Lubrication system for a mechanism, in particular for a rotary bearing in a spacecraft

• US 6,085,871 A
• Filed: 09/09/1998
• Issued: 07/11/2000
• Est. Priority Date: 09/10/1997
• Status: Expired due to Fees

• Current Assignee: Agence Spatiale Europeenne
• Original Assignee: Agence Spatiale Europeenne
• Inventors: Karamata, Boris
• Primary Examiner(s): Graysay, Tamara L.
• Assistant Examiner(s): KIM, CHONG HWA
• Application Number:
  US09/150,299
• Time in Patent Office: 671 Days
• Field of Search: 184/32, 184/27.1, 184/27.4, 184/79, 184/75, 222/333, 222/378, 137/807, 251/355, 251/129.06, 417/417, 417/489
• US Class Current: 184/75
• CPC Class Codes: F16N 17/00 Lubrication of machines or apparatus working under extreme conditions additives to lubricating oil or lubricating grease C10M
• CPC Class Codes: F16N 17/06 in vacuum or under reduced pressure lubrication of evacuating pumps F04; of rotary anodes of X-ray tubes H01J35/10
• CPC Class Codes: F16N 29/00 Special means in lubricating arrangements or systems providing for the indication or detection of undesired conditions; Use of devices responsive to conditions in lubricating arrangements or systems
• CPC Class Codes: F16N 7/36 with feed by pumping action of the member to be lubricated or of a shaft of the machine; Centrifugal lubrication
• CPC Class Codes: Y10T 137/2082 Utilizing particular fluid

Abstract

The invention relates to a lubrication system for a mechanism (27), on-board a spacecraft. It comprises a non pressurized tank (20) communicating with the mechanism (27) via a tube (220). A piston (23) closes the tube (220) while the mechanism is at rest. The piston (23) is controlled by a first spring (5) and by a second, shape memory, spring (24) opposing the latter, which lengthen by thermal effect. A controller (25, 26) supplies this spring with a current (I) to actuate it. An annular element(7), pushed by a cylindrical spring (6), defines a capillarity filled pumping chamber (22). When the temperature of the shape memory alloy (24) falls back below a threshold, the spring (24) recovers its original shape, the first spring (5) pushes back the piston (23) and expels a dose of lubrication fluid (4).

Claims

1. Lubrication system for a mechanism, comprising a non pressurized tank, containing a lubrication fluid, and a distribution channel for said fluid having a first port and a second port, opening through the first port into said tank and supplying through the second port said mechanism to be lubricated, wherein said lubrication system comprises:

a piston reciprocating inside the tank in translation along its longitudinal axis, so as to provide two determined states, a first state in which said piston obturates said first port of the distribution channel, and a second state in which said piston is at a determined distance from said first port of the distribution channel, so as to create a pumping enclosure, of a determined volume, communicating by capillarity in said second state with the tank, and allow said lubricating fluid penetrating therein, and

control means for said piston causing a motion from said first state to said second state, so as to fill said pumping enclosure by capillarity effect, and a motion in the opposite direction from said second state to said first state, so as to expel via said distribution channel a determined volume of lubricating fluid towards said mechanism to be lubricated.

2. System according to claim 1, wherein said tank comprises a main body having a first wall with a channel opening into the interior of tank, said first port of said distribution channel opens into a second wall opposite to said first wall, said piston is disposed in said channel and comprises a head having a section the same section as a section of the channel, and said piston control means comprise a first spring which pushes said head back towards the first port of the distribution channel and a shape memory actuator member, taking when actuated a first predetermined geometric shape so as to exert a driving force on the piston to bring it into said first state, and taking when non activated a second predetermined geometric shape so as to authorize the piston returning to said first determined state.

3. System according to claim 2, wherein said shape memory actuator member is a helical spring with turns, said control means of the piston further comprise an electric power supply and a switch disposed in series with said turns, so as to heat up, when said switch is closed, said helical spring by allowing a flow of an electric current, and so as to cause a swing from said second predetermined geometrical shape to said first predetermined geometrical shape by means of a thermal effect lengthening of the spring, of a determined magnitude, and a return to said second predetermined geometrical shape is obtained through spontaneous cooling of said material below a determined threshold, when said switch is open and disconnects said electric power supply (26).

4. System according to claim 3, wherein said switch is under control of electronic circuits which according to a determined cycle generate opening and closing control signals so as to obtain a succession of said first and second states of said piston, and to supply said mechanism to be lubricated, at predetermined time intervals, with doses of lubrication fluid of a determined volume.

5. System according to claim 2, wherein said second wall of the tank includes an annular chamber, wherein said annular chamber contains a tubular element and a cylindrical spring disposed between said tubular element and a bottom of said annular chamber, so as to push back said tubular element in order for it to press against said head of piston, wherein under the thrust of said cylindrical spring, said tubular element is driven inside said tank in a translation motion of a limited magnitude when said piston is in said second state, so as form a transverse wall of said pumping enclosure, and wherein said limited magnitude is such that an annular overture remains between the head of said piston and said tubular element, so as to allow filling said pumping enclosure by capillary effect.

6. System according to claim 5, wherein said determined distance between the piston and said first port is equal to twice said translation motion of a limited magnitude.

7. System according to claim 2, wherein said pumping enclosure consists of a pot with a cylindrical wall, closed by a bottom disk made of a material with resilient properties, wherein said bottom has a central opening orifice prolonged by a rigid tube, inserted in said second wall of tank, and communicating with said distribution channel, wherein an end of said cylindrical wall of the pot has a profile of a first determined shape, wherein said head of piston has an annular profile of a second determined shape, complementary to said first determined shape, so that they engage into each other and constitute a seal when the head of piston nears said pot, upon returning from said first state to said second state, and wherein the translation motion causes resilient deformation of said bottom and the expulsion of the lubrication fluid present in said pumping enclosure toward said mechanism to be lubricated, via said rigid tube and the distribution channel.

8. System according to claim 7, wherein said profiles of determined shapes are bevels, with the bevel of the annular profile of the head of piston facing inwardly and the bevel of the profile of the end of said wall of pot facing outwardly.

9. System according to claim 1, wherein the interior of said tank has a biconical revolution shape around said longitudinal axis.

10. System according to claim 1, wherein said lubrication system is adapted to be mounted in a spacecraft, having a rotary bearing to be lubricated.