Process for recovering energy from liquefied gases

• US 3,992,891 A
• Filed: 02/18/1975
• Issued: 11/23/1976
• Est. Priority Date: 02/16/1974
• Status: Expired due to Term

• Current Assignee: Linde AG (Linde Plc)
• Original Assignee: Linde AG (Linde Plc)
• Inventors: Pocrnja, Anton
• Primary Examiner(s): Wayner, William E.
• Assistant Examiner(s): Capossela, Ronald C.
• Application Number:
  US05/550,590
• Time in Patent Office: 644 Days
• Field of Search: 62/52, 62/53, 62/86, 62/87, 62/88, 62/401, 62/402, 62/403, 60/648, 60/650, 60/651, 60/671, 60/682, 60/684
• US Class Current: 62/50.3
• CPC Class Codes: F02C 7/143 before or between the compressor stages
• CPC Class Codes: F17C 2265/05 Regasification
• CPC Class Codes: F17C 9/04 Recovery of thermal energy
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

In a process for recovering the energy from a liquefied gas by evaporation in heat exchange with a cycle medium which is simultaneously cooled, said cycle medium being thereafter compressed, heated, subjected to engine expansion and recovered in a cyclical manner, wherein the improvement comprises operating the cycle so that the cycle medium remains in the gaseous phase throughout the entire cycle.

Claims

1. In a process for recovering the energy from a liquefied gas by evaporation in heat exchange with a closed cycle medium which is simultaneously cooled, said cycle medium being thereafter compressed, heated by indirect heat exchange, subjected to engine expansion and recovered in a cyclical manner,

the cycle being operated so that the cycle medium remains in the gaseous phase through the entire cycle,

wherein the improvement comprises further heating resultant vaporized liquefied gas in indirect heat exchange with said cycle medium after said cycle medium has been engine expanded but before being cooled, and thereafter engine expanding the resultant further heated vaporized liquid.

2. A process according to claim 1, the improvement further comprising heating the cycle medium in part by supplying external heat and in part by heat exchange with itself after expansion thereof.

3. A process according to claim 1, the improvement further comprising maintaining the pressure of the cycle medium just prior to compression at between 1 and 20 bars and just after compression between 15 and 60 bars.

4. A process according to claim 3, the improvement further comprising maintaining the temperature of the cycle medium prior to the engine expansion between 800 and 1300 K, and prior to compression, at about the temperature of the liquefied gas to be evaporated.

5. A process according to claim 1, wherein the cycle medium is air.

6. A process according to claim 1, wherein air is employed as the cycle medium.

7. A process according to claim 1, wherein said liquefied gas is liquefied natural gas.

8. Apparatus for evaporating and further heating liquefied gas comprising:

A. main heat exchanger for the evaporation of liquefied gas, said main heat exchanger having a first flow cross section for evaporating liquefied gas and a second flow cross section for a gaseous medium;

B. gas compressor for compressing said gaseous medium, arranged downstream of said second flow cross section of said main heat exchanger;

C. recuperator for recovering heat of compression of said gaseous medium, arranged downstream of said gas compressor, said recuperator having a first flow cross section for receiving hot gas from said compressor and a second flow cross section for heating said gaseous medium to be sent to said main heat exchanger;

D. heater means for heating said gas medium leaving said first flow cross section of said recuperator, said heater means being indirect heat exchange means heated by external heat;

E. expansion turbine for expanding heated gaseous medium and arranged downstream of said heater means;

F. supplemental heat exchanger for further heating evaporated liquefied gas, said supplemental heat exchanger including a first flow cross section for evaporated liquefied gas and a second flow cross section for cooling resultant expanded gaseous medium, said second flow cross section arranged downstream of said expansion turbine and upstream of said recuperator; and

conduit means for effecting communication between components A, B, C, D, E, F as a closed cycle between A and F for the liquefied gas.

9. Apparatus according to claim 8, comprising a further expansion turbine for expanding said further heated expanded liquefied gas, arranged downstream of said first flow cross section of said supplemental heat exchanger, and conduit means for effecting communication between said first flow cross section and said further expansion turbine.