US1026415A - Automatic steering device for flying machines. - Google Patents
Automatic steering device for flying machines. Download PDFInfo
- Publication number
- US1026415A US1026415A US00000000A US1026415DA US1026415A US 1026415 A US1026415 A US 1026415A US 00000000 A US00000000 A US 00000000A US 1026415D A US1026415D A US 1026415DA US 1026415 A US1026415 A US 1026415A
- Authority
- US
- United States
- Prior art keywords
- steering device
- automatic steering
- flying machines
- mixture
- priming
- 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
- 239000000203 mixture Substances 0.000 description 15
- 230000037452 priming Effects 0.000 description 7
- 239000000843 powder Substances 0.000 description 6
- USXDFAGDIOXNML-UHFFFAOYSA-N Fulminate Chemical compound [O-][N+]#[C-] USXDFAGDIOXNML-UHFFFAOYSA-N 0.000 description 5
- 239000004615 ingredient Substances 0.000 description 4
- 239000007800 oxidant agent Substances 0.000 description 2
- VKJKEPKFPUWCAS-UHFFFAOYSA-M potassium chlorate Chemical compound [K+].[O-]Cl(=O)=O VKJKEPKFPUWCAS-UHFFFAOYSA-M 0.000 description 2
- WLWIMKWZMGJRBS-UHFFFAOYSA-N primin Chemical compound CCCCCC1=CC(=O)C=C(OC)C1=O WLWIMKWZMGJRBS-UHFFFAOYSA-N 0.000 description 2
- YPMOSINXXHVZIL-UHFFFAOYSA-N sulfanylideneantimony Chemical compound [Sb]=S YPMOSINXXHVZIL-UHFFFAOYSA-N 0.000 description 2
- BZWKPZBXAMTXNQ-UHFFFAOYSA-N sulfurocyanidic acid Chemical compound OS(=O)(=O)C#N BZWKPZBXAMTXNQ-UHFFFAOYSA-N 0.000 description 2
- 229910001369 Brass Inorganic materials 0.000 description 1
- 241000218652 Larix Species 0.000 description 1
- 235000005590 Larix decidua Nutrition 0.000 description 1
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 1
- ZJRXSAYFZMGQFP-UHFFFAOYSA-N barium peroxide Chemical compound [Ba+2].[O-][O-] ZJRXSAYFZMGQFP-UHFFFAOYSA-N 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- 238000013329 compounding Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 1
- 229910052753 mercury Inorganic materials 0.000 description 1
- MHWLNQBTOIYJJP-UHFFFAOYSA-N mercury difulminate Chemical compound [O-][N+]#C[Hg]C#[N+][O-] MHWLNQBTOIYJJP-UHFFFAOYSA-N 0.000 description 1
- 229910052700 potassium Inorganic materials 0.000 description 1
- 239000011591 potassium Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/02—Control of position or course in two dimensions
- G05D1/0206—Control of position or course in two dimensions specially adapted to water vehicles
Definitions
- ViLLiAM H. BUELL a citizen of the United States, residing at New Haven, in the county of New Haven and State of Connecticut, have invented a new and useful Improvement in Priming Mixtures; and I do hereby declare the following to be a full, clear, and exact description of the same.
- Hy invention relates'to an improvement in that class of priming mixtures whichare known as non-fulminate or non-mercuri mixtures for the reason that they are compounded withoutthe use of fulminate of mercury which is the characteristic ingredient of all fulminate mixtures, the object of my present invention being to pro prise a non-fulminate mixture of superior character in so far as it insures the rapid and even ignition of the entire priming mass and the production of a hot and uniform tiame for the immediate and uniform ignition of the powder so that the same will be entirely ignited and consumed at the breechend of the barrel rather than progressively throughout the barrel as is often the case.
- my invention consists in a non-fulminate mixture composed and compounded as hereinafter described.
- the compounding of the above ingredicuts produce a fine. grayish-brown powder which by preference is intrmlured dry into the primer cups in which it scaled by heavy pressure which results in the reduction of the powder into the form of a thin hard cake in the bottom of the cup.
- This calre is preferably sealed in place by the application to it of a thin film of collodion which extends over it and up into the side walls of the cup, enough of the collodion entering the cake to bind it thereto.
- An anvil of any approved construction is then introduced into the primer-cup in the ordinary manner as indicated in my prior Patent No. 962,888 of June 28, 1910.
- my improved primer mixture in rim-fire ammunition, it is preferably wet with a suitable moistening fluid and driven by centrifugal force into the outwardly projecting annular hollow rim of the cartridgeshell.
- a suitable moistening fluid By preference it is then, covered with collodion applied so as to cover it and extend up upon the side walls of the shell as shown in my prior Patent No.
- My improved non-fulminatepriming mixture is so homogeneous in its character and so easy of ignition that the whole mass ignites practically at the same time and produces a hot and uniform flame leaving the minimum of residue.
- the flame produced by it penetrates the powder and so diffuses itself therein that; the whole mass or body thereof is simultaneously ignited and burned at the breech end of the gun whereby the effect of'thc slow or progressive burningof the powder upon the barrel and upon the accuracy and eliicicncy of the aminunition is avoided.
- My improved nonfulminate priming mixture to amalgamate' with the brass of primers and cartridge shells, and therefore avoids the very serious objection attached to the use of all priming mixtures containing mercury in any form.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Curing Cements, Concrete, And Artificial Stone (AREA)
Description
R. M. THOMPSON.
AUTOMATIC STEERING DEVICE FOR FLYING MACHINES.
APPLIGATION FILED JUNE 29, 1910.
Patented'May 14, 1912.
l7 I I i PI I I I I IL I/V VE [1170B id/ef/ 75.40
WITNESSES:
X). Z) a.
ATTORNEY itildi'iiiilE TATE PATENT WILLIAM H. IBUELL, OF NEW HAVEN, CONNECTICUT, ASSIGNOR TO WINCHESTER REPEATING ARMS 00., OF NEW HAVEN, CONNECTICUT, A CORPORATION.
PRIMIN Gr MIXTURE.
No Drawing.
Specification of Letters Patent.
Patented May 28,1912.
Application filed It'larch 14, 1912. Serial No. 683,877.
To all whom it may concern Be it known that I, \ViLLiAM H. BUELL, a citizen of the United States, residing at New Haven, in the county of New Haven and State of Connecticut, have invented a new and useful Improvement in Priming Mixtures; and I do hereby declare the following to be a full, clear, and exact description of the same. V
Hy invention relates'to an improvement in that class of priming mixtures whichare known as non-fulminate or non-mercuri mixtures for the reason that they are compounded withoutthe use of fulminate of mercury which is the characteristic ingredient of all fulminate mixtures, the object of my present invention being to pro duce a non-fulminate mixture of superior character in so far as it insures the rapid and even ignition of the entire priming mass and the production of a hot and uniform tiame for the immediate and uniform ignition of the powder so that the same will be entirely ignited and consumed at the breechend of the barrel rather than progressively throughout the barrel as is often the case.
iYith these ends in view my invention consists in a non-fulminate mixture composed and compounded as hereinafter described.
In carrying out my invention, I mix together about 20% of antimony sulfid. 25% of lead sulfocyanid, of potassium chlorate, and 5%- of trinitrololuol. These several ingredients are preferably employed in substantially the proportions indicated, but the proportions may be varied as may be found necessary to secure the best results, and to take into account the ordinary trade. variations in the strength of the ingredients.
Furthermore variations in thelrlmracter of the powders with which my improved priming mixture is employed may require some corresponding adjustment of the mixture in order to secure the best results. I, do not, therefore, limit myself to the exact proport ons given for the 01 oral ingredients.
The compounding of the above ingredicuts produce a fine. grayish-brown powder which by preference is intrmlured dry into the primer cups in which it scaled by heavy pressure which results in the reduction of the powder into the form of a thin hard cake in the bottom of the cup. This calre is preferably sealed in place by the application to it of a thin film of collodion which extends over it and up into the side walls of the cup, enough of the collodion entering the cake to bind it thereto. An anvil of any approved construction is then introduced into the primer-cup in the ordinary manner as indicated in my prior Patent No. 962,888 of June 28, 1910.
In the use of my improved primer mixture in rim-fire ammunition, it is preferably wet with a suitable moistening fluid and driven by centrifugal force into the outwardly projecting annular hollow rim of the cartridgeshell. By preference it is then, covered with collodion applied so as to cover it and extend up upon the side walls of the shell as shown in my prior Patent No.
966.163 of August 2, 1910.
My improved non-fulminatepriming mixture is so homogeneous in its character and so easy of ignition that the whole mass ignites practically at the same time and produces a hot and uniform flame leaving the minimum of residue. The flame produced by it penetrates the powder and so diffuses itself therein that; the whole mass or body thereof is simultaneously ignited and burned at the breech end of the gun whereby the effect of'thc slow or progressive burningof the powder upon the barrel and upon the accuracy and eliicicncy of the aminunition is avoided. My improved nonfulminate priming mixture to amalgamate' with the brass of primers and cartridge shells, and therefore avoids the very serious objection attached to the use of all priming mixtures containing mercury in any form.
I do not limit myself, as already stated. to
the exact proportions herein given, and turper.
moreover. contains nothing a 1 2mm In testimony whereof, I have signed this specification in the presence of two subscrlbmg witnesses.
' W'ILLIAM H. BUELL.
potassium chlorate solely as an oxidizing agent, I may employ other oxidizing agents such as barium peroxid. I
5 A non-fulminate priming mixture 0e1n J posed of antimony sulfid, lead sulfocyanid, I potassium chlorateand trinitroteluol.
Vitnesses GLARA VEED, GEORGE D. SEYMOUR.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1026415TA |
Publications (1)
Publication Number | Publication Date |
---|---|
US1026415A true US1026415A (en) | 1912-05-14 |
Family
ID=3094710
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00000000A Expired - Lifetime US1026415A (en) | Automatic steering device for flying machines. |
Country Status (1)
Country | Link |
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US (1) | US1026415A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504139A (en) * | 1945-06-30 | 1950-04-18 | Jarly C Malen | Automatic pilot |
-
0
- US US00000000A patent/US1026415A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504139A (en) * | 1945-06-30 | 1950-04-18 | Jarly C Malen | Automatic pilot |
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