GB2138149A - Wind indicator - Google Patents

Wind indicator Download PDF

Info

Publication number
GB2138149A
GB2138149A GB08409558A GB8409558A GB2138149A GB 2138149 A GB2138149 A GB 2138149A GB 08409558 A GB08409558 A GB 08409558A GB 8409558 A GB8409558 A GB 8409558A GB 2138149 A GB2138149 A GB 2138149A
Authority
GB
United Kingdom
Prior art keywords
indicator
status
datum
parachute
cord
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.)
Granted
Application number
GB08409558A
Other versions
GB2138149B (en
Inventor
Trevor Rowland Kirby-Smith
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from GB838310177A external-priority patent/GB8310177D0/en
Application filed by UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB08409558A priority Critical patent/GB2138149B/en
Publication of GB2138149A publication Critical patent/GB2138149A/en
Application granted granted Critical
Publication of GB2138149B publication Critical patent/GB2138149B/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00Indicating or recording presence, absence, or direction, of movement
    • G01P13/02Indicating direction only, e.g. by weather vane

Abstract

A device for indicating wind speed and direction to a parachutist comprises a datum element (10) for plummeting to the ground, a status element (13) having a parachute (14) for floating to the ground, a cord (17) linking the two elements, and different lights (12),(16) on each element. After the element (10) hits the ground the element (13) is carried, until it also reaches the ground, in the direction of the wind and for a distance proportional to the wind speed. <IMAGE>

Description

SPECIFICATION Wind indicator The present invention relates to wind direction indicators for use by parachutists, particularly parachutists using gliding parachutes.
By comparision with a traditional parachute the user of a gliding parachute is able to traverse fairly considerable lateral distances during his descent, and the difference between his lateral speed relative to the ground and that relative to the air affected by local wind speed and direction can be such as to affect the safety of landing. That is, if the wind is strong and behind him he could incur injuries on landing sufficient to immobilize him, whereas if it is strong and ahead his ground speed could be nil and his landing particularly safe. Moreover there are circumstances even in day time when the parachutist may not appreciate that his ground speed is dangerously high. Neither is an indication necessarily reliable if it comes from something streaming from or falling from the user, because air movement in the vicinity of the parachutist is unlikely to be representative.
The present invention provides a wind indicator which will give a parachutist adequate wind speed and direction information to enable him to adjust his ground speed before landing.
According to the present invention a wind indicator device comprises a datum element carrying a datum marker, a status element having a parachute and a marker, and a cord linking the datum element and the status element, the arrangement being such that the indicator is portable by a parachutist and droppable so that the datum element falls rapidly to the ground and the status element floats to the ground, the ground distance and direction of the status marker from the datum marker providing to the parachutist an indication of wind speed and direction.
In a first embodiment of the invention the indicator is arranged so that the status parachute is uninflated for a landing phase of the datum element, whereby the combination effectively plummets to the ground, the status element parachute only inflating after the datum element has landed. Accordingly the cord may pass freely via a collar approximate the status parachute line confluence and be attached to the apex of the status parachute canopy.
In a second embodiment the weight of the datum element may be arranged to be such with respect to the size of the status element parachute as to prevent the latter affording significant resistance to free fall of the combination.
Advantageously the status parachute has a cruciform canopy, whereby wind life effects thereon are minimised. The parachute lines may possess a degree of stiffness to enable them to avoid entanglement.
In order to ensure that the cord, which may be of the order of 30 metres long, deploys readily when the indicator is dropped, the device may include a cord store for paying out cord. A suitable cord store is described in co-pending UK Patent application of Agent's 8310176 and comprises a series of loops of the cord stuck between a pair of adhesive tapes, one end of the store being anchored to the datum element. The adhesive may be a wax.
Preferably the cord is so stored that when deployment of the device is initiated by the device being allowed to fall freely as a whole, the parachute inflates in order for the status element to float downward while the datum element is plummetting and cord is paying out from the store.
Whilst the wind indicator may be arranged to be deployed progressively from the person, with the apparently concomitant possibility of minimising the distance between the device and the user just prior to his landing, it is much preferred for itto be arranged to be released from the person as a whole and to deploy after release. This latter mode of deployment minimises the possibility of parachutist motion affecting the final relative positions of the datum and status markers.
Accordingly the device may have a pouch attachable to the person, be releasable as a whole therefrom, and arranged to deploy progressively thereafter, as above described.
At least the datum marker may have ribbons of a glowing fabric, such as a fabric coated with a phosphorescent, eg 'DAYGLO' (TM), preparation.
Both markers may incorporate light emitters of the type comprising two fluids which emit light upon mixing. Atypical example is the 'Cyalume' (Registered Trade Mark of American Cyanamid Co) light-stick which is activated by flexing the tube.
Preferably the datum and status markers are different colours.
Typically the datum element has a width of order of 0.4-0.5 Kg, and the status parachute carries a load of 0.15-0.25 Kg. These weights may comprise lead shot, so that the whole wind indicator can be so packed that a singleflexure prior to dropping activates the marker light. However the loads may comprise parts of a parachutist's other equipment when weight is at a great premium.
Two wind indicator devices in accordance with the present invention will now be described by way of example with reference to the accompanying drawings, of which: Figure 1 illustrates an unpacked indicator of a first device prior to deployment, Figure 2 is a schematic section of a packed indicator of the type illustrated in Figure 1, Figure 3 schematically illustrates a second indicator, unpacked, and Figure 4 schematically illustrates a second indicator, packed.
The indicator shown in Figures 1 and 2 comprises a datum element 10 incorporating a datum weight 11 and a datum marker 12, a status element 13 incorporating a cruciform parachute 14 with a status load 15 and a market 16, and a cord 17 linking the datum and status elements.
The parachute has lines 14a formed of nylon cord which connect with the load 15 via a confluence ring 18, to which the lines and the load are attached. The cord 17 passes through the ring 18 and is attached to the apex of the parachute 14. The markers are 'CYALUME' (RTM) Light-sticks, the datum marker 12 being tinted orange. They are attached to their respective loads, which comprise flexible tubes of lead shot.
The cord 17 is formed into a cord store, in which a series of loops of the cord are retained in that belt array by adhesive tape 17a, attached to both sides thereof, the store being packaged in a plastics film tube 17b.
The device is packaged in a compartmented envelope 20 so flexible as to permit the lightsticks to be flexed prior to opening the envelope. The envelope 20 is attachable to the person via a cover 21, and is openable to permit the device to fall away completely.
There now follows a description of the operation deployment and use of this device by a parachutist.
Just prior to a night-time jump he gently flexes the complete device so that both lightsticks 12, 16 begin to glow (for a day time jump this may not be necessary). He then attaches the envelope 20 containing it to his clothing via the cover 21. After the jump, when he reaches a specified altitude he opens the cover 21 and the envelope 20, allowing the device to fall therefrom. The parachute 14 inflates, as a result of which the datum element 10 falls faster than the status element 13 and the cord 17 is pulled out of the store. When the cord 17 is taut it draws the apex of the parachute 14 to the confluence ring 18 deflating the parachute so that the device can plummet groundwards.
When the datum element 10 reaches the ground, tension on the cord 17 relaxes except in very strong winds, the parachute 14 re-inflates and the status element 13 then floats to the ground, the datum element 10 remaining stationary. The status element 13 then lands on the ground at a point a distance and direction from the datum element commensurate with wind speed and direction respectively.
In a typical embodiment of the invention the datum and status element weights are 0.45 Kg and 0.19 Kg respectively, and the cord 17 is 30 m long.
The parachute 14 has an arm total length of 48 cm and an arm width of 12 cm and eight lines 14a 48 cm long. If this is released by a parachutist at 150 m altitude it will have 8 or 9 seconds in which to assess the wind and adjust his direction for landing.
In the second embodiment of the invention, shown in Figures 3 and 4, the indicator itself differs from the first embodiment principally in that the datum unit carries no load 14 addition to the marker 16, in place of the confluence ring 18 is a simple swivel confluence 30, and there is no facility of exchanging the marker 16 for ribbons (since the parachute canopy can be arranged for daylight visibility).
The package for the device, shown in Figure 4, comprises a polythene tubular inner envelope 40 in which the device is arranged, with an inner tube 40 or for the parachute 14, and a nylon fabric envelope 41 into which the envelope 40 can be arranged by means of tapes 42. The envelope 41 has a cord 43 by which it can be attached to the person and a flap 44, closable by touch-and-close fastener means 45, to retain closed to envelope 40.
For operation of this second embodiment, the parachutist gently bends the package to activate the light stick, if necessary, and attaches it to his person via the cord 43. When, after jumping, the parachutist has an altitude of about 150 m he opens the nylon flap 44 and points the tube 40 downward, permitting the device to slide out of the tube. Because initially there is less drag associated with the datum element than with the status element the former falls more rapidly than the latter whilst the line 17 deploys.
When the line is taut the status element is caused to fall rapidly due to the mass of the datum element, until the latter hits the ground, when the status element begins to float to a location on the ground determined by wind speed and direction.
In a specified form of the second embodiment the datum element carries a weight 11 of 0.45 Kg, while the parachute 14 has an arm length of 22 cm, an arm width of 5.5. cm and a line of a length of 30 cm.

Claims (12)

1. Awind indicator comprising a datum element carrying a datum marker, a status element having a parachute and a marker, and a cord linking the datum element and the status element, the arrangement being such that the indicator is portable by a parachutist and droppable so that the datum element falls rapidly to the ground and the status element floats to the ground, the ground distance and direction ofthe status marker from the datum marker providing to the parachutist an indication of wind speed and direction.
2. A wind indicator as claimed in claim 1 and arranged so that the status parachute is uninflated for a landing phase of the datum element, whereby the combination effectively plummets to the ground, the status element parachute only inflating after the datum element has landed.
3. A wind indicator as claimed in claim 2 and wherein the cord passes freely via a collar approximate the status parachute line confluence and is attached to the apex of the status parachute canopy.
4. A wind indicator as claimed in claim 1 and wherein the weight of the datum element is arranged to be such with respect to the size of the status element parachute as to preventthe latter affording significant resistance to free fall of the combination.
5. A wind indicator as claimed in any one of claims 1 to 4 and wherein the status parachute has a cruciform canopy, whereby wind life effects thereon are minimised.
6. Awind indicator as claimed in any one of the preceding claims and wherein the parachute lines possess a degree of stiffness to enable them to avoid entanglement.
7. A wind indicator as claimed in any one of the preceding claims and wherein the cord store comprises a series of loops of the cord stuck between a pair of adhesive tapes, one end of the store being anchored to the datum element.
8. Awind indicator as claimed in any one of the preceding claims and wherein the cord is so stored that when deployment of the device is initiated by the device being allowed to fall freely as a whole, the parachute inflates in order for the status element to float downward while the datum element is plummetting and cord is paying out from the store.
9. Awind indicator as claimed in any one of the preceding claims and having a pouch attachable to the person, the indicator being the person, be releasable as a whole therefrom, and arranged to deploy progressively thereafter.
10. A wind indicator as claimed in any one of the preceding claims the datum marker has ribbons of a glowing fabric.
11. A wind indicator as claimed in any one of the preceding claims the markers incorporate light em itters of the type comprising two fluids which emit light upon mixing.
12. Awind indicator substantially as hereinbefore described with reference to the accompanying drawings.
GB08409558A 1983-04-14 1984-04-12 Wind indicator Expired GB2138149B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08409558A GB2138149B (en) 1983-04-14 1984-04-12 Wind indicator

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB838310177A GB8310177D0 (en) 1983-04-14 1983-04-14 Wind indicator
GB08409558A GB2138149B (en) 1983-04-14 1984-04-12 Wind indicator

Publications (2)

Publication Number Publication Date
GB2138149A true GB2138149A (en) 1984-10-17
GB2138149B GB2138149B (en) 1987-06-24

Family

ID=26285830

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08409558A Expired GB2138149B (en) 1983-04-14 1984-04-12 Wind indicator

Country Status (1)

Country Link
GB (1) GB2138149B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2421229A (en) * 2004-12-14 2006-06-21 Maxine Von Wollenmann Parachute canopy with light-emitting means

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2045521A (en) * 1934-04-30 1936-06-23 Hertelendy Andor De Wind direction indicator
US3869913A (en) * 1972-06-01 1975-03-11 Shale J Niskin Method and apparatus for determining surface wind velocity

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2045521A (en) * 1934-04-30 1936-06-23 Hertelendy Andor De Wind direction indicator
US3869913A (en) * 1972-06-01 1975-03-11 Shale J Niskin Method and apparatus for determining surface wind velocity

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2421229A (en) * 2004-12-14 2006-06-21 Maxine Von Wollenmann Parachute canopy with light-emitting means
GB2421229B (en) * 2004-12-14 2006-11-22 Maxine Von Wollenmann Illuminated parachute

Also Published As

Publication number Publication date
GB2138149B (en) 1987-06-24

Similar Documents

Publication Publication Date Title
EP1233905B1 (en) Launch and recovery system for unmanned aerial vehicles
US9669946B2 (en) Launch and recovery system for unmanned aerial vehicles
US4337913A (en) Means for releasably attaching strands
US7204049B2 (en) Emergency drop system for an aircraft advertising display
US4623109A (en) Low altitude parachute system
US6814638B2 (en) Airdrop type buoy apparatus
CN109204834A (en) Flapping wing landing knapsack
US3724817A (en) Long line loiter technique
CN209567087U (en) Flapping wing landing knapsack
US6505575B1 (en) Location indicator and method
US4554827A (en) Wind indicators
GB2138149A (en) Wind indicator
US5622337A (en) Method and reference point apparatus for training free fall parachutists
US2998950A (en) Integrated parachute deployment pack
US4487102A (en) Stowage pack for controlled bomb/mine lanyard payout
US3612448A (en) Aerial delivery system
US3420479A (en) Tree snagging parachute
US4850128A (en) Aerial fish probe
US2997259A (en) Balloon weigh-off and launching means and method
AU764504C (en) Emergency drop system for an aircraft advertising display
KR200166363Y1 (en) Deployment bag with pilotchute for rescue parachute
Kalabukhova et al. UT-15, series 2 parachute
GB2107675A (en) Rope dispenser
EP0085686A1 (en) Store delivery by retarder
Hennings et al. Design and Testing of a Collapsible Drogue Parachute for the X-37 Vehicle

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940412