US3355050A - Lunar cryostat - Google Patents
Lunar cryostat Download PDFInfo
- Publication number
- US3355050A US3355050A US39396964A US3355050A US 3355050 A US3355050 A US 3355050A US 39396964 A US39396964 A US 39396964A US 3355050 A US3355050 A US 3355050A
- Authority
- US
- United States
- Prior art keywords
- stack
- dish
- cryostat
- lunar
- members
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 230000002745 absorbent Effects 0.000 claims description 4
- 239000002250 absorbent Substances 0.000 claims description 4
- 230000005855 radiation Effects 0.000 claims description 4
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 239000011888 foil Substances 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000002985 plastic film Substances 0.000 description 1
- 229920006255 plastic film Polymers 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
- F17C3/085—Cryostats
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
- F17C2270/0509—"Dewar" vessels
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/901—Liquified gas content, cryogenic
Definitions
- the present invention relates to a cryostat which may be employed in the vacuum and other conditions found on the moon. It is therefore a primary object of my invention to provide such a cryostat.
- FIGURE 1 is a perspective view of a cryostat made as herein taught
- FIGURE 2 is a side view thereof.
- FIGURE 3 is a top view.
- the present device consists of a plurality of dishshaped insulation-reflector shields which are stacked in the form of an appropriate unit member and wherein the individual members of the stack are separated from each other by legs or other separation elements made of materials characterized by high thermal insulation properties.
- metallized plastic films of irregular crinkling could be. used which would eliminate the need for such separation elements.
- the essential feature of my cryostat is to provide for shielding against re-radiated heat from the moon surface and further shielding against higher elevational structures such as mountains which may surround the area in which such device is being used. At the same time the device must be so made as to progressively minimize the radiation of heat to successive dish structures above in the stack.
- the device is to be used during the lunar night. In the vacuum of the lunar atmosphere and during the lunar night the only source of heat to be shielded against is the radiated heat of the moon itself. If it is deemed desirable, surface shielding may also be used above the device to cover against remote radiation from the earth (or from the impact of micrometeoritea) although the device will function better on the side of the moon opposed to the earth.
- a lunar cryostat comprising in combination: a nesting stack of a plurality of spaced upwardly concave dishshaped members, each of said dish-shaped members being characterized by a diametrical curvature adequate to block lateral thermal radiation from entering the innermost portion thereof, each of said members having its convex surface highly reflective to radiant heat and its opposed concave surface highly absorbent to radiant heat, said stack being formed so as to have all like surfaces facing in the same direction and to have a convex heat reflecting surface at the bottom of said stack and wherein the top of said stack and the spaces between each of said dish-shaped members are open to ambient environment, and thermal insulating means separating the dish-shaped members of said stack from each other.
- cryostat as defined in claim 1 wherein said thermal insulating means are leg-like structures.
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Packages (AREA)
Description
Nov. 28, 1967 N. P. RUZIC 3,355,050
LUNAR CRYOSTAT Filed Sept. 2, 1964 INVENTOR.
NEIL P RUZ/C BY M United States Patent Ofihce 3,355,050 LUNAR CRYOSTAT Neil P. Ruzic, Beverly Shores, Ind. 46301 Filed Sept. 2, 1964, Ser. No. 393,969 3 Claims. (Cl. 2209) The present invention relates to a cryostat which may be employed in the vacuum and other conditions found on the moon. It is therefore a primary object of my invention to provide such a cryostat.
It is known that temperatures approaching absolute zero, that is below 20 K. is extremely useful for both cryogenic research and for manufacturing and processing techniques under cryogenic conditions. By the device of the present invention it is possible readily to achieve and maintain such low temperatures on the moon at night.
In the drawings appended hereto:
FIGURE 1 is a perspective view of a cryostat made as herein taught;
FIGURE 2 is a side view thereof; and
FIGURE 3 is a top view.
The present device consists of a plurality of dishshaped insulation-reflector shields which are stacked in the form of an appropriate unit member and wherein the individual members of the stack are separated from each other by legs or other separation elements made of materials characterized by high thermal insulation properties. Alternatively, metallized plastic films of irregular crinkling could be. used which would eliminate the need for such separation elements.
The essential feature of my cryostat is to provide for shielding against re-radiated heat from the moon surface and further shielding against higher elevational structures such as mountains which may surround the area in which such device is being used. At the same time the device must be so made as to progressively minimize the radiation of heat to successive dish structures above in the stack.
The device is to be used during the lunar night. In the vacuum of the lunar atmosphere and during the lunar night the only source of heat to be shielded against is the radiated heat of the moon itself. If it is deemed desirable, surface shielding may also be used above the device to cover against remote radiation from the earth (or from the impact of micrometeoritea) although the device will function better on the side of the moon opposed to the earth.
The device consists of a series of dish-shaped members 11 which are separated from each other by the separating means 12. Each dish may be made of materials such as thin sheet aluminum, aluminum foil, or other materials of high radiant heat reflectance or plastic-coated alu- 3,355,050 Patented Nov. 28, 1967 minum or similar materials. The high reflecting surface is provided on the bottom surface of the shield, whereas a heat absorbent surface is provided on the top face thereof. To provide absorbent surface on the top face the shield is most preferably made black.
To operate the device is most simple. One need only to provide an appropriate number of stacks 11 separated by the elements 12 in the vacuum environment of a lunar surface and place the material 13 to be treated at the cryogenic temperatures in the center portion on the top of the uppermost shield. The temperature required for treatment may be varied by the number of shields which are employed.
It will be understood that various modifications and variations may be effected without departing from the spirit or scope of the novel concepts of my invention.
I claim as my invention:
1. A lunar cryostat comprising in combination: a nesting stack of a plurality of spaced upwardly concave dishshaped members, each of said dish-shaped members being characterized by a diametrical curvature adequate to block lateral thermal radiation from entering the innermost portion thereof, each of said members having its convex surface highly reflective to radiant heat and its opposed concave surface highly absorbent to radiant heat, said stack being formed so as to have all like surfaces facing in the same direction and to have a convex heat reflecting surface at the bottom of said stack and wherein the top of said stack and the spaces between each of said dish-shaped members are open to ambient environment, and thermal insulating means separating the dish-shaped members of said stack from each other.
2. The cryostat as defined in claim 1 wherein said thermal insulating means are leg-like structures.
3. The cryostat as defined in claim 1 wherein said thermal insulating means are integral with said dish-shaped members.
References Cited UNITED STATES PATENTS 1,956,356 4/1934 Justheim 22010 1,964,795 7/ 1934 Frary 2209 2,037,813 4/ 1936 Munters 2209 2,053,252 9/1936 Cook et al 220-9 2,119,438 5/1938 OLeary 2209 2,196,373 4/ 1940 Wallach 2209 3,018,016 3/1965 Hnilicka 22015 FOREIGN PATENTS 248,527 11/ 1963 Australia.
THERON E. CONDON, Primary Examiner. JAMES R. GARRETT, Examiner.
Claims (1)
1. A LUNAR CRYOSTAT COMPRISING IN COMBINATION: A NESTING STACK OF A PLURALITY OF SPACED UPWARDLY CONCAVE DISHSHAPED MEMBERS, EACH OF SAID DISH-SHAPED MEMBERS BEING CHARACTERIZED BY A DIAMETRICAL CURVATURE ADEQUATE TO BLOCK LATERAL THERMAL RADIATION FROM ENTERING THE INNERMOST PORTION THEREOF, EACH OF SAID MEMBERS HAVING ITS CONVEX SURFACE HIGHLY REFLECTIVE TO RADIANT HEAT AND ITS OPPOSED CONCAVE SURFACE HIGHLY ABSORBENT TO RADIANT HEAT, SAID STACK BEING FORMED SO AS TO HAVE ALL LIKE SURFACES FACING IN THE SAME DIRECTION AND TO HAVE A CONVEX HEAT REFLECTING SURFACE AT THE BOTTOM OF SAID STACK AND WHEREIN THE TOP OF SAID STACK AND THE SPACES BETWEEN EACH OF SAID DISH-SHAPED MEMBERS ARE OPEN TO AMBIENT ENVIRONMENT, AND THERMAL INSULATING MEANS SEPARATING THE DISH-SHAPED MEMBERS OF SAID STACK FROM EACH OTHER.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US39396964 US3355050A (en) | 1964-09-02 | 1964-09-02 | Lunar cryostat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US39396964 US3355050A (en) | 1964-09-02 | 1964-09-02 | Lunar cryostat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3355050A true US3355050A (en) | 1967-11-28 |
Family
ID=23556995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US39396964 Expired - Lifetime US3355050A (en) | 1964-09-02 | 1964-09-02 | Lunar cryostat |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3355050A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6634519B2 (en) * | 2000-05-26 | 2003-10-21 | L'air Liquide - Societe Anonyme A Directoire Et Conseil De Surveillance Pour L'etude Et L'exploitation Des Procedes Georges Claude | Method for manufacturing a tank for a cryogenic fluid and tank thus produced |
| WO2023099837A1 (en) * | 2021-12-02 | 2023-06-08 | Airbus Defence And Space Sas | Cryostat for a space component |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1956356A (en) * | 1933-09-11 | 1934-04-24 | Clarence I Justheim | Insulated dish |
| US1964795A (en) * | 1931-01-16 | 1934-07-03 | Aluminum Co Of America | Refrigerating unit |
| US2037813A (en) * | 1932-04-04 | 1936-04-21 | Termisk Isolation Ab | Heat insulation |
| US2053252A (en) * | 1930-11-25 | 1936-09-08 | Gen Motors Corp | Refrigerating apparatus |
| US2119438A (en) * | 1933-11-28 | 1938-05-31 | William C O'leary | Vacuum wall receptacle |
| US2196373A (en) * | 1935-08-07 | 1940-04-09 | American Flange And Mfg Compan | Refrigerator structure and insulation therefor |
| US3018016A (en) * | 1959-09-24 | 1962-01-23 | Nat Res Corp | Vacuum device |
-
1964
- 1964-09-02 US US39396964 patent/US3355050A/en not_active Expired - Lifetime
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2053252A (en) * | 1930-11-25 | 1936-09-08 | Gen Motors Corp | Refrigerating apparatus |
| US1964795A (en) * | 1931-01-16 | 1934-07-03 | Aluminum Co Of America | Refrigerating unit |
| US2037813A (en) * | 1932-04-04 | 1936-04-21 | Termisk Isolation Ab | Heat insulation |
| US1956356A (en) * | 1933-09-11 | 1934-04-24 | Clarence I Justheim | Insulated dish |
| US2119438A (en) * | 1933-11-28 | 1938-05-31 | William C O'leary | Vacuum wall receptacle |
| US2196373A (en) * | 1935-08-07 | 1940-04-09 | American Flange And Mfg Compan | Refrigerator structure and insulation therefor |
| US3018016A (en) * | 1959-09-24 | 1962-01-23 | Nat Res Corp | Vacuum device |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6634519B2 (en) * | 2000-05-26 | 2003-10-21 | L'air Liquide - Societe Anonyme A Directoire Et Conseil De Surveillance Pour L'etude Et L'exploitation Des Procedes Georges Claude | Method for manufacturing a tank for a cryogenic fluid and tank thus produced |
| WO2023099837A1 (en) * | 2021-12-02 | 2023-06-08 | Airbus Defence And Space Sas | Cryostat for a space component |
| FR3129924A1 (en) * | 2021-12-02 | 2023-06-09 | Airbus Defence And Space Sas | cryostat for a space component |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4560850A (en) | Container with steam port for use in microwave ovens | |
| EP0511177B1 (en) | A protective vessel for a getter material | |
| US3012895A (en) | Food package | |
| ES2050713T3 (en) | MICROWAVE RECEIVING HEATING SHEETS AND CONTAINING CONTAINERS. | |
| RU96107250A (en) | HEAT INSULATION PANEL AND METHOD OF HEAT INSULATION WITH ITS APPLICATION | |
| WO1983000476A1 (en) | Lid for receptacle | |
| US3355050A (en) | Lunar cryostat | |
| GB1182048A (en) | Electric Infrared Heater | |
| US3285411A (en) | Receiving, storing, and ripening device for one or more perishable food objects | |
| JPH0356719Y2 (en) | ||
| FR2016135A1 (en) | Food slice portion pack with film separators | |
| ES478762A1 (en) | Storage Vessels | |
| JPH0642860A (en) | Heat insulator | |
| JP3513006B2 (en) | Electric water heater | |
| US4417566A (en) | Solar oven access door | |
| JP2019158134A (en) | Heat insulation material and heat insulation method for battery | |
| US3219798A (en) | Heated lunch box | |
| CN2220213Y (en) | Thermal insulation stewing device | |
| FR2424196A1 (en) | MULTI-COMPARTMENT CONTAINER | |
| JPS6331960Y2 (en) | ||
| US3687331A (en) | Cook ware container cover | |
| JPS5682348A (en) | Solar heat collector | |
| GB882148A (en) | Improvements in and relating to the cooling of material | |
| US3380614A (en) | Thermal insulation under vacuum | |
| US3397773A (en) | Special package |