermal stability of compound1has a significantly higher E value than that of compound2. Thus, it is shown that the addition of the epoxy group to the structure decreases the thermal stability.The plot ofE versus the degree of conversion is commonly used to indicate the degradation mechanism, that is, whether it is one-step or more. As shown in Figure 4(a) (using the KAS method), the mechanism was almost constant up to α
=
0.8; E is deduced to be between 81 and 103 kJ mol−1 for compound1 and between 75 and 65 kJ mol−1 for compound2, which means that the compounds have only one degradation mechanism. The activation energies calculated through the Tang method for the compounds as a function of the degree of conversion (Figure 4(b)) also showed that the E values were almost constant up to 80% and then increased. Thus, it can be concluded that thethermal degradation mechanisms of compound1 and compound2 exhibit similar behavior. Secondly, the increase in the E values as a function of α may be attributed essentially to thermally more stable structures because of secondary reactions which had occurred during the progress of thermal degradation [16].(a) The plot of activation energy (E) versus the degree of conversion (α) for KAS method of compounds1 and2. (b) The plot of activation energy (E) versus the degree of conversion (α) for Tang method of compounds1 and2.
(a)
(b)Figure 5
The possible reactions of compound2.


## 2.1. Thermogravimetric Analysis of the Compounds (1 and 2)

Figures2(a) and 2(b) show the TG and DTG thermograms of compound1 and compound2 under nitrogen atmosphere over a temperature range from 30 to 600°C with a heating rate of 10°C min−1, respectively. The derivative of the thermogram with respect to temperature, also known as a differential thermogram or a DTG, shows the maximum rate of compound decomposition (T
max
⁡). The initial (T
i) and maximum (T
max
⁡) degradation temperatures related to the thermograms are summarized in Table 1.Table 1
Initial (T
i) and maximum (T
max
⁡) degradation temperatures for the thermal degradation of the compounds.
Compound number
T
i (°C)
T
max
⁡ (°C)
1
154
276
2
152
248(a) Typical TG curves for compounds1 and2 in N2atmosphere at 10°C min−1. (b) Typical DTG curves for compounds1 and2 in N2atmosphere at 10°C min−1.
(a)
(b)As far as thermal degradation of compounds is concerned, only one degradation stage was observed. TheT
max
⁡ of compound1 was about 276°C while that of compound2 was 248°C. Thus, these results show that the thermal stability of compound1 was approximately 28°C higher than that of compound2. Obviously, it is the epoxy unit, the critical component of the compound, which decreases the thermal stability. In order to obtain detailed information related to the thermal stability of the compounds, the activation energy of the degradation was calculated using the KAS and Tang methods. The KAS and Tang methods were used to analyze the TG data of the compounds because they were independent of any thermal degradation mechanism.


## 2.2. Thermal Degradation Kinetics of the Compounds (1 and 2)

Compounds1 and2 were heated thermogravimetrically under various heating rates such as 5, 10, 15, and 20°C min−1 in a temperature range of 30 to 600°C to determine their thermal degradation activation energies. The TG curves obtained for compounds1 and2 are shown in Figures 3(a) and 3(b), respectively. The individual degradation behavior of each compound was analogous at all heating rates as seen from the figure. The activation energies for the compounds were estimated by the KAS and Tang methods.(a) The TG thermograms of compound1 in argon atmosphere at different heating rates (5, 10, 15, and 20°C min−1). (b) The TG thermograms of compound2 in argon atmosphere at different heating rates (5, 10, 15, and 20°C min−1).
(a)
(b)The average activation energies for compounds1 and2 were found to be 96 and 69 kJ mol−1, respectively, by means of the KAS method. By comparison, the average activation energies when calculated by the Tang method for compounds1 and2 were 113 and 87 kJ mol−1, respectively. The activation energies determined by the KAS and Tang methods indicate that the thermal stability of compound1has a significantly higher E value than that of compound2. Thus, it is shown that the addition of the epoxy group to the structure decreases the thermal stability.The plot ofE versus the degree of conversion is commonly used to indicate the degradation mechanism, that is, whether it is one-step or more. As shown in Figure 4(a) (using the KAS method), the mechanism was almost constant up to α
=
0.8; E is deduced to be between 81 and 103 kJ mol−1 for compound1 and between 75 and 65 kJ mol−1 for compound2, which means that the compounds have only one degradation mechanism. The activation energies calculated through the Tang method for the compounds as a function of the degree of conversion (Figure 4(b)) also showed that the E values were almost constant up to 80% and then increased. Thus, it can be concluded that thethermal degradation mechanisms of compound1 and compound2 exhibit similar behavior. Secondly, the increase in the E values as a function of α may be attributed essentially to thermally more stable structures because of secondary reactions which had occurred during the progress of thermal degradation [16].(a) The plot of activation energy (E) versus the degree of conversion (α) for KAS method of compounds1 and2. (b) The plot of activation energy (E) versus the degree of conversion (α) for Tang method of compounds1 and2.
(a)
(b)Figure 5
The possible reactions of compound2.


## 3. Experimental Section

### 3.1. Materials

Epichlorohydrin (stated purity 99%), NaOH (stated purity ≥ 97%, pellets), tetrabutylammonium bromide (stated purity 98%), 1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (α-chloralose) (stated purity ≥ 98%), EtOAc (stated purity 99%), sodium hydrogen carbonate (stated purity 98%), Na2SO4 (stated purity 98%), n-hexane (stated purity 99%), and CH2Cl2 (stated purity 99%) were purchased from Merck A.G and Sigma-Aldrich. The materials and chemicals were used without any further purification.


### 3.2. Instrumentation

The structures of the synthesized compounds were determined by means of1H NMR (nuclear magnetic resonance) spectra of the compounds dissolved in deuterated chloroform using a Varian 400 MHz NMR Spectrometer.The FTIR (Fourier transform infrared spectroscopy) spectra of the compounds were obtained using a Perkin Elmer 100 FT-IR Spectrometer and the KBr pellet technique.The TG (thermogravimetric analysis) curves were recorded using Perkin Elmer, Diamond TG/DTA. The samples were heated under N2 atmosphere over a temperature range of 30 to 600°C with a heating rate of 10°C min−1. The weight loss (TG curve) and its first derivative according to the temperature (DTG curve) were recorded simultaneously.


### 3.3. 5,6-O-Isopropylidene-1,2-O-(R)-trichloro-ethylidene-α-D-glucofuranose (1)

A solution of 1,2-(R)-trichloroethylidene-α-D-glucofuranose (α-chloralose) (5.0 g, 16.2 mmol), 2,2-dimethoxypropane (4 mL, 32.4 mmol), and PTSA (5 mg) in DMF (50 mL) was stirred for 24 h at room temperature. The mixture was neutralized with a 5% solution of NaHCO3 and the solution was removed. The syrupy residue was crystallized from methanol (4.72 g, 84%), m.p. 103–105°C, [
α
]
D
31
-
32.0 (c 1, MeOH). 1H NMR (CDCl3, 400 MHz): δ 6.12 (d, 1H, J
1
,
2 4.0 Hz, H-1), 5.31 (s, 1H, HCCl3), 4.75 (d, 1H, H-2), 4.59 (ddd, 1H, H-5), 4.45 (dd, 1H, J
4
,
5 2.8 Hz, H-4), 4.32 (br d, 1H, J
3,4 3.2 Hz, H-3), 4.16 (dd, 1H, J
6
a
,
6
b 8.8, J
5,6
a 6.4 Hz, H-6a), 3.96 (dd, J
5
,
6
b 5.2 Hz, H-6b), 2.65 d (br s, 1H, OH), 1.42 (s, 3H, CH3-isop.), 1.35 (s, 3H, CH3-isop.).


### 3.4. 5,6-O-Isopropyliden-1,2-O-(R)-trichloroethylidene-3-O-(2′,3′-epoxypropan-1′-yl)-α-D-glucofuranose (2)

Epichlorohydrin (20 mL, 256 mmol) was stirred with aq NaOH (50%, 1.25 mL) and tetrabutylammonium bromide (0.5 g, 1.55 mmol) for 30 min. 5,6-O-Isopropyliden-1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (1) (2 g, 5.8 mmol) was added slowly at approximately 5°C under stirring and the reaction was continued at the same temperature for 3 hours, followed by additional 12 hours at room temperature. The reaction mixture was poured over crushed ice and extracted with EtOAc (4
×
10 mL); the organic layer was neutralized with aqueous saturated sodium hydrogen carbonate and washed with distilled water (2
×
5 mL) and dried over anhydrous Na2SO4 and filtered. The filtrate was concentrated to give syrup. The syrup was crystallized from hot hexane at 0°C to give the pure compound2 (1.75 g, 76%), m.p. 101-102°C, [
α
]
D
25
-
0.20 (c 1, CH2Cl2). 1H NMR (CDCl3, 400 MHz): δ 6.05 (d, 1H, J
1
,
2 4.0 Hz, H-1), 5.28 (s, 1H, HCCl3), 4.74 (d, 1H, H-2), 4.65 (m, 1H, H-5), 4.48 (dd, 1H, J
4
,
5 2.8 Hz, H-4), 4.32 (br d, 1H, J
3
,
4 3.2 Hz, H-3), 4.16 (dd, 1H, J
6
a
,
6
b 8.8, J
5
,
6
a 6.4 Hz, H-6a), 3.96 (dd, J
5
,
6
b 5.2 Hz, H-6b), 3.92 (two sets of dd, 1H, J
1
′
,
2
′ 6.4 Hz, H-1′), 3.13 (m, 1H, H-2′), 2.80 (two sets of dd, 1H, J
2
′
,
3
′ 11.6 Hz, H-3′), 1.39 (s, 3H, CH3-isop.), 1.33 (s, 3H, CH3-isop.).


## 3.1. Materials

Epichlorohydrin (stated purity 99%), NaOH (stated purity ≥ 97%, pellets), tetrabutylammonium bromide (stated purity 98%), 1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (α-chloralose) (stated purity ≥ 98%), EtOAc (stated purity 99%), sodium hydrogen carbonate (stated purity 98%), Na2SO4 (stated purity 98%), n-hexane (stated purity 99%), and CH2Cl2 (stated purity 99%) were purchased from Merck A.G and Sigma-Aldrich. The materials and chemicals were used without any further purification.


## 3.2. Instrumentation

The structures of the synthesized compounds were determined by means of1H NMR (nuclear magnetic resonance) spectra of the compounds dissolved in deuterated chloroform using a Varian 400 MHz NMR Spectrometer.The FTIR (Fourier transform infrared spectroscopy) spectra of the compounds were obtained using a Perkin Elmer 100 FT-IR Spectrometer and the KBr pellet technique.The TG (thermogravimetric analysis) curves were recorded using Perkin Elmer, Diamond TG/DTA. The samples were heated under N2 atmosphere over a temperature range of 30 to 600°C with a heating rate of 10°C min−1. The weight loss (TG curve) and its first derivative according to the temperature (DTG curve) were recorded simultaneously.


## 3.3. 5,6-O-Isopropylidene-1,2-O-(R)-trichloro-ethylidene-α-D-glucofuranose (1)

A solution of 1,2-(R)-trichloroethylidene-α-D-glucofuranose (α-chloralose) (5.0 g, 16.2 mmol), 2,2-dimethoxypropane (4 mL, 32.4 mmol), and PTSA (5 mg) in DMF (50 mL) was stirred for 24 h at room temperature. The mixture was neutralized with a 5% solution of NaHCO3 and the solution was removed. The syrupy residue was crystallized from methanol (4.72 g, 84%), m.p. 103–105°C, [
α
]
D
31
-
32.0 (c 1, MeOH). 1H NMR (CDCl3, 400 MHz): δ 6.12 (d, 1H, J
1
,
2 4.0 Hz, H-1), 5.31 (s, 1H, HCCl3), 4.75 (d, 1H, H-2), 4.59 (ddd, 1H, H-5), 4.45 (dd, 1H, J
4
,
5 2.8 Hz, H-4), 4.32 (br d, 1H, J
3,4 3.2 Hz, H-3), 4.16 (dd, 1H, J
6
a
,
6
b 8.8, J
5,6
a 6.4 Hz, H-6a), 3.96 (dd, J
5
,
6
b 5.2 Hz, H-6b), 2.65 d (br s, 1H, OH), 1.42 (s, 3H, CH3-isop.), 1.35 (s, 3H, CH3-isop.).


## 3.4. 5,6-O-Isopropyliden-1,2-O-(R)-trichloroethylidene-3-O-(2′,3′-epoxypropan-1′-yl)-α-D-glucofuranose (2)

Epichlorohydrin (20 mL, 256 mmol) was stirred with aq NaOH (50%, 1.25 mL) and tetrabutylammonium bromide (0.5 g, 1.55 mmol) for 30 min. 5,6-O-Isopropyliden-1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (1) (2 g, 5.8 mmol) was added slowly at approximately 5°C under stirring and the reaction was continued at the same temperature for 3 hours, followed by additional 12 hours at room temperature. The reaction mixture was poured over crushed ice and extracted with EtOAc (4
×
10 mL); the organic layer was neutralized with aqueous saturated sodium hydrogen carbonate and washed with distilled water (2
×
5 mL) and dried over anhydrous Na2SO4 and filtered. The filtrate was concentrated to give syrup. The syrup was crystallized from hot hexane at 0°C to give the pure compound2 (1.75 g, 76%), m.p. 101-102°C, [
α
]
D
25
-
0.20 (c 1, CH2Cl2). 1H NMR (CDCl3, 400 MHz): δ 6.05 (d, 1H, J
1
,
2 4.0 Hz, H-1), 5.28 (s, 1H, HCCl3), 4.74 (d, 1H, H-2), 4.65 (m, 1H, H-5), 4.48 (dd, 1H, J
4
,
5 2.8 Hz, H-4), 4.32 (br d, 1H, J
3
,
4 3.2 Hz, H-3), 4.16 (dd, 1H, J
6
a
,
6
b 8.8, J
5
,
6
a 6.4 Hz, H-6a), 3.96 (dd, J
5
,
6
b 5.2 Hz, H-6b), 3.92 (two sets of dd, 1H, J
1
′
,
2
′ 6.4 Hz, H-1′), 3.13 (m, 1H, H-2′), 2.80 (two sets of dd, 1H, J
2
′
,
3
′ 11.6 Hz, H-3′), 1.39 (s, 3H, CH3-isop.), 1.33 (s, 3H, CH3-isop.).


## 4. Conclusions

Two compounds, 5,6-O-isopropylidene-1,2-O-(R)-trichloroethylidene-α-D-glucofuranose (compound1) and the new compound, 5,6-O-isopropylidene-1,2-O-(R)-trichloroethylidene-3-O-(2′,3′-epoxypropan-1′-yl)-α-D-glucofuranose (compound2), were synthesized and characterized by FTIR, 1H NMR, and TG-DTA techniques. The thermal degradation of compounds1 and2 in nitrogen is a one-stage reaction according to thermogram. The thermal degradation kinetics of the compounds were evaluated using the KAS and Tang methods. The average activation energies calculated by the KAS method were found to be 96 kJ mol−1 for compound1 and 69 kJ mol−1 for compound2, respectively, while they were found to be 113 kJ mol−1 for compound1 and 87 kJ mol−1 for compound2 by the Tang method. Thus, it is concluded that thethermal degradation of compound2 is found to be more favorable in comparison to that of compound1.The activation energies of the compounds as a function of degree of conversion showed that the compounds degraded in two steps. In the first step which is up to 80% conversion,E remained almost constant. In the second step, which is between 80 and 100% conversion, E increased. It is also concluded that thethermal degradation mechanisms of compound1 and compound2 exhibit similar behavior. Since the new compound (2) exhibits lower thermal degradation characteristics compared to compound (1) without the epoxy ring, it is possible that this could affect the properties of the polymers synthesized using this as a potential monomer.



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*Source: 737953-2014-09-09.xml*