US3261180A - Cooler unit - Google Patents
Cooler unit Download PDFInfo
- Publication number
- US3261180A US3261180A US9996A US999660A US3261180A US 3261180 A US3261180 A US 3261180A US 9996 A US9996 A US 9996A US 999660 A US999660 A US 999660A US 3261180 A US3261180 A US 3261180A
- Authority
- US
- United States
- Prior art keywords
- compartment
- container
- tube
- compartments
- exhaust tube
- 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
- 239000002826 coolant Substances 0.000 claims description 30
- 239000007788 liquid Substances 0.000 claims description 24
- 238000012856 packing Methods 0.000 claims description 12
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 8
- 238000001816 cooling Methods 0.000 description 8
- 238000005192 partition Methods 0.000 description 6
- 239000004065 semiconductor Substances 0.000 description 6
- 239000010956 nickel silver Substances 0.000 description 5
- 230000002093 peripheral effect Effects 0.000 description 5
- 239000011491 glass wool Substances 0.000 description 4
- 239000000377 silicon dioxide Substances 0.000 description 4
- 240000007711 Peperomia pellucida Species 0.000 description 3
- 238000009835 boiling Methods 0.000 description 3
- 239000011521 glass Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- VOPWNXZWBYDODV-UHFFFAOYSA-N Chlorodifluoromethane Chemical compound FC(F)Cl VOPWNXZWBYDODV-UHFFFAOYSA-N 0.000 description 2
- 229910000531 Co alloy Inorganic materials 0.000 description 2
- KGWWEXORQXHJJQ-UHFFFAOYSA-N [Fe].[Co].[Ni] Chemical compound [Fe].[Co].[Ni] KGWWEXORQXHJJQ-UHFFFAOYSA-N 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- PXBRQCKWGAHEHS-UHFFFAOYSA-N dichlorodifluoromethane Chemical compound FC(F)(Cl)Cl PXBRQCKWGAHEHS-UHFFFAOYSA-N 0.000 description 2
- 235000019404 dichlorodifluoromethane Nutrition 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 239000003507 refrigerant Substances 0.000 description 2
- 210000002268 wool Anatomy 0.000 description 2
- 240000008042 Zea mays Species 0.000 description 1
- 235000005824 Zea mays ssp. parviglumis Nutrition 0.000 description 1
- 235000002017 Zea mays subsp mays Nutrition 0.000 description 1
- AFYPFACVUDMOHA-UHFFFAOYSA-N chlorotrifluoromethane Chemical compound FC(F)(F)Cl AFYPFACVUDMOHA-UHFFFAOYSA-N 0.000 description 1
- 235000005822 corn Nutrition 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 235000020004 porter Nutrition 0.000 description 1
- 230000035945 sensitivity Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L23/00—Details of semiconductor or other solid state devices
- H01L23/34—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
- H01L23/46—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements involving the transfer of heat by flowing fluids
- H01L23/473—Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements involving the transfer of heat by flowing fluids by flowing liquids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25D—REFRIGERATORS; COLD ROOMS; ICE-BOXES; COOLING OR FREEZING APPARATUS NOT OTHERWISE PROVIDED FOR
- F25D7/00—Devices using evaporation effects without recovery of the vapour
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L2924/00—Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
- H01L2924/0001—Technical content checked by a classifier
- H01L2924/0002—Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
Definitions
- This invention relates to cooling and seeks to provide a cooler unit having the capability of cooling, adapted, upon operation, rapidly to cool an object of small thermal inertia in thermal contact with the unit and to maintain a low temperature for a limited period of time.
- Such an object may be, for example, a semiconductor detector of infrared radiations.
- a semiconductor detector of infrared radiations To increase the sensi tivity of detection, it is advantageous to cool the semiconductor below 0 C. and preferably to a temperature below -30 C. To prevent false indications due to subsequent temperature rise of the semiconductor, it is also advantageous to maintain the low temperature at least for the operative period of detection.
- a cooler unit having the capability of cooling comprises a temporarily sealed container divided into two compartments, filled or substantially filled with liquid coolant, an open transfer tube for coolant extending between the two compartments, a temporarily sealed exhaust tube leading from one compartment, means to open the exhaust tube external to the container, and a liquid-restrictive packing through which coolant passes to escape from the exhaust tube.
- the packing is contained in the one compartment from which the exhaust tube leads.
- Suitable packings are, for example, silica wool and glass wool.
- the transfer tube is restrictive compared to the exhaust tube.
- the transfer tube may be narrow throughout its length or contain a narrow restriction. It may, alternatively, incorporate both forms of restriction.
- the transfer tube may extend from that end or from a position adjacent that end.
- the end of the transfer tube may be secured to that end and have side apertures for the passage of coolant.
- the transfer tube may extend to a position adjacent the end of the other compartment remote from that end of the one compartment.
- the exhaust tube may lead from a position adjacent that end of the one compartment.
- the container may have a common dividing wall through which the transfer tube extends.
- the exhaust tube may also extend through the common dividing wall.
- the means to open the exhaust tube may include a frangible portion external to the container.
- FIGURE 1 is a longitudinal cross section of one embodiment of a cooler unit according to the invention in combination with a detector cell;
- FIGURE 2 is a cross section on the line IIII of FIG- URE 1;
- FIGURE 3 is a cross section on the line III-III of FIGURE 2;
- FIGURE 4 is a cross section on the line IVIV of FIGURE 2.
- FIGURE 5 is a cross section of a second embodiment of cooler unit according to the invention.
- the detector cell shown in FIGURES l to 4 comprises a cylindrical envelope of iron-nickel-cobalt alloy formed in two parts 10 and 11.
- the part 10 is in the shape of a top hat and has a closed end 12 and a radial flange 13 by which the combined unit and cell can be mounted.
- the part 11 is an open-ended cylinder which fits into and is sealed to the part 10 at one end and has its other end closed by a transparent closure 14. Electrical leads 15 pass through seals 16 in the part 10 and are connected to i4semiconductor/detector mounted adjacent the closure
- the cell so far described does not form part of this invention but is merely one example of an object of small thermal inertia to which the invention is applicable.
- the cooler unit 20 comprises a container formed in two cylindrical parts 21 and 22 of iron-nickel-cobalt alloy.
- the part 21 has a closed end 23 and is longer and of slightly smaller diameter than the part 22.
- the part 22 has a closed end 24 and the parts 21 and 22 are inte-rfitted and sealed.
- the semiconductor detector is mounted on the closed end 23 in close proximity to the closure 14.
- a metal diaphragm 25 is secured across the part 21 to divide the container into two compartments 26 and 27 separated by a common dividing wall.
- An open metal transfer tube 28 extends through a sealed aperture in the diaphragm 25 and affords communication between the compartments 26 and 27.
- the tube 28 has its one end secured to the central part of the end 23 on the opposite side to the detector.
- a diametrical slot 29 (FIGURES 3 and 4) is formed in the one end of the tube 28 and prevents closure of that end.
- the other end of the tube 28 is open and located adjacent the end 24 of the compartment 27 remote from the end 23 of the compartment 26.
- An exhaust tube 30 also extends through a sealed aperture in the diaphragm 25 and has one open end adjacent the end 23 of the compartment 26. Inside the compartment 27, the tube 30 is bent and passes radially through a German silver bush 31 in a peripheral hole in the part 22 and a similar aligned bush in a peripheral hole in the part 10. Communication betwen the compartment 26 and the exterior of the detector cell is thus alforded, all the connections being sealed. Secured on the end of the tube 30 outside the cell is an externally threaded sleeve 33 of German silver.
- the compartment 26 also contains a packing 38 of silica or glass Wool.
- a second pair of aligned German silver bushes 34 and 35 (FIGURES 2 and 4) are mounted in peripheral holes in the parts 10 and 22.
- a short inlet pipe 36 is sealed into the bushes 34 and 35 and affords communication between the compartment 27 and the exterior of the detector cell.
- An externally threaded sleeve 37 of German silver is secured on the end of the pipe 36 outside the cell.
- the cooler unit 20 is accurately located and mounted within the cell by the pipe 36 and tube 30.
- the transfer tube 28 is narrow and the slot 29 small so as to set up a restriction to the passage of coolant as compared to the exhaust tube 30 which is comparatively wide.
- the cooler unit is filled with liquid coolant, such as Freon 13, Freon 22, or Freon 12, which boils at a desired low temperature at an ambient pressure corresponding to that likely to be encountered when cooling is required.
- liquid coolant such as Freon 13, Freon 22, or Freon 12
- coolant is used in this sense.
- the filling takes place through the inlet pipe 36, and after the compartment 27 is full, liquid passes through the transfer tube' 28 into the compartment 26. After the compartment 26 is full, liquid emergesthrough the exhaust tube 30.
- the exhaust tube 30 is then sealed with a frangible seal, for example in the form of a glass bulb 38'.
- the inlet pipe is then sealed.
- the frangible glass bulb is broken by release of a conventional detent-held spring-urged plunger 39. There is an immediate fiow of coolant through the exhaust tube 30 from the compartment 26 due to the pressure in the unit 20 and boiling of the liquid coolant.
- the duration of the limited period of time during which cooling is maintained is largely determined by the amount of liquid coolant left in the container after the initial rapid cooling caused by the rapid escape of coolant through the exhaust tube.
- the escaping coolant should be in the form of vapour and the silica or glass wool packing assists towards this.
- the wool acts as a liquidrestrictive packing and traps much of the liquid which would, in its absence, It will be under stood that other materials may be used inert to the coolant and such as to present a difiicult path for liquid whilst permitting passage of vapour.
- the detector is similar to that shown in FIGURES 1 to 4, and parts "of the cooler unit similar to those in FIGURES 1 to 4 carry the same reference numerals.
- an exhaust tube 40 extends through a sealed aperture in the diaphragm 25 and has its one end secured to the central part of the end 23 on the opposite side to the detector.
- a side aperture 41 is formed in the one end of the tube 40 and prevents closure of that end.
- the tube 40 is bent and passes radially through a German silver bush 31 in a peripheral hole in the part 22 and a similar aligned bush 32 in a peripheral hole in the part 10. Communication between the compartment 26 and the exterior of the detector cell is thus afforded, all the connections being sealed.
- a metal transfer tube 42 extends through another sealed aperture in the diaphragm 25 to afford communication between the compartments 26 and 27 and has its one end secured to the central part of the end 23 on the opposite side to the detector.
- a side aperture 43 is formed in the one end of the tube 28 and prevents closure of that end.
- the other end of the tube 42 is bent around the exhaust tube 40 in the compartment 27 so that its open end remote from the end 23 of the corn partment 26 lies centrally of the unit.
- the exhaust tube 40 and transfer tube 42 are brazed together in heat exchange relationship along their lengths.
- the compartments 26 and 27 also contain packings 44 and 45 of silica or glass wool.
- the transfer tube 42 is narrow so as to set up a restriction to the passage of coolant as compared to the exhaust tube 40, which is comparatively wide.
- the cooler unit is filled with liquid coolant, such as Freon 1'3, Freon 22, or Freon 12, which boils at a desired low temperature at an ambient pressure corresponding to that likely to be encountered when cooling it required.
- liquid coolant such as Freon 1'3, Freon 22, or Freon 12
- the filling takes place in the same manner as with the first embodiment, and the exhaust tube 40 is then sealed with a frangible seal, for example in the form of the glass bulb 38.
- the container of the unit is now sealed and substantially filled with liquid coolant under a pressure equal to the vapor pressure of the coolant at the highest ambient temperature likely to be encountered in order to prevent expansion problems.
- the detector cell is evacuated as thoroughly as possible.
- the central location of the transfer tube assists passage of cool-ant even under high rotational accelerations.
- the side apertures 41 and 43 are disposed in different directions to improve the flow of coolant past the end to be cooled.
- the flow of cold vapor through the exhaust tube helps to cool the coolant passing along the transfer tube.
- the evacuation of the cell surrounding the cooler unit is advantageous as this thermally isolates the unit from its surroundings except for the inlet and exhaust tubes.
- the arrangement of the two compartments, the transfer tube and the exhaust tube, enables the cooler unit to operate in any spatial position and under considerable acceleration forces.
- the unit, once sealed, is capable of storage over a long period of time and subsequent use.
- a cooler unit comprising a sealed container divided into two compartments, liquid coolant in each compartment, a transfer tube within the container extending between the two compartments and placing the compartments in communication with each other, a liquid flow restricting packing in at least one of said compartments, an exhaust tube connecting said one compartment to the exterior of said container, said tube extending through the other compartment of said container and means normally closing the exhaust tube and operable to place the interior of said one compartment in communication with the exterior of said container, said transfer tube having a means positioned on the end extending into said one compartment to restrict the flow therethrough relative to the flow afforded to the exhaust tube.
- a cooler unit according to claim 1 including a closable inlet pipe opening from the exterior of said container to the interior of the other of said two compartments.
- a cooler unit comprising a sealed container having a wall portion to be cooled, a partition within said container dividing said container into two compartments, liquid coolant in each compartment, said wall portion being associated with and at least partly bounding one of said compartments, a liquid flow restricting packing in at lea-st said one compartment, an exhaust tube connecting the interior of said one compartment to the exterior of the container, said tube extending through the other compartment of said container, means norm-ally closing said exhaust tube externally of said container and operable to place the interior of said one compartment in communication with the exterior of said container and a transfer tube extending through said partition in a liquid-tight manner permanently to place said two compartments in communication with each other, said transfer tube having a means positioned on the end extending into said one compartment to restrict the flow of fluid therethrough relative to the flow afforded to the exhaust tube.
- a cooler unit comprising a sealed container having a wall portion to be cooled, a partition within said container dividing said container into two compartments, liquid cool-ant in each compartment, said wall portion being associated with and bounding one of said compartments, at liquid flow restricting packing in at least said one compartment, an exhaust tube connecting the exterior of said container through the other of said two compartments and through said partition in a liquidtight manner to the interior of said one compartment, frangi'ble closure means normally closing said exhaust tube externally of said container and a transfer tube extending through said partition in a liquid-tight manner permanently to place said other compartment in communication with said one compartment at a location adjacent to said wall portion, said transfer tube having a means positioned on the end extending into said one compartment to restrict the flow of fluid therethrough relative to the flow afforded to the exhaust tube.
- a cooler unit according to claim 5 wherein said other compartment is shaped to be substantially symmetrical about an axis and said transfer tube opens to said other compartment on said axis and is connected to said exhaust tube in heat exchange relationship.
- a cooler unit comprising a sealed container having a wall portion to be cooled, an evacuated envelope, a transparent closure to said envelope disposed to allow radiations derived externally of said envelope to fall upon said Wall portion, a partition Within said container dividing said container into tWo compartments, said wall portion at least partly bounding one of said compartments, liquid coolant in each compartment a liquid flow restricting packing in at least said one compartment, an exhaust tube connecting the exterior of said envelope to the interior of said one compartment, said tube extending through the other compartment of said container,
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Power Engineering (AREA)
- General Physics & Mathematics (AREA)
- Computer Hardware Design (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Radiation Pyrometers (AREA)
- Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
Description
Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5860/59A GB1008740A (en) | 1959-02-20 | 1959-02-20 | Refrigeration unit |
Publications (1)
Publication Number | Publication Date |
---|---|
US3261180A true US3261180A (en) | 1966-07-19 |
Family
ID=9803981
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US9996A Expired - Lifetime US3261180A (en) | 1959-02-20 | 1960-02-19 | Cooler unit |
Country Status (3)
Country | Link |
---|---|
US (1) | US3261180A (en) |
DE (2) | DE1929109U (en) |
GB (1) | GB1008740A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3353371A (en) * | 1966-06-23 | 1967-11-21 | Gen Dynamics Corp | Dual tube regenerative cryostat |
US3371499A (en) * | 1966-11-02 | 1968-03-05 | Union Carbide Corp | Cryosorption vacuum pumping system |
US3389578A (en) * | 1966-09-30 | 1968-06-25 | Trw Inc | Refrigerator for multiplier phototubes |
US3391546A (en) * | 1965-08-06 | 1968-07-09 | Hymatic Eng Co Ltd | Refrigerating apparatus |
US3424230A (en) * | 1966-12-19 | 1969-01-28 | Andonian Associates Inc | Cryogenic refrigeration device with temperature controlled diffuser |
US3909225A (en) * | 1974-05-03 | 1975-09-30 | Robert Edward Rooney | Cryogenic dewar |
US4182129A (en) * | 1978-08-07 | 1980-01-08 | Beckman Instruments, Inc. | Heat exchanger |
US4526015A (en) * | 1984-10-15 | 1985-07-02 | General Electric Company | Support for cryostat penetration tube |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB189807773A (en) * | 1898-04-01 | 1899-03-04 | William Hampson | Improvements in the Process and Apparatus for the Self-intensive Refrigeration of Gases by Expansion and Counter-current Interchange. |
US1057052A (en) * | 1910-12-15 | 1913-03-25 | Philippe Auguste Guye | Process of recovering nitrous vapors or oxids of nitrogen diluted in indifferent gases. |
US1515119A (en) * | 1922-10-03 | 1924-11-11 | B M J Utilities Inc | Refrigerating device |
US2515092A (en) * | 1946-09-30 | 1950-07-11 | Miller Liter Company | Lighter |
US2566301A (en) * | 1946-06-13 | 1951-09-04 | Albert Alan | Portable refrigeration box |
US2791104A (en) * | 1956-04-25 | 1957-05-07 | Duz Angel | Liquefied gas refrigerator unit |
US2818717A (en) * | 1957-02-08 | 1958-01-07 | Morris Mecom | Cigarette lighter |
-
1959
- 1959-02-20 GB GB5860/59A patent/GB1008740A/en not_active Expired
-
1960
- 1960-02-19 DE DEH34305U patent/DE1929109U/en not_active Expired
- 1960-02-19 US US9996A patent/US3261180A/en not_active Expired - Lifetime
- 1960-02-20 DE DEH38708A patent/DE977324C/en not_active Expired
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB189807773A (en) * | 1898-04-01 | 1899-03-04 | William Hampson | Improvements in the Process and Apparatus for the Self-intensive Refrigeration of Gases by Expansion and Counter-current Interchange. |
US1057052A (en) * | 1910-12-15 | 1913-03-25 | Philippe Auguste Guye | Process of recovering nitrous vapors or oxids of nitrogen diluted in indifferent gases. |
US1515119A (en) * | 1922-10-03 | 1924-11-11 | B M J Utilities Inc | Refrigerating device |
US2566301A (en) * | 1946-06-13 | 1951-09-04 | Albert Alan | Portable refrigeration box |
US2515092A (en) * | 1946-09-30 | 1950-07-11 | Miller Liter Company | Lighter |
US2791104A (en) * | 1956-04-25 | 1957-05-07 | Duz Angel | Liquefied gas refrigerator unit |
US2818717A (en) * | 1957-02-08 | 1958-01-07 | Morris Mecom | Cigarette lighter |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3391546A (en) * | 1965-08-06 | 1968-07-09 | Hymatic Eng Co Ltd | Refrigerating apparatus |
US3353371A (en) * | 1966-06-23 | 1967-11-21 | Gen Dynamics Corp | Dual tube regenerative cryostat |
US3389578A (en) * | 1966-09-30 | 1968-06-25 | Trw Inc | Refrigerator for multiplier phototubes |
US3371499A (en) * | 1966-11-02 | 1968-03-05 | Union Carbide Corp | Cryosorption vacuum pumping system |
US3424230A (en) * | 1966-12-19 | 1969-01-28 | Andonian Associates Inc | Cryogenic refrigeration device with temperature controlled diffuser |
US3909225A (en) * | 1974-05-03 | 1975-09-30 | Robert Edward Rooney | Cryogenic dewar |
US4182129A (en) * | 1978-08-07 | 1980-01-08 | Beckman Instruments, Inc. | Heat exchanger |
US4526015A (en) * | 1984-10-15 | 1985-07-02 | General Electric Company | Support for cryostat penetration tube |
Also Published As
Publication number | Publication date |
---|---|
DE1929109U (en) | 1965-12-16 |
DE977324C (en) | 1965-12-02 |
GB1008740A (en) | 1965-11-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: BRITISH AEROSPACE PUBLIC LIMITED COMPANY Free format text: CHANGE OF NAME;ASSIGNOR:BRITISH AEROSPACE LIMITED;REEL/FRAME:004080/0820 Effective date: 19820106 Owner name: BRITISH AEROSPACE PUBLIC LIMITED COMPANY, DISTRICT Free format text: CHANGE OF NAME;ASSIGNOR:BRITISH AEROSPACE LIMITED;REEL/FRAME:004080/0820 Effective date: 19820106 |
|
AS | Assignment |
Owner name: BRITISH AEROSPACE, BROOKLANDS RD., WEYBRIDGE SURRE Free format text: ASSIGNOR HEREBY ASSIGNS NUNC PRO TUNC AS OF NOV. 22, 1978, THE ENTIRE INTEREST TO SAID ASSIGNEE TO SAID ASSIGNEE IN SAID PATENTS AND PATENT APPLICATIONS;ASSIGNOR:HAWKER SIDDELEY DYNAMICS LIMITED;REEL/FRAME:003949/0771 Effective date: 19811218 Owner name: BRITISH AEROSPACE, ENGLAND Free format text: ASSIGNOR HEREBY ASSIGNS NUNC PRO TUNC AS OF NOV. 22, 1978, THE ENTIRE INTEREST TO SAID ASSIGNEE TO SAID ASSIGNEE IN SAID PATENTS AND PATENT APPLICATIONS;ASSIGNOR:HAWKER SIDDELEY DYNAMICS LIMITED;REEL/FRAME:003949/0771 Effective date: 19811218 |