Claims
- 1. Process for the catalytic codimerization of norbornadiene with acrylonitrile comprising:
- (a) contacting norbornadiene and acrylonitrile in the presence of a catalytic amount of a three-component homogeneous catalytic system consisting of nickel acetylacetonate, triphenylphosphine and an alkyl aluminum chloride selected from the group consisting of diethylaluminum chloride, ethyl aluminum dichloride and ethyl aluminum sesquichloride;
- (b) having the contacting occurring at a temperature within the range between from about -20.degree. C to about 100.degree. C; and
- (c) continuing the contacting until a norbornadiene-acrylonitrile codimer having the following structure ##STR4## is prepared.
- 2. Process according to claim 1 wherein the triphenylphosphine to the acetylacetonate mole ratio is in the range between from about 0.1 to about 100.
- 3. Process according to claim 1 wherein the norbornadiene to acrylonitrile mole ratio is in the range between from about 0.1 to about 20.
- 4. Process according to claim 1 wherein the norbornadiene to the acetylacetonate mole ratio is in the range between from about 10 to about 2000.
- 5. Process according to claim 1 wherein the alkyl aluminum chloride to the acetylacetonate mole ratio is in the range between from about 1 to about 100.
- 6. Process according to claim 5 wherein an inert solvent is present.
- 7. Process according to claim 6 wherein the inert solvent is selected from the group consisting of aromatic hydrocarbon, cycloparaffin, cycloolefin, ether, halogenated aromatic, halogenated paraffin and halogenated cycloparaffin.
- 8. Process according to claim 7 wherein the triphenylphosphine to the acetylacetonate mole ratio is in the range between from about 0.1 to about 100.
- 9. Process according to claim 8 wherein the alkyl aluminum chloride to the acetylacetonate mole ratio is in the range between from about 1 to about 100.
- 10. Process according to claim 9 wherein the norbornadiene to the acrylonitrile mole ratio is in the range between from about 0.1 to about 20.
BACKGROUND OF THE INVENTION
The invention herein described was made in the course of or under a contract thereunder with the United States Air Force Systems Command.
US Referenced Citations (6)
Non-Patent Literature Citations (1)
Entry |
Noyori, et al., J.A.C.S., 97:4 (2-19-75) pp. 812-820. |