US1115162A - Aeromobile. - Google Patents
Aeromobile. Download PDFInfo
- Publication number
- US1115162A US1115162A US44795108A US1908447951A US1115162A US 1115162 A US1115162 A US 1115162A US 44795108 A US44795108 A US 44795108A US 1908447951 A US1908447951 A US 1908447951A US 1115162 A US1115162 A US 1115162A
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- US
- United States
- Prior art keywords
- blade
- blades
- arms
- secured
- cross
- 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
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
Definitions
- aero-mobiles or helico sters in ⁇ which rotary horizontal blades are employed, arranged at such an angle that they exert a lifting action upon the machine.
- the principal object of theinvention is to provide an improved blade or propeller structure, which is so shaped and braced as not only to preventbreakage or distortion when subjected to abnormal strain, but to hold each blade at all times in proper relative position to the other, and in proper relation to every other part of its own surface.
- Figure 1 is a side elevation of an aeromobile propeller, constructed in accordance with my invention.
- Fig. 2 is a trans-verse sectional view ofthe same on ⁇ line 2-2 of Fig. 1, the vertical shaft and cross arms being shown in elevation;
- Fig. 3 is a detail perspective view of a portion of the blade structure, showing the arrangement of one of the braces;
- Fig. 4 is a detail section through one of the brace-connecting arms;
- Fig. 5 is a detail perspective view, showing one of the brace connections with the blade.
- the base or main frame of the apparatus is merely typical. It comprises a. pair of triangular end frames a, connected by tubes 7).
- the tubes which constitute the flooring and upper structure, are provided with bearings for the reception of a pair of vertically disposed parallel shafts o and Z, which are connected by gearing d.
- a motor On the sha-ft o is a motor, which may be driven by any suitable power, but is preferably a hydrocarbon motor.
- This motor as shown conventionally in Fig. 1 mounted'on the shaft c, is rotatable about a vertical axis and carries a small pinion meshing with the gear d.
- the vertical shaft 1 carries a sleeve or collar 2, secured in place by a key or the like. From this sleeve extend diametrically opposite socket members 2, in which are seated blade-carrying arms 4, which are preferably of rectangular form in ⁇ cross section and gradually taper from their inner to their outer ends. 4 i
- fan blades 5 which preferably are formed of sheet metal, said blades being inclined in opposite directions respectively, ⁇ and their active faces being slightly concaved by tension wires 6, which extend vacross the blade surfaces near the outer ends'thereof.
- the thin metallicblades have reinforcing strips 7 extending along each edge of their rear surfaces, and extending from side to side of 'the face of each blade are cross strips 8, these being bowed across the arms 4, and being permanently secured to the arms and blades 5 by suitable-rivets, as shown at 9.
- spacing blocks 10 Arranged between the cross strips 8 and the blade, are spacing blocks 10 which are located about midway between the arm 4 and the edges of the blade and secured by bolts or rivets 11.
- upper and lower arms 12 and 13 Secured to the vertical shaft are upper and lower arms 12 and 13, disposed parallel with each other and at right angles to the arms 4. These arms 12 and 13 are in the form of T bars in cross section, and are arranged to hold the ends of a number of brace rods or wires that extend from the fan blades.
- the primary brace rod 14 of the blades is in the form of a tension wire that passes through an opening 15 formed in the shaft 1.
- the ends of this wire pass to the ends of the arm 4 and extend through openings formed in small cross bars 16 that are secured to the extreme outer ends of the arms 4 and pass through openings in the blades (see Fig. 3).
- the ends of the rod are threaded and receive clamping nuts 17, by which it is properly tensioned and held in place.
- To the lower ends of the cross bars 16 are secured the outer ends of brace rods 18, that pass to the lower arm 13 and eX- tend through openings 19- forrned in said bar.
- These rods 18 incline forward in the direction of rotative movement of the blade to which they are attached ⁇ and greatly strengthen the blade.
- auxiliary bracing rods is also employed. rl'hese extend from the arrns 12, 13 to the blades, and at the latter pointiare :connected in the manner best shown in Fig. 5.
- Iauxiliary ⁇ braces arranged .in .pairs (eee 30e-31) run from the rear :and ⁇ lower edges of the blades Ato ⁇ the yarn'ls 12 and 13, andi are confined by nuts 32.
- a carrying g erm extending elena' the lenetudualeenvter ,of ,fthe blade and Tsecured 5to the rear face thereof, reinforcing battens secured te theI edge portions of the rear face of the blade, and cross strips .extending transversely of the blade V.and arched over'the carrying arin, vsaid strips being secured l(to 'the battei'is and :the anni; v
- a-rroneller having cured to the rear face of the blade ⁇ reinforc ing battens at the opposite edges of the blade, cross stri-ps arched across the arm,
- a shaft a cross thereon. blade carrying extending from said shaft, a blade ⁇ secured to each arm and provided with an opening -at the gouter of the arm, .a c ross .barertending through fthe opening and hayiing a central portion 4secured to the 'end of the erna e .Gross secured to 'fthe Shaft, e tension lmember connecting the upper arins of the blade cross bars and extending tation, wherebv said members may act as through an opening in the shaft, and tension draft devices for the blades.
- 10 members extending from the lower arms of In testimonv whereof I affix my signathe blade cross bars to the shaft cross arm, ture, in preseneee of two witnesses.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cleaning Implements For Floors, Carpets, Furniture, Walls, And The Like (AREA)
Description
E. BBRLNBB..
AEROMOBILE.
APPLICATION rILED AUG.11, 19108 Patented 0G13. 27, 1914.
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THE MORRIS PETERS Co., PH01oLlTHo., WASHINGTON. n, c
E1 BERLINER.
AEROMOBILE.
APPLICATION FILED AUG, 11, 190s.
Patented Oct. 27, 1914.
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WMe/awr') attenua;
1HE MORRIS PETERS C0..PH0TD-LITI1 L WASHING roN. D. C.
Fltllll@ EMILE ERLINER, 0F WASHINGTON, DISTRICT OF COLUMBIA.
AEROMOBILE.
Specification of' Letters Patent.
Application filed August 11, 1908.
Fatented Oct. 27, 1914.
Serial No. 447,951.
known as aero-mobiles or helico sters in` which rotary horizontal blades are employed, arranged at such an angle that they exert a lifting action upon the machine.
The principal object of theinvention is to provide an improved blade or propeller structure, which is so shaped and braced as not only to preventbreakage or distortion when subjected to abnormal strain, but to hold each blade at all times in proper relative position to the other, and in proper relation to every other part of its own surface.
With the foregoing and other objects in view, the invention consists in the novel construction and arrangements hereinafter described and referred to in the appended claims. i
The invention is illustrated in the accompanying drawings, in which,-
Figure 1 is a side elevation of an aeromobile propeller, constructed in accordance with my invention. Fig. 2 is a trans-verse sectional view ofthe same on `line 2-2 of Fig. 1, the vertical shaft and cross arms being shown in elevation; Fig. 3 is a detail perspective view of a portion of the blade structure, showing the arrangement of one of the braces; Fig. 4 is a detail section through one of the brace-connecting arms; and Fig. 5 is a detail perspective view, showing one of the brace connections with the blade.
The base or main frame of the apparatus, as shown in the drawing, is merely typical. It comprises a. pair of triangular end frames a, connected by tubes 7). The tubes which constitute the flooring and upper structure, are provided with bearings for the reception of a pair of vertically disposed parallel shafts o and Z, which are connected by gearing d. On the sha-ft o is a motor, which may be driven by any suitable power, but is preferably a hydrocarbon motor. This motor as shown conventionally in Fig. 1 mounted'on the shaft c, is rotatable about a vertical axis and carries a small pinion meshing with the gear d.
The vertical shaft 1 carries a sleeve or collar 2, secured in place by a key or the like. From this sleeve extend diametrically opposite socket members 2, in which are seated blade-carrying arms 4, which are preferably of rectangular form in `cross section and gradually taper from their inner to their outer ends. 4 i
On the arms are secured fan blades 5, which preferably are formed of sheet metal, said blades being inclined in opposite directions respectively, `and their active faces being slightly concaved by tension wires 6, which extend vacross the blade surfaces near the outer ends'thereof.
The thin metallicblades have reinforcing strips 7 extending along each edge of their rear surfaces, and extending from side to side of 'the face of each blade are cross strips 8, these being bowed across the arms 4, and being permanently secured to the arms and blades 5 by suitable-rivets, as shown at 9.
' Arranged between the cross strips 8 and the blade, are spacing blocks 10 which are located about midway between the arm 4 and the edges of the blade and secured by bolts or rivets 11.
Secured to the vertical shaft are upper and lower arms 12 and 13, disposed parallel with each other and at right angles to the arms 4. These arms 12 and 13 are in the form of T bars in cross section, and are arranged to hold the ends of a number of brace rods or wires that extend from the fan blades.
The primary brace rod 14 of the blades is in the form of a tension wire that passes through an opening 15 formed in the shaft 1. The ends of this wire pass to the ends of the arm 4 and extend through openings formed in small cross bars 16 that are secured to the extreme outer ends of the arms 4 and pass through openings in the blades (see Fig. 3). The ends of the rod are threaded and receive clamping nuts 17, by which it is properly tensioned and held in place. To the lower ends of the cross bars 16 are secured the outer ends of brace rods 18, that pass to the lower arm 13 and eX- tend through openings 19- forrned in said bar. These rods 18 incline forward in the direction of rotative movement of the blade to which they are attached `and greatly strengthen the blade.
of auxiliary bracing rods is also employed. rl'hese extend from the arrns 12, 13 to the blades, and at the latter pointiare :connected in the manner best shown in Fig. 5.
rlghrough the edge battens 7, the .blades 5,2 and cross strips .8, are drilled vholes for the; Vreception off pins 2d, These vpir-1s project `jbeyond the opposite faces `of the blades, and?y yhave lopenings ,for the passage of the braces, the latter being threaded and theld .in placey by .nuts '25. l
Probably the greatest .stra-in .fon each blade These brace's Vpass through openings 28 formed in .both the upper and :lower arinsl 1213` at the saine side as the forward edge of the blade, and are held in 4place by nuts- 29.` The Jbraces run vin pairs from the upper and vvlower Afaces ofthe blade, their tension .may nbe readily adjusted ,by `turning :the `nutslf? and 29. In addition yto these, four Iauxiliary `braces arranged .in .pairs (eee 30e-31) run from the rear :and `lower edges of the blades Ato `the yarn'ls 12 and 13, andi are confined by nuts 32.
a These serve to i Atraiisinit the strain vJQQBOL bllrd@ et@ iblad, and
make :the whole fabric :taut and .properly braced and 'tensioned for moving at lhigh speed. Lt will be seen that by arranging the moving .-partsof the motor -to rotate horizontally, thatsaid l motor will ac t as a gyroseope to steady .the vessel while the same is in motion.
Having thus particularly Adescribed my invention, what l claim as. new desir-e yto secure by Letters Batent 1. In a .flyinginachind'a propel-ler having blades each farmed of sheet inaterial :and @ensei/ed transversely. e serrertns annex- .tending longitudinally ,of the blade, and secured to the central `,pmt-iran of its rear face, and -a plurality .of arched cross strips secured to the edge portions of the b ,lade and ,ieXtendigng over `and vsecured ,to Asaid arm. 2. In a dying meChi-ne1 :a @reseller baring blades formed of Sheet material. a carrying g erm extending elena' the lenetudualeenvter ,of ,fthe blade and Tsecured 5to the rear face thereof, reinforcing battens secured te theI edge portions of the rear face of the blade, and cross strips .extending transversely of the blade V.and arched over'the carrying arin, vsaid strips being secured l(to 'the battei'is and :the anni; v
3. In a flying machine, a-rroneller having cured to the rear face of the blade` reinforc ing battens at the opposite edges of the blade, cross stri-ps arched across the arm,
i Yand secured to the battens and the arm, and ln addition to the central braces, a series Sewing :t0 ereh the lei-eide transversely, e e
carryingfarrn secured ,to-,the rear face of the 3 blade, and rigid `ler-acing Lmembers extendy ing across andsecu-red to the y-arin and .to the is at its upper edge, and from this point eX- g -tend four tensi'on'braces or wires 26 Aand 27 f connected as beforedeseribed by the pins 25.
melfenal versions of the blade. A
5. In a machine of the class described,ga revoluble shaft, blade .carrying arins extending therefrom, `tralisversely concaved blades secured to fsaid arn1s ,cnossarnis carried by ,the shaft .at .points abeye and below the blade .ar-Ins, lsaid cross .arms ,being disposed 1 at an angle with respect to fthe lengthof the blade aryms,te,nsion rnenibersextending from 'the cross arms to the forward edges of the blades, .and auxiliary members extending `from said bars `'to the rear ,edges .of `the ,Inat- ,ing :blade :to permit distribution of the strain from blade to blade.
6. In a machine of vthe class described, ,a revoluble shaft with .arms proiecting there.- .fro1 n, blades carried lby Isaid arins, and a ,tension Ain ein'gber extending .continuously longitudinally c f said .blades tand `connected at its opposite ends at or -near the outer ends of said blades.
7. Ina machine of the iclass described', a shaft, arms extending -thereirolm blades secured -to said arrns and each proyided with an opening at the Vouter end of vthe arm,
and .hayingtheir ,central poltionsse'cured 1to f .the ,ends of the arms, cross arms-secured to the shaft. tension members lconnecting the upper ends of ,the blades to the cross arms, and -tenserl members extending from the lower arins of Vthe b lade cross bars vto the shaft @rees fari/111s, :the attaching point with .the latter arms being in advance of the face fof-f the blade, wherebygseel members may act as draft devices for the blades.
8. In y a machine of the class described, a shaft, a cross thereon. blade carrying extending from said shaft, a blade `secured to each arm and provided with an opening -at the gouter of the arm, .a c ross .barertending through fthe opening and hayiing a central portion 4secured to the 'end of the erna e .Gross secured to 'fthe Shaft, e tension lmember connecting the upper arins of the blade cross bars and extending tation, wherebv said members may act as through an opening in the shaft, and tension draft devices for the blades. 10 members extending from the lower arms of In testimonv whereof I affix my signathe blade cross bars to the shaft cross arm, ture, in preseneee of two witnesses.
the direction of said tension members eon- EMILE BERLINER. neoting the lower arms of the blade cross Witnesses:
bars with said shaft cross arm being or- A. M. PARKINS.
wardly with respect to the direction of ro- C. S. STURTEVANT.
Copies of this patent may be obtained for ve cents each, by addressing the Commissioner of Patents,
Washington, D. C.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US44795108A US1115162A (en) | 1908-08-11 | 1908-08-11 | Aeromobile. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US44795108A US1115162A (en) | 1908-08-11 | 1908-08-11 | Aeromobile. |
Publications (1)
Publication Number | Publication Date |
---|---|
US1115162A true US1115162A (en) | 1914-10-27 |
Family
ID=3183344
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US44795108A Expired - Lifetime US1115162A (en) | 1908-08-11 | 1908-08-11 | Aeromobile. |
Country Status (1)
Country | Link |
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US (1) | US1115162A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3572969A (en) * | 1969-05-13 | 1971-03-30 | Gen Motors Corp | Turbomachine rotor |
US4029435A (en) * | 1976-01-29 | 1977-06-14 | Barker Sidney L | Retractable blade for a helicopter rotor |
US4036916A (en) * | 1975-06-05 | 1977-07-19 | Agsten Carl F | Wind driven electric power generator |
-
1908
- 1908-08-11 US US44795108A patent/US1115162A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3572969A (en) * | 1969-05-13 | 1971-03-30 | Gen Motors Corp | Turbomachine rotor |
US4036916A (en) * | 1975-06-05 | 1977-07-19 | Agsten Carl F | Wind driven electric power generator |
US4029435A (en) * | 1976-01-29 | 1977-06-14 | Barker Sidney L | Retractable blade for a helicopter rotor |
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