. An annotated bibliography of patents related to coastal engineering. Patents; Coastal engineering. NOVEMKEK 26, 1974 GENERAL AND MECHANICAL 1447 3,849,988 COM8LSTION CHAMBtRS FOR rNTERNAL COMBUSTION ENGIVKS KQl' WITH A TtRBO-COMPKKSSOR LIMT WITH RKIIKATINC UPSTKbAM OK Tilt ll RBINb Jean Melchior, Paris, France, a^si>>nor to Ktat FrancaU, Paris, France Filed Mar. 29. 1973. Ser. No. Claim] prloril;, applicalitjn France, Apr. 6, 1972. int. CI. F» CI. 60-606 21 culms 3,849,989 INFLATABLE BARRIER FOR FLOATING ON WATtR Paul Prcus, Box 1002. Tom
. An annotated bibliography of patents related to coastal engineering. Patents; Coastal engineering. NOVEMKEK 26, 1974 GENERAL AND MECHANICAL 1447 3,849,988 COM8LSTION CHAMBtRS FOR rNTERNAL COMBUSTION ENGIVKS KQl' WITH A TtRBO-COMPKKSSOR LIMT WITH RKIIKATINC UPSTKbAM OK Tilt ll RBINb Jean Melchior, Paris, France, a^si>>nor to Ktat FrancaU, Paris, France Filed Mar. 29. 1973. Ser. No. Claim] prloril;, applicalitjn France, Apr. 6, 1972. int. CI. F» CI. 60-606 21 culms 3,849,989 INFLATABLE BARRIER FOR FLOATING ON WATtR Paul Prcus, Box 1002. Toms River. NJ. 08753 Filed May 25. 1973. Ser. No. Inl. CI, t02b JW. lflU4 U,S. CL6I-IF 4 Claims. 1, A floating barrier for substances floating on water com- prising: a floatation means including pluralit> of inflatuhle chambers hingeJty connected in end to end relationship, each of said chambers being divided into plural independent subchambers by flexible wall means disposed therein and liquid impervious skirt means depending from said flou- tion means to provide a liquid barrier below the water line thereof. 3, ANTI-HEAVE PROTECTIVE SYSTEM Jacques Eduuard Lamy. Fonlenav-Aux-Roses. France, as- signor to C. G. Doris (Compagnie Generate pour les De%e- loppements Opemtlnnnels des Richesses ). Paris. France Filed Jan. 17. 1973. Ser. No. Claims priority, application France, Jan. 18, 1972. Inl, CI. E02b JI06 U,S, CI. 61-3 II Claims 1, Combustion chamber for a turbo-compressor unit associ- ated with an internal combustion engine operable for reheat- ing gases upstream of the turbine of said lurbo-compressor unit, said combustion chamber being adapted to be supplied with fuel and at the same llmeliy exhaust gases emerging from the engine and by fresh air taken through a bypass pipe con- nected between the outlet of the compressor and the inlet of said turbine of said turbo-compressor unit in bypass relation to the engine, said combustion
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