US2432509A - Glider pickup device - Google Patents
Glider pickup device Download PDFInfo
- Publication number
- US2432509A US2432509A US559720A US55972044A US2432509A US 2432509 A US2432509 A US 2432509A US 559720 A US559720 A US 559720A US 55972044 A US55972044 A US 55972044A US 2432509 A US2432509 A US 2432509A
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- United States
- Prior art keywords
- coupling
- glider
- sleeve
- collar
- cylinder
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- 230000008878 coupling Effects 0.000 description 26
- 238000010168 coupling process Methods 0.000 description 26
- 238000005859 coupling reaction Methods 0.000 description 26
- 230000001133 acceleration Effects 0.000 description 2
- 244000299507 Gossypium hirsutum Species 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
Definitions
- the invention herein disclosed relates to glider pick-up apparatus of the type in which the glider which is at rest to begin with, is given a steady acceleration by energy obtained from a plane in flight until it reaches the speed of the plane, at which time a towline which has been picked up by the plane and which is connected to the apparatus, is released therefrom, and is gripped by a device on the glider for the subsequent towing of the glider by the plane.
- the present application is a division of application Serial No. 507,931, led October 28, 1943, and is for the release means referred to above.
- the energy necessary for accelerating the glider with a steady and reasonable acceleration is transferred from the plane in flight until the Yglider attains the speed of the plane, and then the towline is fixed for the subsequent towing of the glider by the plane. This is accomplished without the necessity of carrying any of the apparatus in the glider or the plane, except for a very light pulley on the glider comprising a part oi the gripping means and a light pick-up hook on the plane.
- a hydraulic mechanism is used in the operation of this apparatus against a pressure accumulator to provide a continuous. steady pull on one end of the towline which is passed around the pulley at the nose of the glider while the other end of the towline is being pulled by the plane, thus storing a part of the energy during the rst part of the accelerating operation above referred to while the gliders Velocity is low, and returning it during-the latter part thereof, thereby continuously providing only half of the steady accelerating force to the glider, the other half being in the meantime supplied to the glider directly from the plane through the other portion of the towline passed around the pulley.
- the apparatus thus includes a take-up line connested between the hydraulic means ard the towline which is passed around the pulley on the glider.
- the object of the present invention is to provide means to release the towline from the take-up line when the glider reaches the speed ci the plane.
- a further object is to provide a coupling between the towline and the take-up line which will break the connection upon impact or pressure of the coupling against a buffer sleeve through which the take-up line is passed.
- Fig. 1 is a perspective view of the deck sheave post and buffer assembly used in the above referred to apparatus
- Fig. 2 is a cross-sectional view of the buier and the releasable coupling between the towline and take-up line prior to release.
- Fig. 3 is the same view with the parts in position immediately after release, the broken line iigure showing the towline end fitting broken away from the rest of the coupling an instant later,
- Fig. 4 is a cross-section taken at 4--4 of Fig. 2.
- the buffer sleeve 34 has an inner shoulder 43 against which the slidable collar member 36 is normally resiliently held by spring 3l, the other end of which is biased against the iixed collar member 44.
- Take-up line 33 passes through this buffer and is attached to the coupling plug 45 fitted against an inner shoulder in sleeve 38 and supporting one end of spring il therein, the other end of which biases a pin member le which extends through a collar fixed in the end of the sleeve 38.
- the other end of sleeve 38 has a series of resilient prongs 39 extending therefrom around its periphery.
- prongs have a collar 4l) mounted around their wedge formed ends so that when the collar is pushed over the wedged portions it brings the prongs radially toward the axis of the coupling.
- a peripheral shoulder formed by projections on the prongs is thereby moved radially within the cir ⁇ cumference of the sleeve. while normally it has a greater diameter and is adaptable to hook over an internal shoulder 6l formed in a groove on the inside of the cylinder 35 comprising the other part of the coupling which is attachedat 5i) tothe towline 3.
- the closed end of this cylinder forces the pin member 48 in against the pressure of spring il when the coupling is locked.
- a coupling co-nnecting two lines, a buer through which one of the lines passes comprising a collar resiliently held against axial displacement, and means on said coupling Vto release it when the line is moved through the buier so as to cause the coupling to strike said collar .in an axial direction ltending to displace it, including slidable means on said coupling, and resilient ejecting means for separating said coupling upon its release.
- a releasable two-part coupling having each part connected to one portion of an automatically ⁇ breakable line, -a buffer element having a resiliently urged member, one portion of the line passing through said member, a releasing means on the part of the coupling nearest the buffer, so that as the line moves through the buifer the releasing means strikes the resiliently urged member in the buier and the reaction releases the two parts of the coupling, and resilient means in one of said coupling parts for urging them apart.
- a releasa'ble coupling connecting two portions ,of an automatically breakable line comprising a cylinder having a elo-sed end connected to one of said portions, a coupling plug connected to said other portion, a sleeve for said plug with a closed end and an inwardly projecting shoulder near its open end for retaining said plug and having a :bored opening in its closed end'a pin member in said sleeve with its pin extending through said bored opening and resilient means between said pin member and said plug, said cylinder having an internal circumferential groove with a square shoulder near its open end, said sleeve being slidable in said cylinder and having resi'lently spreading prongs extending axially from its open end with square shoulders fitting against the square shoulder in said circumferential groove when said sleeve is pressed into said cylinder until said pin abuts the closed end of said cylinder and said resilient means is slightly compressed.
- a releasable coupling connecting two portions of an automatically breakable line comprising a cylinder having a closed end connected to one ,of said portions, a plug connected to said other portion, a sleeve for said plunger with a closed end and an inwardly projecting shoulder near its open end for retaining said plug and having a bored opening in said closed end, a pin member in said sleeve with its pin extending through said bored opening, resilient means between said plug and said pin member, said cylindelhaving an internal circumferential groove with a square shoulder near its open end, said sleeve being slidable in said cylinder and having resiliently spreading prongs extending axially from its open end with square shoulders tting against the square shoulder in said sleeve groove when the sleeve is pressed into said cylinder until said pin abuts Athe closed end of said cylinder and lsaid resilient means is slightly compressed, said prongs having projections converg- :ing axially
- a releasable coupling connecting two vportions of an automatically breakable line comprising a cylinder having a closed 'end connected to one of said portions, a plug connected to said other portion, a sleeve for said plug with a closed end and an inwardly projecting shoulder near its open end for retaining said plug and having a bored opening Vin said vclosed end, a pin member with its pin extending through said Abored opening, resilient ,means between ⁇ said plug and pin member, said -cylinder having an internal .circumferential groove with a square shoulder rnear its Open end.
- said sleeve member being sldable in said Cylinder .and having resi-Henny spreading prongs extending ⁇ axially from its open end With square shoulders tting lagainst the square shoulder in said circumferential groove when the sleeve member is pressed into said ⁇ cylinder until said in abuts vthe closed end of said cylinder ⁇ and lsaid resilient means is slightly compressedsaid prongs having projections converging axially, a collar around said projections ,adapted for withdrawing the prong shoulders out of jsaid groove when the collar is pushed back over ⁇ said converging projections, retaining means on the end of said projections for said collar, and resi-lient buffer means around the plug portion of the line for pushing said collar back over said converging projections as the line is pulled through said buffer means.
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- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Buckles (AREA)
Description
Dec. '16, 1947. R. B. COTTON GLIDER PICK-UP DEVICE original Filed oct. 28, 1945' FIG 2 Patented Dec. 16, 1947 UNITED STATES PATENT OFFICE Divided and this application October 21, 1944, Serial No. 559,720
(Granted under the act of March 3, 1883, as amended April 30, 1928; 370 0. G. 757) Claims.
The invention herein disclosed relates to glider pick-up apparatus of the type in which the glider which is at rest to begin with, is given a steady acceleration by energy obtained from a plane in flight until it reaches the speed of the plane, at which time a towline which has been picked up by the plane and which is connected to the apparatus, is released therefrom, and is gripped by a device on the glider for the subsequent towing of the glider by the plane.
The present application is a division of application Serial No. 507,931, led October 28, 1943, and is for the release means referred to above.
In the apparatus, which is the subject of the parent application, the energy necessary for accelerating the glider with a steady and reasonable acceleration is transferred from the plane in flight until the Yglider attains the speed of the plane, and then the towline is fixed for the subsequent towing of the glider by the plane. This is accomplished without the necessity of carrying any of the apparatus in the glider or the plane, except for a very light pulley on the glider comprising a part oi the gripping means and a light pick-up hook on the plane.
A hydraulic mechanism is used in the operation of this apparatus against a pressure accumulator to provide a continuous. steady pull on one end of the towline which is passed around the pulley at the nose of the glider while the other end of the towline is being pulled by the plane, thus storing a part of the energy during the rst part of the accelerating operation above referred to while the gliders Velocity is low, and returning it during-the latter part thereof, thereby continuously providing only half of the steady accelerating force to the glider, the other half being in the meantime supplied to the glider directly from the plane through the other portion of the towline passed around the pulley.
The apparatus thus includes a take-up line connested between the hydraulic means ard the towline which is passed around the pulley on the glider.
The object of the present invention is to provide means to release the towline from the take-up line when the glider reaches the speed ci the plane.
A further object is to provide a coupling between the towline and the take-up line which will break the connection upon impact or pressure of the coupling against a buffer sleeve through which the take-up line is passed.
These and other more specific objects will become apparent as the details of the subject releasable coupling means are described, having reierence to the accompanying drawings, wherein: Fig. 1 is a perspective view of the deck sheave post and buffer assembly used in the above referred to apparatus,
Fig. 2 is a cross-sectional view of the buier and the releasable coupling between the towline and take-up line prior to release.
Fig. 3 is the same view with the parts in position immediately after release, the broken line iigure showing the towline end fitting broken away from the rest of the coupling an instant later,
Fig. 4 is a cross-section taken at 4--4 of Fig. 2.
Referring more specically to the several figures wherein the corresponding parts are designated by like numerals, the buffer sleeve 34 has an inner shoulder 43 against which the slidable collar member 36 is normally resiliently held by spring 3l, the other end of which is biased against the iixed collar member 44. Take-up line 33 passes through this buffer and is attached to the coupling plug 45 fitted against an inner shoulder in sleeve 38 and supporting one end of spring il therein, the other end of which biases a pin member le which extends through a collar fixed in the end of the sleeve 38. The other end of sleeve 38 has a series of resilient prongs 39 extending therefrom around its periphery. These prongs have a collar 4l) mounted around their wedge formed ends so that when the collar is pushed over the wedged portions it brings the prongs radially toward the axis of the coupling. A peripheral shoulder formed by projections on the prongs is thereby moved radially within the cir` cumference of the sleeve. while normally it has a greater diameter and is adaptable to hook over an internal shoulder 6l formed in a groove on the inside of the cylinder 35 comprising the other part of the coupling which is attachedat 5i) tothe towline 3. The closed end of this cylinder forces the pin member 48 in against the pressure of spring il when the coupling is locked. When the coupling is pulled in against the buffer collar 36 by movement of the take-up line 33, the collar 36 strikes the collar 40 which normally rests `against the shoulder formed at the nose 4| of the prong assembly. Movement of the prong ends into the hollow of the sleeve 34 and collar 3G where they are further wedged by the conical shape of the hollow in this collar, moves the collar il over the wedge portions of the prongs to draw the shoulder formed by the prongs inwardly out of the groove 6l, and the pin member i8 assists in releasing the outer sleeve so as to break the connection and separate the coupling.
Although a specific application of the releasable coupling is shown in this disclosure, it is obvious that the device is applicable to other uses'wherever an automatic break in a lmoving line is desired upon it reaching a predetermined axial position in its movement.
Likewise, various modications in design in the several parts of the coupling and buffer sleeve may be made witho-ut departing from the spirit and scope of this invention, as dened in the appended claims. Y
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
What is claimed is:
1. A coupling co-nnecting two lines, a buer through which one of the lines passes comprising a collar resiliently held against axial displacement, and means on said coupling Vto release it when the line is moved through the buier so as to cause the coupling to strike said collar .in an axial direction ltending to displace it, including slidable means on said coupling, and resilient ejecting means for separating said coupling upon its release.
2. A releasable two-part coupling having each part connected to one portion of an automatically `breakable line, -a buffer element having a resiliently urged member, one portion of the line passing through said member, a releasing means on the part of the coupling nearest the buffer, so that as the line moves through the buifer the releasing means strikes the resiliently urged member in the buier and the reaction releases the two parts of the coupling, and resilient means in one of said coupling parts for urging them apart.
3. A releasa'ble coupling connecting two portions ,of an automatically breakable line, comprising a cylinder having a elo-sed end connected to one of said portions, a coupling plug connected to said other portion, a sleeve for said plug with a closed end and an inwardly projecting shoulder near its open end for retaining said plug and having a :bored opening in its closed end'a pin member in said sleeve with its pin extending through said bored opening and resilient means between said pin member and said plug, said cylinder having an internal circumferential groove with a square shoulder near its open end, said sleeve being slidable in said cylinder and having resi'lently spreading prongs extending axially from its open end with square shoulders fitting against the square shoulder in said circumferential groove when said sleeve is pressed into said cylinder until said pin abuts the closed end of said cylinder and said resilient means is slightly compressed.
4. A releasable coupling connecting two portions of an automatically breakable line, comprising a cylinder having a closed end connected to one ,of said portions, a plug connected to said other portion, a sleeve for said plunger with a closed end and an inwardly projecting shoulder near its open end for retaining said plug and having a bored opening in said closed end, a pin member in said sleeve with its pin extending through said bored opening, resilient means between said plug and said pin member, said cylindelhaving an internal circumferential groove with a square shoulder near its open end, said sleeve being slidable in said cylinder and having resiliently spreading prongs extending axially from its open end with square shoulders tting against the square shoulder in said sleeve groove when the sleeve is pressed into said cylinder until said pin abuts Athe closed end of said cylinder and lsaid resilient means is slightly compressed, said prongs having projections converg- :ing axially, a collar around said projections adapted for withdrawing the prong shoulders out of said groove when the collar is pushed back over said converging projections, and retaining means on the end of said projections for said collar.
v5. A releasable coupling connecting two vportions of an automatically breakable line, comprising a cylinder having a closed 'end connected to one of said portions, a plug connected to said other portion, a sleeve for said plug with a closed end and an inwardly projecting shoulder near its open end for retaining said plug and having a bored opening Vin said vclosed end, a pin member with its pin extending through said Abored opening, resilient ,means between `said plug and pin member, said -cylinder having an internal .circumferential groove with a square shoulder rnear its Open end. said sleeve member being sldable in said Cylinder .and having resi-Henny spreading prongs extending `axially from its open end With square shoulders tting lagainst the square shoulder in said circumferential groove when the sleeve member is pressed into said `cylinder until said in abuts vthe closed end of said cylinder `and lsaid resilient means is slightly compressedsaid prongs having projections converging axially, a collar around said projections ,adapted for withdrawing the prong shoulders out of jsaid groove when the collar is pushed back over `said converging projections, retaining means on the end of said projections for said collar, and resi-lient buffer means around the plug portion of the line for pushing said collar back over said converging projections as the line is pulled through said buffer means.
ROBERT B. COTTON.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES IPATENTS Number Name Date 1,091,449 Westin V Mar 24, 1914 1,677,009 Wiltsie July 10, 1928 1,719,144 Stokes et al. July 2, 1929 2,111,303 Switlik 1 Mar. 15, 1938 2,350,999 Beirise June 13, 1944
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US559720A US2432509A (en) | 1943-10-28 | 1944-10-21 | Glider pickup device |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US507931A US2432508A (en) | 1943-10-28 | 1943-10-28 | Glider pickup device |
| US559720A US2432509A (en) | 1943-10-28 | 1944-10-21 | Glider pickup device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2432509A true US2432509A (en) | 1947-12-16 |
Family
ID=27056032
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US559720A Expired - Lifetime US2432509A (en) | 1943-10-28 | 1944-10-21 | Glider pickup device |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2432509A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3094345A (en) * | 1962-02-08 | 1963-06-18 | Koch & Sons Inc H | Separable line coupling |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1091449A (en) * | 1912-10-01 | 1914-03-24 | Louis Arthur Westin | Overload uncoupling coupling. |
| US1677009A (en) * | 1927-07-11 | 1928-07-10 | Wiltsie Oliver Ernest | Adjustable releasing device |
| US1719144A (en) * | 1928-04-30 | 1929-07-02 | Reed Roller Bit Co | Overshot |
| US2111303A (en) * | 1935-01-17 | 1938-03-15 | James Hale Strong | Parachute device |
| US2350999A (en) * | 1942-10-27 | 1944-06-13 | John C Beirise | Airplane towing means |
-
1944
- 1944-10-21 US US559720A patent/US2432509A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1091449A (en) * | 1912-10-01 | 1914-03-24 | Louis Arthur Westin | Overload uncoupling coupling. |
| US1677009A (en) * | 1927-07-11 | 1928-07-10 | Wiltsie Oliver Ernest | Adjustable releasing device |
| US1719144A (en) * | 1928-04-30 | 1929-07-02 | Reed Roller Bit Co | Overshot |
| US2111303A (en) * | 1935-01-17 | 1938-03-15 | James Hale Strong | Parachute device |
| US2350999A (en) * | 1942-10-27 | 1944-06-13 | John C Beirise | Airplane towing means |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3094345A (en) * | 1962-02-08 | 1963-06-18 | Koch & Sons Inc H | Separable line coupling |
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