US3162189A - Ray intensity control for solar mirror - Google Patents

Ray intensity control for solar mirror Download PDF

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US3162189A
US3162189A US44686A US4468660A US3162189A US 3162189 A US3162189 A US 3162189A US 44686 A US44686 A US 44686A US 4468660 A US4468660 A US 4468660A US 3162189 A US3162189 A US 3162189A
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reflector
blades
energy
energy device
axis
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US44686A
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Leslie C Small
Trent H Holmes
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Raytheon Technologies Corp
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United Aircraft Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S50/00Arrangements for controlling solar heat collectors
    • F24S50/40Arrangements for controlling solar heat collectors responsive to temperature
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S23/00Arrangements for concentrating solar-rays for solar heat collectors
    • F24S23/70Arrangements for concentrating solar-rays for solar heat collectors with reflectors
    • F24S23/71Arrangements for concentrating solar-rays for solar heat collectors with reflectors with parabolic reflective surfaces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S40/00Safety or protection arrangements of solar heat collectors; Preventing malfunction of solar heat collectors
    • F24S40/50Preventing overheating or overpressure
    • F24S40/52Preventing overheating or overpressure by modifying the heat collection, e.g. by defocusing or by changing the position of heat-receiving elements
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers

Definitions

  • This invention relates to reflector systems. More particularly it relates to controlling the amount of reflection from a reflector.
  • a feature of this invention is a device which interferes with and controls the transmission of energy between the reflecting surface and the energy device.
  • the invention may be used in connection with a reflector system for outer space such as that described in US. application Serial No. 21,988, now Patent No. 3,064,534, which is assigned to the assignee in the present applica tion.
  • a feature of this invention is the control of the amount of heat delivered to the boiler from the reflecting surface.
  • Another feature of this invention is the control of the amount of heat delivered to the boiler in any amount from a desired maximum to a desired minimum.
  • Still another feature of this invention is the control of the amount of heat delivered to the boiler as a function of the temperature of the fluid in the boiler.
  • Still another feature of the present invention is to control the amount of heat reflected to the boiler by interfering with the heat rays reflected from the reflecting surface.
  • the reflector system operates on the principle of reflecting heat rays, and concentrating them at the focal point of the reflecting surface, and a boiler is located adjacent to the focal point. If heat rays are reflected to a point other than the focal point of the reflecting surface, it is possible that structural parts of the boiler or supporting members may become weakened by excessive heating. Therefore, a feature of this invention is the diverting of some of the heat rays entirely away from the reflector system.
  • the reflector system described in US. application Serial No. 21,988, new Patent No. 3,064,534 is designed to fit into an extremely small package while being transported through the atmosphere, and it is expanded into the operating position when it arrives at its destination in space.
  • Another feature of the present invention is to contain the control system within a very small space when the reflector is collapse so as not to interfere with the collapsing and packaging of the reflector for travel.
  • FIG. 1 is a view showing the reflector system in its closed position.
  • FlG. 2 is a view showing the reflector system in its extended position.
  • FIG. 3 is a view showing the details of the reflection controlling mechanism.
  • FIG. 4 is a view along line 44 of FIG. 3.
  • FIG. 5 is a plan view showing the reflector system in its extended position.
  • FIGS. 1 and 2 show a reflector system 2 which is composed of a plurality of reflector sectors 4, a boiler 6 and a plurality of blades 8 interposed between reflector sectors sectors 4 and boiler 6.
  • the outer ends of reflector sectors 4 extend well beyond the outer ends of the blades 8, and hence the blades 8 are contained entirely within the extremities of the reflector.
  • Boiler 6 is located adjacent to the focal point of extended reflector sectors 4 and is attached to a base 18 by struts 12, and reflector sectors 4 are rotatably connected to base 10.
  • Reflector sectors 4 and bales 8 can be retracted so that in the closed position, the reflector system can be encased in a container 14, the diameter of which is substantially equal to the diameter of base 10.
  • US. application Serial No. 21,988, now Patent No. 3,064,534 for the details of the actuation of reflector sectors 4.
  • a ring 16 is attached to struts i2 and a pair of bearings 18 are attached to ring 16.
  • a shaft 20 is rotatably mounted in bearings 18, and a pair of springs 22 are attached to shaft 20.
  • Springs 22 are attached to and support the reflection control blade 8.
  • An arm 26 extends from shaft 20, and a roller 28 is mounted on arm 26.
  • a spring 30 is connected to one of the bearings 18 and to shaft 20.
  • the reflector system contains a plurality of units consisting of bearings 18, shaft 28, springs 22, blade 8, arm 26, roller 28 and spring 30.
  • a fluid filled temperature bulb 32 of well-known construction is located in boiler 6 to sense the temperature of the fluid in the boiler. In a well-known manner, bulb 32 communicates through fluid filled line 34 with fluid filled bellows 36.
  • a plate 38 is attached to bellows 36, and a spring 3% is mounted on plate 38. Ring 39 is in contact with roller 28. Changes in temperature in boiler 6 cause an expansion or contraction of bellows 36 and result in translation of plate 38 and attached ring 39. This translation of plate 38 and ring 39 acts through roller 28 and arm 26 to rotate shaft 29 and vary the position of blade 8.
  • A can best be seen in FIG. 4, arm 26 is inclined to the surface of ring 39 to insure ease of motion of arm as.
  • the diameter of ring 39 is such that there is no interference between ring 39 and bearings 18, and, thus, arm 26 can be raised above the axis of shaft 20 so that shaft 20 can be rotated a full Heat rays are reflected from sectors 4 to the focal point of the sectors.
  • Blades 8 are interposed between sectors 4 and boiler 6 to interfere with the reflection of the heat rays. Blades 8 can themselves be reflecting surfaces and the blades 8 are inclined at an angle to the axis of the reflecting surface formed by sectors 4 so that heat rays which strike blades 8 are reflected away from the reflector system. Thus, there is no concentration of heat rays back to reflector sectors 4 or on any structural members of the reflector system due to the action of blades 8.
  • blades 8 offer a minimum amount of interference with the transmission of heat rays between sectors 4 and boiler 6 when blades 8 are in a position substantially perpendicular to sectors 4.
  • a 90 rotation of blades 8 places them in a position of maximum interference with the heat rays transmission. It is ap arent that any degree of control of heat ray transmission can be otained by any amount of rotation of blades 8 up to 90.
  • the boiler temperature may still be above a desired level when blades 3 have been rotated 90 to the position of maximum interference with heat ray transmission.
  • blades 8 When the reflector system is transported, blades 8 must be retracted as is shown in FIG. 1.
  • Springs 22 allow blades 8 .to be placed at an angle to shaft 20 when the reflector-system is packaged, ,and springs 22 will snap blades 8 into doperating position as shownin FIG. 2 when the reflectoris extended.
  • shafts 20 are rotated so that the blades arein the position of'maximum heat ray interference, and then springs 22 are flexed so that blades S-are angled with respect to shafts 20.
  • first reflector means forming substantially a surface of revolution having an axis and a focal point on the axis, an energy device located substantially .at the focal point of said first reflector means, second reflector means interposed between said first reflector means and said energy device for varying the amount of energy transmission from said first reflector means to said energy device, said second reflector means having a reflecting surface at least partially facing said first reflector means and inclined at an angle to said axis to form an obtuse anglebetween said second reflector means and said axis on the side of said second reflector means facing said first reflectormeans such that.
  • the .reflection from said second reflector means is directed away fromsaid first reflecto rmeans and away from said energy device, ,and means associated with said second reflector means for controlling the amount of variationof energy transmission between said first reflector means'and said energy device.
  • a reflector system a base, a-"plurality of first reflector means rotatably attached to said base-said first reflector means in a first position extending substantially radially from said base and forming substantially a surface of revolution having an axis and a focal point on the axis, saidfir st reflector means in a second position being aligned in a direction substantially along said axis, an energy devicelocated substantially at said focal point of said first reflector means, and second reflector means interposed between said first reflector means and .said energy device, said second reflector means in a first position extending substantially radially from said axis and inwasecond position extending in a direction substantially ,along said axis, said first posit-ion of said second reflector means corresponding to said first position of saidfirst reflector means and said second position .of said second reflector ,means corresponding to said second position of said first reflector means;
  • T e c mb n Ion as inclaim 2 including control p *JR., ROBERT A. :OLEARY, Examiners.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Radiation Pyrometers (AREA)

Description

, 1964 L. c. SMALL ETAL 3,162,189
RAY INTENSITY CONTROL FOR SOLAR MIRROR Filed July 22, 1960 3 Sheets-Sheet 1 IV; I I" F IG. 2 a
INVENTORS TRENT H HOLMES LESLIE C. SMALL AGENT Dec. 22, 1964 L. c. SMALL ETAL 3,162,189
RAY INTENSITY CONTROL. FOR SOLAR MIRROR Filed July 22, 1960 5 Sheets-Sheet 2 F/G 3 70 72. 449 ff/K508 INVENTORS TRENT H. HOLMES LESLIE C. SMALL By M $41M AGENT Dec. 22, 1964 c. SMALL ETAL 3,162,189
CONTROL R SOLAR M Filed July 22, 1960 IN VEN TOPS TRENT H HOLMES LESLIE C. SMALL AGENT United States Patent i Delaware Filed July 22, 1960, Ser. No. 44,686 7 ciaims. c1. 126 -2742) This invention relates to reflector systems. More particularly it relates to controlling the amount of reflection from a reflector.
The invention will be described in connection with a reflector system in which heat rays are reflected from a parabolic surface to a boiler located at the focal point of the parabolic surface, but it is to be expressly understood that the invention is applicable to any reflector system in which any form of energy is reflected either from a point outside the reflector to an energy device associated with the reflector such as in the present system, or in which energy is reflected from an energy device to a point outside the reflector such as in a radar system or other electromagnetic wave transmitters. Accordingly, a feature of this invention is a device which interferes with and controls the transmission of energy between the reflecting surface and the energy device.
The invention may be used in connection with a reflector system for outer space such as that described in US. application Serial No. 21,988, now Patent No. 3,064,534, which is assigned to the assignee in the present applica tion. In such a reflector system it is desirable to control the amount of heat reflected from the reflecting surface to the boiler. Accordingly, a feature of this invention is the control of the amount of heat delivered to the boiler from the reflecting surface. Another feature of this invention is the control of the amount of heat delivered to the boiler in any amount from a desired maximum to a desired minimum. Still another feature of this invention is the control of the amount of heat delivered to the boiler as a function of the temperature of the fluid in the boiler. Still another feature of the present invention is to control the amount of heat reflected to the boiler by interfering with the heat rays reflected from the reflecting surface.
The reflector system operates on the principle of reflecting heat rays, and concentrating them at the focal point of the reflecting surface, and a boiler is located adjacent to the focal point. If heat rays are reflected to a point other than the focal point of the reflecting surface, it is possible that structural parts of the boiler or supporting members may become weakened by excessive heating. Therefore, a feature of this invention is the diverting of some of the heat rays entirely away from the reflector system.
The reflector system described in US. application Serial No. 21,988, new Patent No. 3,064,534, is designed to fit into an extremely small package while being transported through the atmosphere, and it is expanded into the operating position when it arrives at its destination in space. Another feature of the present invention is to contain the control system within a very small space when the reflector is collapse so as not to interfere with the collapsing and packaging of the reflector for travel.
Other features and advantages will be apparent from the specification and claims, and from the accompanying drawings which illustrate an embodiment of the invention.
FIG. 1 isa view showing the reflector system in its closed position.
' FlG. 2 is a view showing the reflector system in its extended position.
FIG. 3 is a view showing the details of the reflection controlling mechanism.
FIG. 4 is a view along line 44 of FIG. 3.
3,162,189 Patented Dec. 22, 1964 FIG. 5 is a plan view showing the reflector system in its extended position.
FIGS. 1 and 2 show a reflector system 2 which is composed of a plurality of reflector sectors 4, a boiler 6 and a plurality of blades 8 interposed between reflector sectors sectors 4 and boiler 6. The outer ends of reflector sectors 4 extend well beyond the outer ends of the blades 8, and hence the blades 8 are contained entirely within the extremities of the reflector. Boiler 6 is located adjacent to the focal point of extended reflector sectors 4 and is attached to a base 18 by struts 12, and reflector sectors 4 are rotatably connected to base 10. Reflector sectors 4 and bales 8 can be retracted so that in the closed position, the reflector system can be encased in a container 14, the diameter of which is substantially equal to the diameter of base 10. Reference is made to US. application Serial No. 21,988, now Patent No. 3,064,534, for the details of the actuation of reflector sectors 4.
Referring now to FIG. 3, a ring 16 is attached to struts i2 and a pair of bearings 18 are attached to ring 16. A shaft 20 is rotatably mounted in bearings 18, and a pair of springs 22 are attached to shaft 20. Springs 22 are attached to and support the reflection control blade 8. An arm 26 extends from shaft 20, and a roller 28 is mounted on arm 26. A spring 30 is connected to one of the bearings 18 and to shaft 20. The reflector system contains a plurality of units consisting of bearings 18, shaft 28, springs 22, blade 8, arm 26, roller 28 and spring 30.
A fluid filled temperature bulb 32 of well-known construction is located in boiler 6 to sense the temperature of the fluid in the boiler. In a well-known manner, bulb 32 communicates through fluid filled line 34 with fluid filled bellows 36. A plate 38 is attached to bellows 36, and a spring 3% is mounted on plate 38. Ring 39 is in contact with roller 28. Changes in temperature in boiler 6 cause an expansion or contraction of bellows 36 and result in translation of plate 38 and attached ring 39. This translation of plate 38 and ring 39 acts through roller 28 and arm 26 to rotate shaft 29 and vary the position of blade 8. A can best be seen in FIG. 4, arm 26 is inclined to the surface of ring 39 to insure ease of motion of arm as. The diameter of ring 39 is such that there is no interference between ring 39 and bearings 18, and, thus, arm 26 can be raised above the axis of shaft 20 so that shaft 20 can be rotated a full Heat rays are reflected from sectors 4 to the focal point of the sectors. Blades 8 are interposed between sectors 4 and boiler 6 to interfere with the reflection of the heat rays. Blades 8 can themselves be reflecting surfaces and the blades 8 are inclined at an angle to the axis of the reflecting surface formed by sectors 4 so that heat rays which strike blades 8 are reflected away from the reflector system. Thus, there is no concentration of heat rays back to reflector sectors 4 or on any structural members of the reflector system due to the action of blades 8.
As can best be seen in FIGS. 2 and 5, blades 8 offer a minimum amount of interference with the transmission of heat rays between sectors 4 and boiler 6 when blades 8 are in a position substantially perpendicular to sectors 4. A 90 rotation of blades 8 places them in a position of maximum interference with the heat rays transmission. It is ap arent that any degree of control of heat ray transmission can be otained by any amount of rotation of blades 8 up to 90. Of course, it is possible that the boiler temperature may still be above a desired level when blades 3 have been rotated 90 to the position of maximum interference with heat ray transmission. However, any further rotation of blades 8 would operate to increase the amount of heat ray transmission, and, therefore, stops 40 extend from some of the bearings 18 to limit the travel of plate 38. Spring 38 will have been coiled when plate 38 is translated in response to increases in temperature in .boiler 6. Thus, it can .be seen that spring 30 will act to rotate shaft to move blades 8 toward the position of minimum interference with heat ray transmission when the temperature in boiler 6 decreases. In the event of a failure of temperature bulb 32, line 34, -or bellows 36, spring will insure that blades 8 will assume the position o f minimum interfer- ,ence with beat my transmission,
When the reflector system is transported, blades 8 must be retracted as is shown in FIG. 1. Springs 22 allow blades 8 .to be placed at an angle to shaft 20 when the reflector-system is packaged, ,and springs 22 will snap blades 8 into doperating position as shownin FIG. 2 when the reflectoris extended. In order .to package blades 8, shafts 20 are rotated so that the blades arein the position of'maximum heat ray interference, and then springs 22 are flexed so that blades S-are angled with respect to shafts 20. This rotation of shafts 20 loads springs 30 so that when the reflector is extended blades 8 will -.simultane ously snap into operating position and be rotated by springs 30 to initially .assu-me the ,position of minimumheat ray interference. I Itis to be ,understood that the invention is not limited -to the specific embodiment herein illustrated and described but may be used in other ways without departure from its spirit a sdefined by the following claims.
We claim: i
1. In combination, areflector forming substantially surface of revolution and having an axis and a focal point on the axis, an energy device located substantially at the focal pointofsaid reflector, a plurality :of rotatably mounted blades interposed between said reflector and said energy device and entirely within the extremities of said reflector to vary the amount of energy transmission from said ,reflector to said energy device, each of said blades :having a reflecting surface on one side, thereof, said blades in a first position allowing a maximum transmission of energy from said reflector to said energy device and in .a second ,position allowing a minimum trans mission of energy from said reflector (to :said energy device, means for rotating said blades to any position between said first and second positions, isaid bladesin said second position having the reflecting surfaces thereof faeingsaid reflector and inclined at .to form an obtuse angle between said blades and said that signals impinging on said reflecting surfaces from being packaged to be an angle to said axis 45 axis on the side of said blades :facing said reflector such 7 said reflector are directed away from said energy, device and away from said reflector, and means for preventing rotation of said blades beyond said second position.
2. In combination, a reflector forming substantially a,
surface of revolution and having an axis and a focal .point on the axis, an energy device located substantially at the focal point of said reflector, a plurality of rotatably mounted reflector blades interposed between said reflector and said-energy :deviceand entirely ,within the extremities of said reflector to vary the amount of energy transmission from said reflector to said energy device, .said re-- flector blades in ,a first :position allowing a max mum transmission of energy from said reflector to ,said energy device and in a second, position allowing .a minimum' transmission of energy from said reflector to said energy device, said'reflector blades in said second position being .blades facing said reflector such that energy incident on inclined at an angle to said axis to form an obtuse angle between said blades ,and said axis on the side of said said reflector :blades from said reflector is' directed away I from said renergy device and away ,from s'aidmeflector, means for rotating said bladesto, any posit-ion between means responsive to the temperature of the energy device for deter-mining the degree of rotation of the blades between the'first and second positions.
4. In a reflector system, first reflector means forming substantially a surface of revolution having an axis and a focal point on the axis, an energy device located substantially .at the focal point of said first reflector means, second reflector means interposed between said first reflector means and said energy device for varying the amount of energy transmission from said first reflector means to said energy device, said second reflector means having a reflecting surface at least partially facing said first reflector means and inclined at an angle to said axis to form an obtuse anglebetween said second reflector means and said axis on the side of said second reflector means facing said first reflectormeans such that. the .reflection from said second reflector means is directed away fromsaid first reflecto rmeans and away from said energy device, ,and means associated with said second reflector means for controlling the amount of variationof energy transmission between said first reflector means'and said energy device. v
5; In a reflector system, a base, a-"plurality of first reflector means rotatably attached to said base-said first reflector means in a first position extending substantially radially from said base and forming substantially a surface of revolution having an axis and a focal point on the axis, saidfir st reflector means in a second position being aligned in a direction substantially along said axis, an energy devicelocated substantially at said focal point of said first reflector means, and second reflector means interposed between said first reflector means and .said energy device, said second reflector means in a first position extending substantially radially from said axis and inwasecond position extending in a direction substantially ,along said axis, said first posit-ion of said second reflector means corresponding to said first position of saidfirst reflector means and said second position .of said second reflector ,means corresponding to said second position of said first reflector means;
6. Areflector system as iniclairn 5 wherein saidsecond reflector means includes ,a plurality of blades, each of said blades being conneeted' to arotatably mounted shaft,
' and means forangularly displacing said blades with respect to said shafts. N
7. A reflector system as in claim 5 wherein said second reflector means includes ,a plurality of rotatably mounted blades, and including means for rotating said blades in thefirst position thereof between positions of minimum and maximum interference with transmission between said first reflector means in the first position thereof and said energy dev e, and means for preventing rotation of said blades beyond 'said position if/maximum interference. v, V i
References Cited by the Examiner UNITED STATES PATENTS said first and second positions, means biasing said blades toward said first posi on, and means for preventing rota- ..tion of said blades beyond said second position. v I
T e c mb n Ion as inclaim 2 including control p *JR., ROBERT A. :OLEARY, Examiners.

Claims (1)

1. IN COMBINATION, A REFLECTOR FORMING SUBSTANTIALLY A SURFACE OF REVOLUTION AND HAVING AN AXIS AND A FOCAL POINT ON THE AXIS, AN ENERGY DEVICE LOCATED SUBSTANTIALLY AT THE FOCAL POINT OF SAID REFLECTOR, A PLURALITY OF ROTATABLY MOUNTED BLADES INTERPOSED BETWEEN SAID REFLECTOR AND SAID ENERGY DEVICE AND ENTIRELY WITHIN THE EXTREMITIES OF SAID REFLECTOR TO VARY THE AMOUNT OF ENERGY TRANSMISSION FROM SAID REFLECTOR TO SAID ENERGY DEVICE, EACH OF SAID BLADES HAVING A REFLECTING SURFACE ON ONE SIDE THEREOF, SAID BLADES IN A FIRST POSITION ALLOWING A MAXIMUM TRANSMISSION OF ENERGY FROM SAID REFLECTOR TO SAID ENERGY DEVICE AND IN A SECOND POSITION ALLOWING A MINIMUM TRANSMISSION OF ENERGY FROM SAID REFLECTOR TO SAID ENERGY DEVICE, MEANS FOR ROTATING SAID BLADES TO ANY POSITION BE-
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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3273558A (en) * 1964-07-28 1966-09-20 Gen Electric Self-controlling gas generator
US3915147A (en) * 1973-12-03 1975-10-28 Arthur E Rineer Solar energy steam generator
US4108158A (en) * 1977-03-28 1978-08-22 Sparkler Filters, Inc. Solar energy powered heat generator
FR2478279A1 (en) * 1980-02-20 1981-09-18 Prat Serge Focussing mirror for solar radiation - has cylindrical-parabolic configuration with centre of gravity coinciding with focus for self-balancing
US4304218A (en) * 1979-08-24 1981-12-08 Jon Karlsson Solar energy collector
EP0288237A2 (en) * 1987-04-20 1988-10-26 Halliburton Company Method and apparatus for perforating a gun
WO2004011213A1 (en) 2002-07-29 2004-02-05 L.S. Starrett Company Cutting tool with grooved cutting edge
US20110203574A1 (en) * 2008-09-18 2011-08-25 Geoffrey Lester Harding Non-tracking solar collector device
IT201600084083A1 (en) * 2016-08-10 2018-02-10 Cordivari S R L Automatic hydraulic movement system of elements of a compact solar collector.

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Publication number Priority date Publication date Assignee Title
US1479923A (en) * 1922-04-10 1924-01-08 Marcel E Moreau Solar furnace
US2030350A (en) * 1933-04-10 1936-02-11 Carl G Fisher Solar operated refrigerating system
US2182222A (en) * 1936-11-23 1939-12-05 Stuart A Courtis Solar heater
US2259902A (en) * 1938-10-17 1941-10-21 Mccain John David Solar heater
FR993096A (en) * 1949-06-02 1951-10-26 Prosilis Further training in solar ovens
US2945234A (en) * 1958-05-05 1960-07-12 Avco Mfg Corp Collapsible reflecting structure for electric waves
USRE25105E (en) * 1961-12-26 figure
US3024700A (en) * 1959-04-08 1962-03-13 John F Mcclellan Mechanical shutter of large aperture and high speed

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USRE25105E (en) * 1961-12-26 figure
US1479923A (en) * 1922-04-10 1924-01-08 Marcel E Moreau Solar furnace
US2030350A (en) * 1933-04-10 1936-02-11 Carl G Fisher Solar operated refrigerating system
US2182222A (en) * 1936-11-23 1939-12-05 Stuart A Courtis Solar heater
US2259902A (en) * 1938-10-17 1941-10-21 Mccain John David Solar heater
FR993096A (en) * 1949-06-02 1951-10-26 Prosilis Further training in solar ovens
US2945234A (en) * 1958-05-05 1960-07-12 Avco Mfg Corp Collapsible reflecting structure for electric waves
US3024700A (en) * 1959-04-08 1962-03-13 John F Mcclellan Mechanical shutter of large aperture and high speed

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3273558A (en) * 1964-07-28 1966-09-20 Gen Electric Self-controlling gas generator
US3915147A (en) * 1973-12-03 1975-10-28 Arthur E Rineer Solar energy steam generator
US4108158A (en) * 1977-03-28 1978-08-22 Sparkler Filters, Inc. Solar energy powered heat generator
US4304218A (en) * 1979-08-24 1981-12-08 Jon Karlsson Solar energy collector
FR2478279A1 (en) * 1980-02-20 1981-09-18 Prat Serge Focussing mirror for solar radiation - has cylindrical-parabolic configuration with centre of gravity coinciding with focus for self-balancing
EP0288237A2 (en) * 1987-04-20 1988-10-26 Halliburton Company Method and apparatus for perforating a gun
EP0288237A3 (en) * 1987-04-20 1990-05-02 Halliburton Company Method and apparatus for perforating a gun
WO2004011213A1 (en) 2002-07-29 2004-02-05 L.S. Starrett Company Cutting tool with grooved cutting edge
US20110203574A1 (en) * 2008-09-18 2011-08-25 Geoffrey Lester Harding Non-tracking solar collector device
US8707948B2 (en) * 2008-09-18 2014-04-29 Kloben S.A.S. Di Turco Adelino Ec. Non-tracking solar collector device
IT201600084083A1 (en) * 2016-08-10 2018-02-10 Cordivari S R L Automatic hydraulic movement system of elements of a compact solar collector.
WO2018055648A1 (en) * 2016-08-10 2018-03-29 Cordivari S.R.L. Automatic hydraulic motion system of elements of a compact solar collector

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