US1860327A - Aeroplane float signal - Google Patents
Aeroplane float signal Download PDFInfo
- Publication number
- US1860327A US1860327A US570181A US57018131A US1860327A US 1860327 A US1860327 A US 1860327A US 570181 A US570181 A US 570181A US 57018131 A US57018131 A US 57018131A US 1860327 A US1860327 A US 1860327A
- Authority
- US
- United States
- Prior art keywords
- door
- cylinder
- bolt
- casing
- spring
- 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 - Lifetime
Links
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 12
- 238000010276 construction Methods 0.000 description 2
- 229920000136 polysorbate Polymers 0.000 description 1
- 108010085990 projectin Proteins 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
Definitions
- This invention relates to a floating signal for aeroplanes and the like, the general object of the invention being to provide means for indicating the spot in where an aeroplane or the like has sunk. with means for normally holding the signal in a compartment formed in a part of the fuselage and means for automatically releasing the spring door of the compartment when the plane drops into a body of water so that the signal will float from the compartment and rise to the surface.
- Figure 1 is a view showing the signal in use marking the spot where an aeroplane has sunk into abody of water.
- Fig. 2 is a sectional view through part of the fuselage of the 'plane showing the parts of the invention therein.
- Fig. 3 is a section on line 33 of Fig. 2.
- Fig. 4 is a vertical sectional view thru Fig. 5 is a vertical sectional view thru the lock cylinder.
- Fig. 6 is a view of the cap for said cylinder.
- Fig. 7 is a view of a roll of blotting paper for normally holding the spring bolt in projected position.
- the numeral 1 indicates a casing which forms a small compartmentin the fuselage of the plane and which is "located on one side thereof, and the fuselage is formed with an opening 2 which communimates with the compartment, and this opening is closed by a door which is provided with the spring hinge 4, the spring of which normally holds the door in open position.
- a cylinder 5 is suitably supported in the fuselage adjacent the casing 1, and a bolt 6 is located in the cylinder with a part projecta body of water I ing therefrom to engage the keeper 7 of the door to normally hold the door in closed position.
- the inner end of the bolt is provided with a head 8, and a spring 9 is placed between the head and the lower end of the cylinder and tendsto hold the bolt in retracted position so that the door can he opened by the spring hinge.
- a roll 10 of blotting paper normally holds the bolt projected tween the head 8 and a perforated cap 11, which is detachably connected to the upper end of the cylinder by the screws 12.
- the blotting paper is rolled with the grain and glued together with sealing paper.
- a ring-shaped float or buoy 13 is placed in the chamber formed by the casing 1 and a staff 14 is pivotally arranged in the buoy as shown at 15 and has a weight 16 on its lower end and a flag 17 on its other end, the weight tending to hold the staff in upright position when the float or buoy is floating on the sun; face of the water as shown in Fig. 1. e
- a cable 18 is connected to the float and passes through a hole 19 in the inner Wall of the casing 1, and then passes downwardly and is wound upon a spool, (not shown) located in a housing 20 fastened to an internal wall of the fuselage, and formed with aslot 21 through which the cable passes.
- Means for marking the position of a sunken craft in a body of water comprising body of the craft and thereof, a door for for holding the door in open position, a cylinder arranged adjacent the casing, a bolt passing through one end of the cylinder and engaging a keeper member on the door for holding the door in closed position, a perforated cap closing the other end of the cylinder, a head the spot where a of water comprisbody of the craft and one end of the opening through one wall on the inner end of the bolt a ,wall thereof, a door position, a
- a spring located between the head and the lower end of the cylinder for holding the bolt retract-ed
- a roll of blotting paper located in the cylinder between the head and the erforated cap for holding the bolt projecte a buoy in the casing, a cable connecting the buoy with a part of the body of the craft, and a pivoted and weighted uoy.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Paper (AREA)
Description
P. A. KUHN AEROPLANE FLOAT SIGNAL Filed Oct. 21,1931 2 Sheets-Sheet 1 Inventor May 1932- P. A. KUHN A'EROPLANE FLOAT SIGNAL Filed Oct. 21, 1951 2 Sheets-Sheet 2 Inventor flitorney W (a o W4 6 o o o F 0 ZW M m vp P m Patented May 24. 1932 UNITED STATES PHILLIP A. KUHN, OF GALVESTON, TEXAS AEROPLANE FLOAT SIGNAL Application filed October 21, 1931. Serial No. 570,181.
This invention relates to a floating signal for aeroplanes and the like, the general object of the invention being to provide means for indicating the spot in where an aeroplane or the like has sunk. with means for normally holding the signal in a compartment formed in a part of the fuselage and means for automatically releasing the spring door of the compartment when the plane drops into a body of water so that the signal will float from the compartment and rise to the surface. I
This invention also consists in certain other features of construction and in the combination and arrangement of the several parts to be hereinafter fully described, illustrated in the accompanying drawings and specifically pointed out in the appended claims.
In describing the invention in detail, reference will be had to the accompanying drawings wherein like characters denote like or corresponding parts throughout the several views, and in which Figure 1 is a view showing the signal in use marking the spot where an aeroplane has sunk into abody of water.
Fig. 2 is a sectional view through part of the fuselage of the 'plane showing the parts of the invention therein.
Fig. 3 is a section on line 33 of Fig. 2.
Fig. 4 is a vertical sectional view thru Fig. 5 is a vertical sectional view thru the lock cylinder.
Fig. 6 is a view of the cap for said cylinder.
Fig. 7 is a view of a roll of blotting paper for normally holding the spring bolt in projected position.
In these drawings, the numeral 1 indicates a casing which forms a small compartmentin the fuselage of the plane and which is "located on one side thereof, and the fuselage is formed with an opening 2 which communimates with the compartment, and this opening is closed by a door which is provided with the spring hinge 4, the spring of which normally holds the door in open position.
A cylinder 5 is suitably supported in the fuselage adjacent the casing 1, and a bolt 6 is located in the cylinder with a part projecta body of water I ing therefrom to engage the keeper 7 of the door to normally hold the door in closed position. The inner end of the bolt is provided with a head 8, and a spring 9 is placed between the head and the lower end of the cylinder and tendsto hold the bolt in retracted position so that the door can he opened by the spring hinge.
A roll 10 of blotting paper normally holds the bolt projected tween the head 8 and a perforated cap 11, which is detachably connected to the upper end of the cylinder by the screws 12. The blotting paper is rolled with the grain and glued together with sealing paper.
Thus, as water enters the fuselage, some of this water will pass through the perforations in the top 11 and enter the cylinder 5 so as to moisten the blotting paper which will then collapse under the pressure of the spring 9, so that the spring will retract the bolt 6 and the door will swing open under the action of its springhinge.
A ring-shaped float or buoy 13 is placed in the chamber formed by the casing 1 and a staff 14 is pivotally arranged in the buoy as shown at 15 and has a weight 16 on its lower end and a flag 17 on its other end, the weight tending to hold the staff in upright position when the float or buoy is floating on the sun; face of the water as shown in Fig. 1. e
A cable 18 is connected to the float and passes through a hole 19 in the inner Wall of the casing 1, and then passes downwardly and is wound upon a spool, (not shown) located in a housing 20 fastened to an internal wall of the fuselage, and formed with aslot 21 through which the cable passes.
From the foregoing it will be seen that if the aeroplane should fall into a body of 99 Water, the water entering the fuselage would find its way into the cylinder 5 through the perforations in the can 11. so that the cartridge or roll 10 of blotting paper, would become mo st. and thus collapse under the pressure of the spring 9, so that the spring would retract the bolt 6' and release the door, and then the spring hinge of the door will swing the same to open position.
The flow of water into the casing 1 would 100 as said roll is placed be- 60' ing the cable 18 the buoy out 'of the casing,
surface, pullin the casin of course float and the buoy would rise to the from the spool 20 and the weight 16 will cause the flag sta to assume a vertical position as shown in Fig. 1, so as to mark the spot where the sunken lane rests.
It is thought from'the foregoing description that the advantages and novel features of the invention will be readily apparent.
It is to be understood that changes may be made in the construction and in the combination and arrangement of the several parts, provided that such changes fall within the scope of the appended claims.
Having thus described my'invention, what I claim as new is I member on the door a casing located in the closing the casing, a spring 1. Means for marking the spot where a craft has sunk in a body of a casing attached to the craft, a door for normally closing the casing, spring means for normally holding the door in open position, a bolt for holding the door in closed position, a cylinder in which the bolt is located with the bolt projectin .inder, member formed in the cylinder for normally holding the bolt projected, said cylinder having perforations therein fortheadmission of water to the member, a buoy located in the casing and a flexible memberconnecting the buoy with the craft.
2. Means for marking craft'has sunk i to a body ing a casing carried by the and opening out thru for closing the casing, spring means for normally holding the door in open buoy in the casing, a casin within the craft and having a spool rotatab y arranged therein, a cable wound on the spool into the casing first mentioned and attached to the buoy, a cylinder located in the craft adjacent the door, a bolt passing through one end of the cylinder for engaging a keeper for holding the door in closed position, a head on the inner en of the bolt, a spring located between the head and a part of the cylinder for retracting the bolt, a roll of blotting paper inder between the head cylinder for-holding cylinder having perforations therein.
3. Means for marking the position of a sunken craft in a body of water comprising body of the craft and thereof, a door for for holding the door in open position, a cylinder arranged adjacent the casing, a bolt passing through one end of the cylinder and engaging a keeper member on the door for holding the door in closed position, a perforated cap closing the other end of the cylinder, a head the spot where a of water comprisbody of the craft and one end of the opening through one wall on the inner end of the bolt a ,wall thereof, a door position, a
located in the 03 1-.
a spring located between the head and the lower end of the cylinder for holding the bolt retract-ed, a roll of blotting paper located in the cylinder between the head and the erforated cap for holding the bolt projecte a buoy in the casing, a cable connecting the buoy with a part of the body of the craft, and a pivoted and weighted uoy. y
In testimony whereof I afiix my siganture.
. PHILLIP A. KUHN.
d of the cyl f the bolt, a
and passing I the bolt projected, said I flag carrying staff carried by the
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US570181A US1860327A (en) | 1931-10-21 | 1931-10-21 | Aeroplane float signal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US570181A US1860327A (en) | 1931-10-21 | 1931-10-21 | Aeroplane float signal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1860327A true US1860327A (en) | 1932-05-24 |
Family
ID=24278586
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US570181A Expired - Lifetime US1860327A (en) | 1931-10-21 | 1931-10-21 | Aeroplane float signal |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1860327A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2415863A (en) * | 1945-06-13 | 1947-02-18 | United Shoe Machinery Corp | Recovery buoy for hydrobombs |
| US2470783A (en) * | 1945-05-15 | 1949-05-24 | Vincent A Mead | Plane marker buoy |
| US2474537A (en) * | 1946-03-29 | 1949-06-28 | Sun Chemical Corp | Position indicator for aircraft |
| US2479021A (en) * | 1945-11-29 | 1949-08-16 | Frank G Fetzer | Retriever for submerged articles |
| US2505950A (en) * | 1947-08-05 | 1950-05-02 | Aerial Products Inc | Launching or discharging equipment for signaling |
| US2552969A (en) * | 1946-10-11 | 1951-05-15 | James P Holman | Telltale radio signal device |
| US2675568A (en) * | 1952-08-04 | 1954-04-20 | Edwin E King | Retriever for submerged articles |
| US3280789A (en) * | 1965-10-21 | 1966-10-25 | George D Lewis | Diver-down flag float |
| US3761978A (en) * | 1972-10-04 | 1973-10-02 | H Robinson | Water safety device for occupants of a submerged vehicle |
| US4619066A (en) * | 1984-09-19 | 1986-10-28 | Kirkland Donald R | Float release devices |
-
1931
- 1931-10-21 US US570181A patent/US1860327A/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2470783A (en) * | 1945-05-15 | 1949-05-24 | Vincent A Mead | Plane marker buoy |
| US2415863A (en) * | 1945-06-13 | 1947-02-18 | United Shoe Machinery Corp | Recovery buoy for hydrobombs |
| US2479021A (en) * | 1945-11-29 | 1949-08-16 | Frank G Fetzer | Retriever for submerged articles |
| US2474537A (en) * | 1946-03-29 | 1949-06-28 | Sun Chemical Corp | Position indicator for aircraft |
| US2552969A (en) * | 1946-10-11 | 1951-05-15 | James P Holman | Telltale radio signal device |
| US2505950A (en) * | 1947-08-05 | 1950-05-02 | Aerial Products Inc | Launching or discharging equipment for signaling |
| US2675568A (en) * | 1952-08-04 | 1954-04-20 | Edwin E King | Retriever for submerged articles |
| US3280789A (en) * | 1965-10-21 | 1966-10-25 | George D Lewis | Diver-down flag float |
| US3761978A (en) * | 1972-10-04 | 1973-10-02 | H Robinson | Water safety device for occupants of a submerged vehicle |
| US4619066A (en) * | 1984-09-19 | 1986-10-28 | Kirkland Donald R | Float release devices |
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