DE19953934C2 - Linear actuator for space applications - Google Patents
Linear actuator for space applicationsInfo
- Publication number
- DE19953934C2 DE19953934C2 DE1999153934 DE19953934A DE19953934C2 DE 19953934 C2 DE19953934 C2 DE 19953934C2 DE 1999153934 DE1999153934 DE 1999153934 DE 19953934 A DE19953934 A DE 19953934A DE 19953934 C2 DE19953934 C2 DE 19953934C2
- Authority
- DE
- Germany
- Prior art keywords
- bellows
- lines
- elements
- controller
- electrical
- 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 - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
- F15B9/02—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
- F15B9/08—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor
- F15B9/09—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor with electrical control means
-
- 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
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/04—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
- F15B11/042—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the feed line, i.e. "meter in"
- F15B11/0426—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the feed line, i.e. "meter in" by controlling the number of pumps or parallel valves switched on
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/02—Systems essentially incorporating special features for controlling the speed or actuating force of an output member
- F15B11/04—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed
- F15B11/044—Systems essentially incorporating special features for controlling the speed or actuating force of an output member for controlling the speed by means in the return line, i.e. "meter out"
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B15/00—Fluid-actuated devices for displacing a member from one position to another; Gearing associated therewith
- F15B15/08—Characterised by the construction of the motor unit
- F15B15/10—Characterised by the construction of the motor unit the motor being of diaphragm type
- F15B15/103—Characterised by the construction of the motor unit the motor being of diaphragm type using inflatable bodies that contract when fluid pressure is applied, e.g. pneumatic artificial muscles or McKibben-type actuators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/20—Fluid pressure source, e.g. accumulator or variable axial piston pump
- F15B2211/205—Systems with pumps
- F15B2211/20576—Systems with pumps with multiple pumps
- F15B2211/20592—Combinations of pumps for supplying high and low pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/40—Flow control
- F15B2211/405—Flow control characterised by the type of flow control means or valve
- F15B2211/40576—Assemblies of multiple valves
- F15B2211/40592—Assemblies of multiple valves with multiple valves in parallel flow paths
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/40—Flow control
- F15B2211/42—Flow control characterised by the type of actuation
- F15B2211/426—Flow control characterised by the type of actuation electrically or electronically
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/40—Flow control
- F15B2211/455—Control of flow in the feed line, i.e. meter-in control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/40—Flow control
- F15B2211/46—Control of flow in the return line, i.e. meter-out control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/60—Circuit components or control therefor
- F15B2211/63—Electronic controllers
- F15B2211/6303—Electronic controllers using input signals
- F15B2211/6336—Electronic controllers using input signals representing a state of the output member, e.g. position, speed or acceleration
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/60—Circuit components or control therefor
- F15B2211/665—Methods of control using electronic components
- F15B2211/6654—Flow rate control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/705—Output members, e.g. hydraulic motors or cylinders or control therefor characterised by the type of output members or actuators
- F15B2211/7051—Linear output members
- F15B2211/7052—Single-acting output members
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/75—Control of speed of the output member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/765—Control of position or angle of the output member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
- F15B2211/77—Control of direction of movement of the output member
- F15B2211/7716—Control of direction of movement of the output member with automatic return
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Analytical Chemistry (AREA)
- Actuator (AREA)
Description
Die Erfindung betrifft hochgenaue Positioniersysteme, z. B. für exterrestrische optische Spiegel. Hochgenaue Positioniersysteme benötigen spielfreie, vibrations freie und wartungsfreie Präzisionsantriebe für lineare Bewegungen von maximal ca. 50 mm Hub.The invention relates to highly accurate positioning systems, e.g. B. for extraterrestrial optical mirrors. High-precision positioning systems require backlash-free, vibrations Free and maintenance-free precision drives for linear movements of a maximum of approx. 50 mm stroke.
Aus DE 689 22 968 T2 und DE 41 36 119 A1 sind gattungsgemässe, rein elektrome chanische Linearantriebe für Anwendungen in der Raumfahrt bekannt.DE 689 22 968 T2 and DE 41 36 119 A1 are generic, purely electrome mechanical linear drives known for applications in space travel.
Aufgabe der Erfindung ist es, einen Präzisions-Linearantrieb mit folgenden Merkma
len zu schaffen:
The object of the invention is to provide a precision linear drive with the following features:
- - spielfrei,- play,
- - Wege (je nach Auslegung) ca. 50 mm,- paths (depending on the design) approx. 50 mm,
- - sehr kleine Geschwindigkeiten möglich (0 bis einige µm/s),- very low speeds possible (0 to a few µm / s),
- - sehr gute Geschwindigkeitskonstanz,- very good speed constancy,
- - hohe Stellkräfte.- high actuating forces.
Diese Aufgabe wird erfindungsgemäss durch den Gegenstand des Hauptanspruchs gelöst. Die Unteransprüche betreffen vorteilhafte Ausgestaltungen der Erfindung.This object is achieved by the subject matter of the main claim solved. The subclaims relate to advantageous refinements of the invention.
Ein Ausführungsbeispiel der Erfindung wird nachfolgend anhand einer Figur näher erläutert, die einen Linearantrieb in Seitenansicht zeigt.An embodiment of the invention is described in more detail below with reference to a figure explained, which shows a linear drive in side view.
Der beschriebene Linearantrieb besteht aus einem Faltenbalg 1 aus Metall oder Kunststoff, der mit einer Hydraulikflüssigkeit gefüllt und mittels einer Hydraulikleitung 2 mit einem Präzisionsnadelventil 3 als Stellelement und einem ersten Druck behälter 4 verbunden ist. Der Druckbehälter ist teilweise mit Flüssigkeit gefüllt, wobei ein Innendruck durch ein über der Flüssigkeit stehendes Gaspolster erzeugt wird.The linear actuator described consists of a bellows 1 made of metal or plastic, which is filled with a hydraulic fluid and by means of a hydraulic line 2 with a precision needle valve 3 as an actuator and a first pressure container 4 is connected. The pressure vessel is partially filled with liquid, an internal pressure being generated by a gas cushion above the liquid.
Bei Öffnung des Präzisionsventils 3 strömt Flüssigkeit vom ersten Druckbehälter 4 in den Faltenbalg 1, der dadurch eine lineare Stellbewegung in axialer Richtung ausführt. Mittels eines zweiten Stellelements 5 (Präzisionsnadelventil) kann Flüssig keit aus dem Faltenbalg 1 in einen zweiten drucklosen Behälter 6 zurückströmen. Dadurch kann bei gleichzeitiger Öffnung beider Ventile 3, 5 eine differentielle (sehr kleine) Geschwindigkeit am Faltenbalg 1 erzeugt werden.When the precision valve 3 is opened , liquid flows from the first pressure vessel 4 into the bellows 1 , which thereby executes a linear adjusting movement in the axial direction. By means of a second actuating element 5 (precision needle valve), liquid can flow back from the bellows 1 into a second pressureless container 6 . As a result, a differential (very low) speed can be generated on the bellows 1 when both valves 3 , 5 are opened at the same time.
Wird das mit dem ersten Behälter 4 verbundene Ventil 3 geschlossen, wird die Bewegung reversiert, da jetzt die parallel zum Faltenbalg 1 geschalteten Federelemente 7 Flüssigkeit aus dem Faltenbalg 1 zum zweiten Behälter 6 fördern. Um schnelles Vor- oder Zurückstellen des Aktuatorsystems zu initiieren, sind Bypassventile 8 grossen Querschnitts vorgesehen, über die der Balg 1 schnell mittels der Behälter 4 oder 6 befüllt oder entleert werden kann. Durch Öffnen des Ventils 9 kann die Flüssigkeit bei Bedarf aus dem Behälter 6 in den Behälter 4 zurückströmen (bei entsprechend eingestellter Druckdifferenz P2 < P1). Der Piezoaktuator 10 dient der Kompensation hochfrequenter Störsignale (z. B. von Rauschsignalen aus der Umgebung).If the valve 3 connected to the first container 4 is closed, the movement is reversed since the spring elements 7 connected in parallel with the bellows 1 now convey liquid from the bellows 1 to the second container 6 . In order to initiate rapid advancement or resetting of the actuator system, bypass valves 8 with a large cross section are provided, via which the bellows 1 can be quickly filled or emptied by means of the containers 4 or 6 . By opening the valve 9 , the liquid can flow back from the container 6 into the container 4 if necessary (with a correspondingly set pressure difference P2 <P1). The piezo actuator 10 is used to compensate for high-frequency interference signals (e.g. noise signals from the environment).
Alternativ kann die lineare Stellbewegung des Faltenbalgs 1 auch mittels zweier Mikropumpen (nicht gezeigt) erzeugt werden, die die Ventile 3 und 5 ersetzen. Beide Volumenströme können dann aus einem druckfreien Tank entnommen oder in diesen zurückgeführt werden.Alternatively, the linear actuating movement of the bellows 1 can also be generated by means of two micropumps (not shown) which replace the valves 3 and 5 . Both volume flows can then be taken from a pressure-free tank or returned to it.
Für die Volumenströme und Bewegungen gilt:
Q in < Q out: Bewegung in Richtung +X
Q in < Q out: Bewegung in Richtung -X
Q in = Q out: keine Bewegung.
The following applies to the volume flows and movements:
Q in <Q out: movement towards + X
Q in <Q out: movement in direction -X
Q in = Q out: no movement.
In der Figur ist weiter dargestellt:
Eine Endplatte 12, die Teil einer Struktur 14 ist. An dieser ortsfesten Endplatte stützt
sich ein Ende der Federelemente 7 ab, während das andere Ende der Federele
mente mit einer beweglichen Endplatte 16 in Verbindung steht.The figure also shows:
An end plate 12 that is part of a structure 14 . At this fixed end plate, one end of the spring elements 7 is supported , while the other end of the Federele elements with a movable end plate 16 is in communication.
Zur Geradführung der Platte 16 sind ölgeschmierte hermetisch abgedichtete Gleitla ger 18 vorgesehen, die auf Stangen 20 laufen, wobei die Stangen 20 an der Struktur 14 befestigt sind. Die hermetische Abdichtung der Gleitlager 18 erfolgt mittels der Faltenbalge 22.For straight guidance of the plate 16 , oil-lubricated hermetically sealed Gleitla ger 18 are provided, which run on rods 20 , the rods 20 being attached to the structure 14 . The slide bearings 18 are hermetically sealed by means of the bellows 22 .
Gesteuert wird das System mittels einer Steuerung über elektrische Leitungen, die
nachfolgend erläutert werden:
Leitung (Kabel) 26 verbindet die Steuerung mit P1 und Druckbehälter 4,
Leitung (Kabel) 28 verbindet die Steuerung mit P2 und Behälter 6,
Leitung (Kabel) 30 verbindet die Steuerung mit dem Präzisionsnadelventil 3,
Leitung (Kabel) 32 verbindet die Steuerung mit dem Präzisionsnadelventil 5,
die elektrischen Leitungen 34, 36 verbinden die Steuerung mit dem Piezo-Aktuator
10 und die elektrische Leitung 38 verbindet die Steuerung mit einer Laser-
Messeinrichtung 40.The system is controlled by means of a control via electrical lines, which are explained below:
Line (cable) 26 connects the control with P1 and pressure vessel 4 ,
Line (cable) 28 connects the control with P2 and container 6 ,
Line (cable) 30 connects the control with the precision needle valve 3 ,
Line (cable) 32 connects the control with the precision needle valve 5 ,
the electrical lines 34 , 36 connect the control to the piezo actuator 10 and the electrical line 38 connects the control to a laser measuring device 40 .
Claims (3)
einen Faltenbalg (1), der mit einem Aktuator (10) verbunden ist;
eine ortsfeste Endplatte (12), die ein Teil der Struktur (14) ist und mit einem Ende des Faltenbalgs (1) verbunden ist;
eine bewegliche Endplatte (16), die mit dem anderen Ende des Faltenbalgs (1) verbunden ist;
Zugfederelemente (7), die an beiden Endplatten (12; 16) befestigt sind;
ein Hydrauliksystem, das einen Faltenbalg (1) beaufschlagt, wobei Hydraulik mittel von einem ersten Behälter (4) über Leitungen (2) zum Faltenbalg (1) und vom Faltenbalg (1) über Leitungen (2) zu einem zweiten Behälter (6) geführt werden, die lineare Stellbewegung des Balgs über Stellelemente (3, 5) in den Leitungen gesteuert wird, den Stellelementen (3, 5) jeweils ein Bypassventil (8) zugeordnet ist und die beiden Hydraulikmittelbehälter (4, 6) direkt über eine Leitung mit einem Ventil (9) verbunden sind;
eine elektrische Steuerung (24) mit
elektrischen Leitungen (26, 28), die die Steuerung (24) mit P1, P2 und den Behältern (4, 6) verbinden;
elektrischen Leitungen (30, 32), die die Steuerung (24) mit den Stellelementen (3, 5) verbinden;
elektrischen Leitungen (34, 36), die die Steuerung (24) mit dem Aktuator (10) verbinden und
einer elektrischen Leitung (38), die die Steuerung (24) mit einer Messeinrich tung (40) verbindet.1. Linear drive for high-precision positioning of optical devices or the like for applications in space travel, characterized by :
a bellows ( 1 ) connected to an actuator ( 10 );
a fixed end plate ( 12 ) which is part of the structure ( 14 ) and is connected to one end of the bellows ( 1 );
a movable end plate ( 16 ) connected to the other end of the bellows ( 1 );
Tension spring elements ( 7 ) which are attached to both end plates ( 12 ; 16 );
A hydraulic system which acts on a bellows ( 1 ), hydraulic means being guided from a first container ( 4 ) via lines ( 2 ) to the bellows ( 1 ) and from the bellows ( 1 ) via lines ( 2 ) to a second container ( 6 ) the linear actuating movement of the bellows is controlled via actuating elements ( 3 , 5 ) in the lines, the actuating elements ( 3 , 5 ) are each assigned a bypass valve ( 8 ) and the two hydraulic fluid reservoirs ( 4 , 6 ) directly via a line with a Valve ( 9 ) are connected;
an electrical control ( 24 ) with
electrical lines ( 26 , 28 ) connecting the controller ( 24 ) to P1, P2 and the containers ( 4 , 6 );
electrical lines ( 30 , 32 ) connecting the controller ( 24 ) to the actuating elements ( 3 , 5 );
electrical lines ( 34 , 36 ) which connect the controller ( 24 ) to the actuator ( 10 ) and
an electrical line ( 38 ) connecting the controller ( 24 ) to a measuring device ( 40 ).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1999153934 DE19953934C2 (en) | 1999-11-10 | 1999-11-10 | Linear actuator for space applications |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE1999153934 DE19953934C2 (en) | 1999-11-10 | 1999-11-10 | Linear actuator for space applications |
Publications (2)
Publication Number | Publication Date |
---|---|
DE19953934A1 DE19953934A1 (en) | 2001-06-28 |
DE19953934C2 true DE19953934C2 (en) | 2002-03-21 |
Family
ID=7928467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1999153934 Expired - Fee Related DE19953934C2 (en) | 1999-11-10 | 1999-11-10 | Linear actuator for space applications |
Country Status (1)
Country | Link |
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DE (1) | DE19953934C2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116816768B (en) * | 2023-08-10 | 2024-05-07 | 中国科学院空间应用工程与技术中心 | Long-life fluid drive assembly with space capable of being rapidly disassembled |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4027899A1 (en) * | 1990-09-03 | 1992-03-12 | Gerhard Prof Dr Ing Wendt | Hydraulic servo for linear drive of piston - functions dependent on position of control unit formed as rocker |
DE4136119A1 (en) * | 1991-11-02 | 1993-05-06 | Erno Raumfahrttechnik Gmbh, 2800 Bremen, De | LINEAR ACTUATOR |
DE4244643A1 (en) * | 1991-11-27 | 1993-11-25 | Ortmann Albert | Damping device for actuation of space vehicle equipment - has oil-filled housing sealed by expansion bellows or by sealing membrane |
DE68922968T2 (en) * | 1988-09-08 | 1996-03-21 | Selenia Spazio Spa | Linear drive for antenna alignment, especially for space applications. |
-
1999
- 1999-11-10 DE DE1999153934 patent/DE19953934C2/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE68922968T2 (en) * | 1988-09-08 | 1996-03-21 | Selenia Spazio Spa | Linear drive for antenna alignment, especially for space applications. |
DE4027899A1 (en) * | 1990-09-03 | 1992-03-12 | Gerhard Prof Dr Ing Wendt | Hydraulic servo for linear drive of piston - functions dependent on position of control unit formed as rocker |
DE4136119A1 (en) * | 1991-11-02 | 1993-05-06 | Erno Raumfahrttechnik Gmbh, 2800 Bremen, De | LINEAR ACTUATOR |
DE4244643A1 (en) * | 1991-11-27 | 1993-11-25 | Ortmann Albert | Damping device for actuation of space vehicle equipment - has oil-filled housing sealed by expansion bellows or by sealing membrane |
Also Published As
Publication number | Publication date |
---|---|
DE19953934A1 (en) | 2001-06-28 |
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