SEPARATION DEVICE FOR SPACECRAFT AND A METHOD FOR SEPARATION
20200346788 · 2020-11-05
Inventors
- Jörgen Remmelg (Vikingstad, SE)
- Örjan Arulf (Linköping, SE)
- Anders Helmersson (Linköping, SE)
- Daniel Wramell Kristoffersson (Linköping, SE)
Cpc classification
B64G1/641
PERFORMING OPERATIONS; TRANSPORTING
International classification
B64G1/64
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The invention relates to a separation device for a spacecraft or launcher. The separation device includes an inner housing divided into at least two portions locked to each other by a locking device in a locking position. The locking device is arranged to move between a locking position and a releasing position. The separation device includes an initiator including means for providing high pressure fluid to an expansion chamber when the separation device is switched from a locked state to a released state. The high pressure fluid in an expansion chamber moves the locking device from the locking position to the releasing position when the separation device is switched from the locked state to the released state. The separation device includes a dampening arrangement arranged to attenuate a peak load when the separation device is switched from the locked state to the released state.
Claims
1. A separation device (1) for a spacecraft or launcher, the separation device (1) comprising an inner housing (2) divided into at least two portions locked to each other by a locking device (3) in a locking position, the locking device (3) being arranged to move between a locking position and a releasing position, the separation device (1) comprising an initiator (5) comprising means for providing high pressure fluid to an expansion chamber (6) when the separation device (1) is switched from a locked state to a released state, wherein the high pressure fluid in an expansion chamber (6) moves the locking device (3) from the locking position to the releasing position when the separation device (1) is switched from the locked state to the released state, characterized in that the separation device (1) comprises a dampening arrangement (8) arranged to attenuate a peak load when the separation device (1) is switched from the locked state to the released state.
2. A separation device (1) according to claim 1, wherein the dampening arrangement (8) comprises a guiding means (22) arranged to guide the locking device (3) into a rotational movement when the locking device (3) moves from the locking position to the releasing position.
3. A separation device (1) according to claim 2, wherein the guiding means (22) is a part of the locking device (3).
4. A separation device (1) according to claim 2 or 3, wherein the guiding means (22) comprises a spirally formed recess (23) and a protrusion (24), wherein the guiding means (22) comprises a spirally formed recess (23) in the locking device (3) arranged to cooperate with a protrusion (24) arranged in a surrounding housing (13) or wherein the guiding means (22) is a spirally formed recess (25) in the surrounding housing (13) arranged to cooperate with a protrusion (26) arranged in the locking device (3).
5. A separation device (1) according to any one of claims 2-4, wherein the surrounding housing (13) is the outer housing (13) or an intermediate housing between the outer housing (13) and the locking device (3).
6. A separation device (1) according to any one of the preceding claims, wherein the dampening arrangement (8) comprises a dampening plate (9) in an end position in connection to the releasing position, wherein the dampening arrangement (8) comprises at least one dampening pin (11) arranged between the locking device (3) and the dampening plate (9), wherein the dampening pin (11) is arranged to hit and plastically deform the dampening plate (9) during movement of the locking device (3) from the locking position to the releasing position for absorbing energy from the locking device (3) which attenuates the peak load.
7. A separation device (1) according to claim 6, wherein the dampening pin (11) comprises a pointy end with an angle that allows for the material in the dampening plate (9) to be pressed at an angle to the travelling direction of the dampening pin (11).
8. A separation device (1) according to any one of claim 6 or 7, wherein the dampening plate (9) comprises a guiding plate (10) arranged to hold and guide the dampening pin (11), wherein the locking device (3) is arranged to hit the dampening pin (11) during movement of the locking device (3) from the locking position to the releasing position.
9. A separation device (1) according to any one of claims 6-8, wherein the dampening pin (11) is arranged in connection to the locking device (3), wherein the dampening pin (11) hits the dampening plate (9) during movement of the locking device (3) from the locking position to the releasing position.
10. A separation device (1) according to any one of the preceding claims, wherein the separation device (1) comprises an outer housing (13) having an extension in a longitudinal direction and comprising a first end plate (14) covering a first end portion (14a) of the outer housing (13) and a second end plate (15) covering a second end portion (15a) of the outer housing (13) positioned opposite the first end portion (14a), wherein the second end plate (15) is arranged in connection to the end position, wherein the inner housing (2) is positioned within the outer housing and attached to the second end plate (15), wherein the second end plate (15) comprises the dampening plate (9).
11. A separation device (1) according to claim 10, wherein the locking device (3) is slidably arranged between the locking position and the releasing position within the outer housing and about the inner housing (2).
12. A separation device (1) according to claim 10 or 11, wherein the expansion chamber (6) is positioned between the first end plate and the locking device (3), and wherein the high pressure fluid in the expansion chamber (6) moves the locking device (3) from the locking position to the releasing position in a direction from the first end portion towards the second end portion in the longitudinal direction.
13. A separation device (1) according to any one of the preceding claims, wherein the locking device (3) is a sleeve slidably arranged between the locking position and the releasing position.
14. A separation device (1) according to any one of the preceding claims, wherein the separation device (1) comprises an ejector (18) slidably arranged between the locking position and the releasing position in a channel (19) within the inner housing (2), wherein the expansion chamber (6) is arranged to be in fluid communication with the channel (19).
15. A separation device (1) according to any one of the previous claims, wherein the locking device (3) comprises locking means (7) arranged to engage an inner portion of the outer housing and an outer portion of the inner housing (2) thereby locking the inner housing (2) and hindering separation of the inner housing (2).
16. A separation device (1) according to any one of the previous claims, wherein the separation device (1) comprises a plurality of dampening pins (11).
17. A separation device (1) according to any one of the preceding claims, wherein the initiator (5) comprises at least two initiator units (5).
18. A separation device (1) according to claim 17, wherein the initiator units (5) are arranged to ignite simultaneously.
19. A separation device (1) according to claim 17, wherein the dampening arrangement (8) comprises a control unit (8a) arranged to initiate the initiator units (5) in a sequence with a time interval for chock peak attenuation.
20. A separation device (1) according to any one of the preceding claims, wherein the initiator (5) is a pyrotechnic unit.
21. Method for a separation device (1) according to any one of claims 1-20, wherein the method comprises the steps of: initiating an initiator (5) comprising means for providing high pressure fluid to an expansion chamber (6) when the separation device (1) is switched from a locked state to a released state, moving the locking device (3) from a locking position to a releasing position when the separation device (1) is switched from a locked state to a released state by the high pressure fluid in the expansion chamber (6), attenuating a peak load with a dampening arrangement (8) when the separation device (1) is switched from the locked state to the released state.
22. A method according to claim 21, wherein the dampening arrangement (8) comprises a guiding means (22) and wherein the method comprises the step of the guiding means (22) guiding the locking device (3) into a rotational movement when the locking device (3) moves from the locking position to the releasing position.
23. A method according to claim 21 or 22 , wherein the method comprises the step of plastically deforming a dampening plate (9) with dampening pin(s) (11) when the dampening pin(s) (11) hits the dampening plate (9) for absorbing energy from the locking device (3) for attenuating the peak load.
24. A method according to any one of claims 21-23, wherein the initiator (5) comprises at least two initiator units (5), and wherein the initiator units (5) are arranged to ignite simultaneously or wherein the initiator units (5) are ignited in sequence with a time interval for chock peak attenuation.
Description
BRIEF DESCRIPTION OF DRAWINGS
[0043] The disclosure will be described in greater detail in the following, with reference to the attached drawings, in which;
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DESCRIPTION OF EXAMPLE EMBODIMENTS
[0061] Various aspects of the disclosure will hereinafter be described in conjunction with the appended drawings to illustrate and not to limit the disclosure, wherein like designations denote like elements, and variations of the described aspects are not restricted to the specifically shown embodiments, but are applicable on other variations of the disclosure.
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[0063] In a spacecraft or a launcher a payload (not shown) is mounted to a dispenser body (not shown) forming a dispenser assembly. The payload is mounted and secured to the dispenser body by the separation devices 1 arranged to release the payload at a certain position in space. In order to solve the problem of shock peaks in the payload assembly, the separation device 1 comprises a dampening arrangement 8. In
[0064] Should the dampening comprise a guiding plate 10, then the dampening pin 11 could be arranged in corresponding openings 12 in the guiding plate 10.
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[0068] The fastening means 20 may also be part of the separation device 1 in
[0069] It should be noted that in
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[0072] The following is with reference to
[0073] According to one example, the sleeve 3 is slidably arranged between the locking position and the releasing position within the outer housing 13 and about the inner housing 2. Here, the sleeve is a ring shaped unit comprising locking means 7 arranged to engage an inner portion 16 of the outer housing 13 and an outer portion 17 of the inner housing 2 thereby locking the inner housing 2 and hindering separation of the inner housing 2.
[0074] In the figures, the expansion chamber 6 is positioned between the first end plate 14 and the sleeve 2.
[0075] According to one example shown in
[0076] According to one example, the high pressure fluid in the expansion chamber 6 moves the sleeve 3 from the locking position to the releasing position in a direction from the first end portion 14a towards the second end portion 15a in the longitudinal direction.
[0077] According to one example, the second end plate 15 comprises the guiding plate 10 and the dampening plate 9, wherein the dampening pin 11 is arranged to protrude into a space 21 between the second end plate 15 and the sleeve 3 when the separation device 1 is in the locked state.
[0078] According to
[0079] According to one example, the initiator units 5 are ignited in sequence with a predetermined time interval for additional chock peak attenuation. This arrangement has the advantage of a secure release operation with at least one backup initiator unit. The arrangement has the further advantage of chock peak attenuation due to the ignition delay. The ignition delay, i.e. the predetermined time interval, gives that the shock peak from one initiator unit 5 becomes offset the shock peak from another initiator unit 5. Together with the dampening pin 11 and the dampening plate, the sequenced ignition gives an increased shock peak attenuation compared to any of the dampening pin 11 and sequenced ignition taken separately. Both of them taken separately gives the benefit of securing release and at the same time allowing for an even more lightweight and slim construction. However, the combination of the dampening plate 9 and/or the sequenced ignition and or/the guiding means in
[0080] According to one example, the separation device 1 comprises a plurality of dampening pins 11 and a corresponding number of openings 12 in the guiding plate 10. In
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[0082] Box 141:
[0083] initiating an initiator 5 comprising means for providing high pressure fluid to an expansion chamber 6 when the separation device 1 is switched from a locked state to a released state,
[0084] Box 142
[0085] moving the sleeve from a locking position to a releasing position when the separation device 1 is switched from a locked state to a released state by the high pressure fluid in the expansion chamber 6,
[0086] Box 143
[0087] attenuating a peak load with a dampening arrangement 8 when the separation device 1 is switched from the locked state to the released state
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[0089] Box 143a
[0090] plastically deforming a dampening plate 9 with dampening pin(s) 11 when the dampening pin 11 penetrates the dampening plate 9 for absorbing energy from the movement of the locking device 3.
[0091] Box 143b
[0092] the initiator 5 comprises at least two initiator units, and the initiators are ignited in sequence with a time interval for chock peak attenuation.
[0093] Box 143c
[0094] the dampening arrangement 8 comprises a guiding means 22 and the method comprises the step of the guiding means 22 guiding the locking device 3 into a rotational movement when the locking device 3 moves from the locking position to the releasing position
[0095] It should be noted that the step in Box 143a can be done using one initiator or two or more initiators arranged to ignite simultaneously or with a time interval according to Box 143b. In Box 143a the locking device 3 can be arranged to hit the pin(s) such that the pin is driven into the dampening plate 9. As an alternative, the pin(s) can be arranged in connection to the locking device 3 such that the pin(s) travel together with the locking device 3 towards the dampening plate 9 before hitting the dampening plate 9.
[0096] The pin(s) advantageously comprises a pointy end that penetrates the dampening plate 9 and presses the material in the dampening plate 9 in a direction at an angle to a traveling direction if the pin(s). The angle of the pointy end decides how the pin(s) affects the dampening plate 9 in a known manner with relation to force components. The choice of material in the dampening plate 9 together with the angle of the pointy end are design parameters that is optimized dependent on desired outcome and will not be described further.
[0097] According to one example each initiator 5 is a pyrotechnic unit that generates a high pressure fluid in the form of hot combustion gas.
[0098] The separation device 1 described in connection to
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[0111] It should be noted that the protrusions 24, 26 in
[0112] It will be appreciated that the above description is merely exemplary in nature and is not intended to limit the present disclosure, its application or uses.
[0113] While specific examples have been described in the specification and illustrated in the drawings, it will be understood by those of ordinary skill in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure as defined in the claims. Furthermore, modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular examples illustrated by the drawings and described in the specification as the best mode presently contemplated for carrying out the teachings of the present disclosure, but that the scope of the present disclosure will include any embodiments falling within the foregoing description and the appended claims. Reference signs mentioned in the claims should not be seen as limiting the extent of the matter protected by the claims, and their sole function is to make claims easier to understand.