US3644020A - Variable contour reflector with cooling system - Google Patents
Variable contour reflector with cooling system Download PDFInfo
- Publication number
- US3644020A US3644020A US17103A US3644020DA US3644020A US 3644020 A US3644020 A US 3644020A US 17103 A US17103 A US 17103A US 3644020D A US3644020D A US 3644020DA US 3644020 A US3644020 A US 3644020A
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- US
- United States
- Prior art keywords
- mirror
- reflector
- combination
- set forth
- coolant
- 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
- 238000001816 cooling Methods 0.000 title claims description 9
- 239000002826 coolant Substances 0.000 claims abstract description 20
- 239000012530 fluid Substances 0.000 claims description 2
- 238000005086 pumping Methods 0.000 abstract description 5
- 238000007789 sealing Methods 0.000 abstract description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B26/00—Optical devices or arrangements for the control of light using movable or deformable optical elements
- G02B26/08—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light
- G02B26/0816—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more reflecting elements
- G02B26/0825—Optical devices or arrangements for the control of light using movable or deformable optical elements for controlling the direction of light by means of one or more reflecting elements the reflecting element being a flexible sheet or membrane, e.g. for varying the focus
Definitions
- Weights are located on UNITED STATES PATENTS the outer periphery of the reflector, offset from the center plane of the reflector, to provide a force when the reflector is 1,482,313 1] 1924 Mc.350/3 10 X rotated to vary its contour.
- the outer periphery of the reflec- 3,010,l53 l l/ 1961' Bittner tor is connected to the manifold by sealing means to minimize 3,513,474 5/1970 Gest et al ..343/9l5 X l f oolant at this point.
- the channels of the reflector can provide some pumping action if necessary.
- the reflector can also be cooled by a heat exchanger having grooves under the reflecting surface. With the cooling grooves extending radially outwardly from the center of the mirror the passages can be arranged as a centrifugal pump impeller to pump coolant flow. An auxiliary pump can also be provided in this system for a greater range of coolant flow or reflector shape and r.p.m. requirements.
- the weights are spaced sufficiently close and evenly spaced to provide smooth contouring.
- FIG. 1 is a side view partially in section of the invention.
- FIG. 2 is a view of the reflecting surface of the device with a portion thereof broken away.
- the beam reflecting device 1 is shown comprised offour main parts; l) the reflector or mirror 3, (2) the drive means 5, (3) the cooling system 7, and (4) the mounting means 9.
- the reflector or mirror 3 comprises a thin circular mirror member 11, on one side, having, a reflecting surface 12, which has its opposite side fixed to a grooved side of a circular supporting member 13.
- Supporting member 13 has its rearward surface flat while its forward surface is grooved by ribs 15 forming channels 17, as shown in FIG. 2.
- the assembled mirror is adapted to be cooled by a coolant flowing through said channels.
- a plurality of balance weights 18 are located around the outer periphery of the rearward flat surface of the supporting member 13 for a purpose to be hereinafter described.
- a hollow shaft 19 extends rearwardly from the rearward flat surface of the supporting member 13 and a flange 21 thereon is fixed to said member by bolts or any other means desired. This shaft extends coaxially from the circular supporting member. Hollow shaft 19 is rotatably mounted in housing 23 of the mounting means 9.
- a ball bearing assembly 25 has its inner race fixed to the forward end of said hollow shaft and has its outer race fixed to the housing. This ball bearing assembly prevents'axial movement of the shaft with respect to the housing.
- a roller bearing assembly 27 has its inner race fixed to the rearward end of the hollow shaft 19 and has its outer race fixed to the housing. The roller bearing permits axial movement to provide for thermal movement of the shaft with respect to the housing.
- a bevel gear 30 is fixed to the hollow shaft 19 and it meshes with a bevel gear 32 which is fixedly mounted to a drive shaft 34.
- a driving device 36 including a case 38 having a motor inside with a shaft 34 extending therefrom is fixed to said housing. Mounting flanges 40 on the case 38 are fixed to brackets 42 on the housing 23. The drive shaft 34, extends through a hole in the housing.
- speed control 44 controls the speed of the motor in the casing 38.
- Radial arms 50 extend from the forward part of housing 23 and are connected to an annular supporting member 52 which has a purpose to be hereinafter described. Legs 54 extend from said annular member and fix this end of the device. Legs 56 extend from the rearward part of the housing 23 and fix that end.
- annular collector 60 is mounted on the annular member 52 and has an annular inlet 62 positioned to receive any coolant flow which may pass through the channels 17 from the hollow shaft.
- Annular seal means 66 and 68 prevents leakage at the periphery of the mirror 3.
- the seal means 66 and 68 each are shown comprising a labyrinth type and are located on the front and rear side of the mirror 3. Other types of seal means desired can be used.
- Annular collector 60 has an outlet 70 which directs its flow into a conduit 72 which has its other end connected to the inlet of a pump 74.
- the outlet of pump 74 is connected to the free end of hollow shaft 19 by conduit 76.
- the hollow shaft 19 is rotatably mounted in the conduit 76 and a seal means is located between said members.
- a cooler 78 is positioned in the line 72. While the ribs 15 on the supporting member 13 are formed to provide a pumping action for the coolant, a pump 74 is provided for a greater range in operating conditions.
- a beam-reflecting device having in combination, a circular mirror, said mirror having a shaft extending from one side thereof and being mounted for rotation about its center on said shaft, said mirror having weight means positioned evenly around its periphery on one side thereof, and means for rotating said mirror whereby said weight means act to vary the contour of the mirror.
- said means for rotating said mirror includes a motor, said motor being drivingly connected to said shaft.
- cooling means includes passages in said mirror for flowing a coolant therethrough.
- conduit means connect said collector to said passages in said mirror.
- conduit means includes a cooler for controlling the temperature of the coolant.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Optical Elements Other Than Lenses (AREA)
Abstract
A circular reflector or mirror is mounted in a housing for rotation about a hollow shaft fixed to its center. A drive mechanism is provided to drive the reflector at various speeds. The reflector is provided with channels therein from its center to its outer periphery through which a coolant can flow from said hollow shaft to cool the reflector. A manifold is located around the periphery of the reflector to receive any coolant which passes therefrom. The coolant passes from the manifold and is recirculated through a cooler by a pumping means and directed back into the hollow shaft. Weights are located on the outer periphery of the reflector, offset from the center plane of the reflector, to provide a force when the reflector is rotated to vary its contour. The outer periphery of the reflector is connected to the manifold by sealing means to minimize loss of coolant at this point. The channels of the reflector can provide some pumping action if necessary.
Description
United States Patent Shannon Feb. 22, 1972 [54] VARIABLE CONTOUR REFLECTOR FOREIGN PATENTS OR APPLICA'ITONS WITH COOLING SYSTEM 548,295 4/1932 Germany ..240/47 [72] lnventor: Thomas E. Shannon, Knoxville, Tenn. 1,339,819 9/1963 France [73] Assignee: United Aircraft Corporation, East Hart- Primary Examiner-David Schonberg ford, Conn. Assistant Examiner-John W. Leonard [22] Filed: Mar. 6 1970 Attorney-Jack N. McCarthy [2|] Appl. No.: 17,103 [57] ABSTRACT A circular reflector or mirror is mounted in a housing for rota- 52 us. Cl ..3so/295 240/47 343/915 a Shaft fixed A drive 3 352/202 mechanism is provided to drive the reflector at various speeds. [51] lm Cl G02, 29/00 The reflector is provided with channels therein from its center [58] Fi d 293 310 62 to its outer periphery through which a coolant can flow from c o are I said hollow shaft to cool the reflector. A manifold is located 350/63 343/915 240/47 9 352/202 around the periphery of the reflector to receive any coolant which passes therefrom. The coolant passes from the manifold and is recirculated through a cooler by a pumping means and [56] References Cited directed back into the hollow shaft. Weights are located on UNITED STATES PATENTS the outer periphery of the reflector, offset from the center plane of the reflector, to provide a force when the reflector is 1,482,313 1] 1924 Miethe ..350/3 10 X rotated to vary its contour. The outer periphery of the reflec- 3,010,l53 l l/ 1961' Bittner tor is connected to the manifold by sealing means to minimize 3,513,474 5/1970 Gest et al ..343/9l5 X l f oolant at this point. The channels of the reflector can provide some pumping action if necessary.
1 1 Claims, 2 Drawing Figures /Z ,{Z 0 Ce a,
/ O /JPEfi za/vzeaz A (75 g 6! I W -Z/ J; I I r i? PATENTEDFEB22 I972 l l I I V 9% 7 ag 5 a Z K 4 i C W K M y VARIABLE CONTOUR REFLECTOR WITH COOLING SYSTEM BACKGROUND OF THE INVENTION This invention relates to a beam reflecting device having means for varying the contour of the reflecting surface during operation. U.S. Pat. No. 2,952,189 shows one example of a reflector having an adjustable focal length. U.S. application Ser. No. 733,221, now U.S. Pat. No. 3,514,776, shows other examples of reflectors having variable reflecting surfaces.
SUMMARY OF THE INVENTION The reflector can also be cooled by a heat exchanger having grooves under the reflecting surface. With the cooling grooves extending radially outwardly from the center of the mirror the passages can be arranged as a centrifugal pump impeller to pump coolant flow. An auxiliary pump can also be provided in this system for a greater range of coolant flow or reflector shape and r.p.m. requirements.
The weights are spaced sufficiently close and evenly spaced to provide smooth contouring.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a side view partially in section of the invention. FIG. 2 is a view of the reflecting surface of the device with a portion thereof broken away.
DESCRIPTION OF THE PREFERRED EMBODIMENT Referring to FIG. 1 the beam reflecting device 1 is shown comprised offour main parts; l) the reflector or mirror 3, (2) the drive means 5, (3) the cooling system 7, and (4) the mounting means 9.
The reflector or mirror 3 comprises a thin circular mirror member 11, on one side, having, a reflecting surface 12, which has its opposite side fixed to a grooved side of a circular supporting member 13. Supporting member 13 has its rearward surface flat while its forward surface is grooved by ribs 15 forming channels 17, as shown in FIG. 2. The assembled mirror is adapted to be cooled by a coolant flowing through said channels. A plurality of balance weights 18 are located around the outer periphery of the rearward flat surface of the supporting member 13 for a purpose to be hereinafter described.
A hollow shaft 19 extends rearwardly from the rearward flat surface of the supporting member 13 and a flange 21 thereon is fixed to said member by bolts or any other means desired. This shaft extends coaxially from the circular supporting member. Hollow shaft 19 is rotatably mounted in housing 23 of the mounting means 9. A ball bearing assembly 25 has its inner race fixed to the forward end of said hollow shaft and has its outer race fixed to the housing. This ball bearing assembly prevents'axial movement of the shaft with respect to the housing. A roller bearing assembly 27 has its inner race fixed to the rearward end of the hollow shaft 19 and has its outer race fixed to the housing. The roller bearing permits axial movement to provide for thermal movement of the shaft with respect to the housing.
The middle of the housing 23 is enlarged to provide for a power transmission to be located therein. A bevel gear 30 is fixed to the hollow shaft 19 and it meshes with a bevel gear 32 which is fixedly mounted to a drive shaft 34. A driving device 36 including a case 38 having a motor inside with a shaft 34 extending therefrom is fixed to said housing. Mounting flanges 40 on the case 38 are fixed to brackets 42 on the housing 23. The drive shaft 34, extends through a hole in the housing. A
. Radial arms 50 extend from the forward part of housing 23 and are connected to an annular supporting member 52 which has a purpose to be hereinafter described. Legs 54 extend from said annular member and fix this end of the device. Legs 56 extend from the rearward part of the housing 23 and fix that end.
It can be seen that as the motor is energized by the speed control it will rotate bevel gear 32 which will in turn rotate gear 30 and the hollow shaft 19. Rotation of shaft 19 rotates the mirror 3. In view of the location of the balance weights 18, as the speed of the reflector or mirror increases the supporting member 13 and mirror member 11 will begin to move forwardly at the outer edge forming a concave reflecting surface. It is to be remembered that these movements need not be very large. U.S. Pat. No. 3,229,578 refers to reflectors made of flexible material.
An annular collector 60 is mounted on the annular member 52 and has an annular inlet 62 positioned to receive any coolant flow which may pass through the channels 17 from the hollow shaft. Annular seal means 66 and 68 prevents leakage at the periphery of the mirror 3. The seal means 66 and 68 each are shown comprising a labyrinth type and are located on the front and rear side of the mirror 3. Other types of seal means desired can be used.
Annular collector 60 has an outlet 70 which directs its flow into a conduit 72 which has its other end connected to the inlet ofa pump 74. The outlet of pump 74 is connected to the free end of hollow shaft 19 by conduit 76. The hollow shaft 19 is rotatably mounted in the conduit 76 and a seal means is located between said members. A cooler 78 is positioned in the line 72. While the ribs 15 on the supporting member 13 are formed to provide a pumping action for the coolant, a pump 74 is provided for a greater range in operating conditions.
I claim:
I. A beam-reflecting device having in combination, a circular mirror, said mirror having a shaft extending from one side thereof and being mounted for rotation about its center on said shaft, said mirror having weight means positioned evenly around its periphery on one side thereof, and means for rotating said mirror whereby said weight means act to vary the contour of the mirror.
2. A combination as set forth in claim 1 wherein cooling means are provided for said mirror.
3. A combination as set forth in claim 1 wherein said means for rotating said mirror includes a motor, said motor being drivingly connected to said shaft.
4. A combination as set forth in claim 2 wherein said cooling means includes passages in said mirror for flowing a coolant therethrough.
5. A combination as set forth in claim 4 wherein said shaft has a passageway therein, said passageway being connected to said passages, means for delivering a coolant through said passageway to said passages.
6. A combination as set forth in claim 4 wherein said passages extend radially and act to move the coolant from the center of the mirror to its periphery.
7. A combination as set forth in claim 6 wherein said passages intersect the periphery of the mirror and form holes therearound.
8. A combination as set forth in claim 7 wherein a collector is connected to the holes around the periphery of the mirror to collect the fluid flowing therefrom.
9. A combination as set forth in claim 8 wherein conduit means connect said collector to said passages in said mirror.
10. A combination as set forth in claim 9 wherein said shaft has a passageway therethrough, said passageway forming part of the conduit means.
11. A combination as set forth in claim 9 wherein said conduit means includes a cooler for controlling the temperature of the coolant.
Claims (11)
1. A beam-reflecting device having in combination, a circular mirror, said mirror having a shaft extending from one side thereof and being mounted for rotation about its center on said shaft, said mirror having weight means positioned evenly around its periphery on one side thereof, and means for rotating said mirror whereby said weight means act to vary the contour of the mirror.
2. A combination as set forth in claim 1 wherein cooling means are provided for said mirror.
3. A combination as set forth in claim 1 wherein said means for rotating said mirror includes a motor, said motor being drivingly connEcted to said shaft.
4. A combination as set forth in claim 2 wherein said cooling means includes passages in said mirror for flowing a coolant therethrough.
5. A combination as set forth in claim 4 wherein said shaft has a passageway therein, said passageway being connected to said passages, means for delivering a coolant through said passageway to said passages.
6. A combination as set forth in claim 4 wherein said passages extend radially and act to move the coolant from the center of the mirror to its periphery.
7. A combination as set forth in claim 6 wherein said passages intersect the periphery of the mirror and form holes therearound.
8. A combination as set forth in claim 7 wherein a collector is connected to the holes around the periphery of the mirror to collect the fluid flowing therefrom.
9. A combination as set forth in claim 8 wherein conduit means connect said collector to said passages in said mirror.
10. A combination as set forth in claim 9 wherein said shaft has a passageway therethrough, said passageway forming part of the conduit means.
11. A combination as set forth in claim 9 wherein said conduit means includes a cooler for controlling the temperature of the coolant.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US1710370A | 1970-03-06 | 1970-03-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3644020A true US3644020A (en) | 1972-02-22 |
Family
ID=21780733
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US17103A Expired - Lifetime US3644020A (en) | 1970-03-06 | 1970-03-06 | Variable contour reflector with cooling system |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3644020A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4143946A (en) * | 1977-12-05 | 1979-03-13 | The United States Of America As Represented By The Secretary Of The Navy | Impingement cooled deformable laser mirror |
| US4266857A (en) * | 1980-01-30 | 1981-05-12 | The United States Of America As Represented By The Secretary Of The Treasury | Liquid or gas cooled flexible beam-compensating adjustable cylindrical mirror |
| US5020895A (en) * | 1989-01-10 | 1991-06-04 | Adolf Giesen | Laser mirror head |
| GB2254164A (en) * | 1991-03-15 | 1992-09-30 | Diehl Gmbh & Co | Variable shape convex mirror with central electromechemical actuator |
| US20060103955A1 (en) * | 2002-12-23 | 2006-05-18 | Bae Systems Plc | Deformable-mirror cooling |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1482313A (en) * | 1923-05-12 | 1924-01-29 | Miethe Adolf | Replector |
| DE548295C (en) * | 1930-03-27 | 1932-04-09 | Aeg | Cooling device for lighting fixtures with reflector |
| US3010153A (en) * | 1959-03-12 | 1961-11-28 | Gulton Ind Inc | Construction of paraboloid surfaces |
| FR1339819A (en) * | 1962-11-15 | 1963-10-11 | Cinema projector mirror | |
| US3513474A (en) * | 1967-01-09 | 1970-05-19 | Csf | Collapsible hyperbolic reflector formed of spaced wires |
-
1970
- 1970-03-06 US US17103A patent/US3644020A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1482313A (en) * | 1923-05-12 | 1924-01-29 | Miethe Adolf | Replector |
| DE548295C (en) * | 1930-03-27 | 1932-04-09 | Aeg | Cooling device for lighting fixtures with reflector |
| US3010153A (en) * | 1959-03-12 | 1961-11-28 | Gulton Ind Inc | Construction of paraboloid surfaces |
| FR1339819A (en) * | 1962-11-15 | 1963-10-11 | Cinema projector mirror | |
| US3513474A (en) * | 1967-01-09 | 1970-05-19 | Csf | Collapsible hyperbolic reflector formed of spaced wires |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4143946A (en) * | 1977-12-05 | 1979-03-13 | The United States Of America As Represented By The Secretary Of The Navy | Impingement cooled deformable laser mirror |
| US4266857A (en) * | 1980-01-30 | 1981-05-12 | The United States Of America As Represented By The Secretary Of The Treasury | Liquid or gas cooled flexible beam-compensating adjustable cylindrical mirror |
| US5020895A (en) * | 1989-01-10 | 1991-06-04 | Adolf Giesen | Laser mirror head |
| GB2254164A (en) * | 1991-03-15 | 1992-09-30 | Diehl Gmbh & Co | Variable shape convex mirror with central electromechemical actuator |
| GB2254164B (en) * | 1991-03-15 | 1994-07-13 | Diehl Gmbh & Co | A mechanism for influencing the beam when processing a workpiece with a high-energy laser beam |
| US20060103955A1 (en) * | 2002-12-23 | 2006-05-18 | Bae Systems Plc | Deformable-mirror cooling |
| US7264363B2 (en) | 2002-12-23 | 2007-09-04 | Bae Systems Plc | Deformable-mirror cooling |
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