US1896089A - Vacuum propeller plane - Google Patents

Vacuum propeller plane Download PDF

Info

Publication number
US1896089A
US1896089A US547360A US54736031A US1896089A US 1896089 A US1896089 A US 1896089A US 547360 A US547360 A US 547360A US 54736031 A US54736031 A US 54736031A US 1896089 A US1896089 A US 1896089A
Authority
US
United States
Prior art keywords
planes
disk
air
vacuum
propeller plane
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
Application number
US547360A
Inventor
Krogh Otto Christensen
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.)
Individual
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of US1896089A publication Critical patent/US1896089A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48Units of two or more coaxial propellers

Definitions

  • My invention relates to a vacuum propeller plane, consisting of a plain, circular disk on one side of which are mounted airrarefying planes, which when rotating together with the said dlsk, will produce a lower pressure thanthe atmospherical pressure on the sideof the disk to which the are fixed, while the opposite side of the disk approximately is subjected to the pressure 9 of the atmosphere.
  • the produced difference of pressure can be utilized for propulsion of a body in the direction of the axis of the rotation shaft, for
  • the ventilation technics When utilized in aero lanes their safety will increase, and they wi be able to go vertically upward, to stand still in the air, or 30 End without the often sofatal sliding i t. the ventilation technics the invention can be utilized in agricultural machines, dryin installations, dust suckers and the like.
  • Fig. 3 a section on the line 'CD, in Fig. 1, and v Fig. 4-the vacuum propeller plane in per spective, whilst Fig. 5 shows a number of vacuum planes decreasing in radiate direc- 56 tion and mounted on a common shaft.
  • a round disk 1 is provided with a shaft 2, the hub of which is concentrical with the disk.
  • Two air-raregying planes 3 and 4 are 00 mounted on the isk 1 in such a manner that they turn their current-line sha ed side upward, while their plain under si e is fastened to the disk 1.
  • Fi s. 2 and 3 show' sections of the air- 7 rare ying planes, in the left and the right side relatively.
  • the air-rarefyin planes are hollow and madein a manner ike that of the bearing-planes of an aeroplane.
  • arrow indicates the direction 7 of the rotation of the vacuum ropeller plane.
  • the air-rarefying planes 3 and 4 are connected mutually by the disk 1, the pieces 9 and 10 of the disk, see Fig. 4, will prevent a balancing of the pressure so that the vacuum produced by the planes 3 and 4 gets active on the whole areaof the disk 1, and thus the superiority of my vacuum propeller plane, as to utilizing the obtained, difference of pressure, is fully explained.
  • the back side of the air-rarefying planes can be shaped according to the riphery of the disk, and the cross-section o the air-rarefying lanes can decrease in the direction of the ra ius of the disk 1, in order to make the formation of the current-line as eas as possible.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)

Description

Feb. 7, 1933. o. c. KROGH 1,896,089
' VACUUM PROPELLER PLANE Filed June 27. 1931 2 Sheets-Sheet l z1; y a c R a ZE2 v I I 2 Feb. 7, 1933, o. c. KROGH VACUUM PHOPELLER PLANE Filed June 27, 1931 2 Sheets-Sheet 2 r ams F b. 1.1m
UNITED STATES PATENT OFFICE '1'10 CHBIBTDTSH KBOGE, OI ODENSE, DENMARK VACUUH PROPELLER PLANE Application fled June 87, 1981, Serial No. 547,860, and in Denmark July 29, 1939.
My invention relates to a vacuum propeller plane, consisting of a plain, circular disk on one side of which are mounted airrarefying planes, which when rotating together with the said dlsk, will produce a lower pressure thanthe atmospherical pressure on the sideof the disk to which the are fixed, while the opposite side of the disk approximately is subjected to the pressure 9 of the atmosphere. p
The produced difference of pressure can be utilized for propulsion of a body in the direction of the axis of the rotation shaft, for
instance for aeroplanes, or for producing air currents for ventilation purposes, dust suckers and the like.
It is well-known that the bearing-planesof aero lanes are current-line shaped in order to pr uce, by a certain speed, a lower pressure (vacuum) on the upper side of the planes, which in co-action with the pressure on the under side gives the necessary buoyancy to the aero lanes.
It is also wellown to 've the air-proeller blades 9. current-line fi iaped fore-side, y which means, a lower pressure is roduced on this fore-side, whilst the'back si e, which is placed aslant presses the air together, if
30 anything, but as the air can stream freely from the front to the back side in the rotation plane of the ropeller, the produced vacuum is not turne to account to such a degree as by my invention.
By means of my vacuum propeller plane it is possible to obtain a considerably greater 'buo ancy or .propulsion than by formerly used elements.
When utilized in aero lanes their safety will increase, and they wi be able to go vertically upward, to stand still in the air, or 30 End without the often sofatal sliding i t. the ventilation technics the invention can be utilized in agricultural machines, dryin installations, dust suckers and the like.
y invention is illustrated in the accompanying drawing, in which Figure 1 shows the vacuum propeller plane in top view; Fig. 2 a section on the hue AB, in F g. 1;
Fig. 3 a section on the line 'CD, in Fig. 1, and v Fig. 4-the vacuum propeller plane in per spective, whilst Fig. 5 shows a number of vacuum planes decreasing in radiate direc- 56 tion and mounted on a common shaft.
In Fig. 1 a round disk 1 is provided with a shaft 2, the hub of which is concentrical with the disk.
Two air- raregying planes 3 and 4 are 00 mounted on the isk 1 in such a manner that they turn their current-line sha ed side upward, while their plain under si e is fastened to the disk 1.
'The fore-edges 5 and 6 of the air-raref in 66 planes 3 and 4 are lying radiately on the dis% '1, and the back edges 7 and 8, which are parallel with the fore-edges 5 and 6,- form tangents to the circumference of the disk 1.
Fi s. 2 and 3 show' sections of the air- 7 rare ying planes, in the left and the right side relatively. The air-rarefyin planes are hollow and madein a manner ike that of the bearing-planes of an aeroplane.
In Fig. 4 the arrow indicates the direction 7 of the rotation of the vacuum ropeller plane.
By the quick rotation of t e vacuum propeller plane the relative movement of the air, immediately 'above the air-rarefying planes, partly will follow current-lines, by 30 which means the lower pressure as known from the current-line theory is produced on the upper side of the air-rarefying planes. The underside of the disk 1. being plain,
nearly a normal air-pressure will be reigning here.
As the air-rarefying planes 3 and 4 are connected mutually by the disk 1, the pieces 9 and 10 of the disk, see Fig. 4, will prevent a balancing of the pressure so that the vacuum produced by the planes 3 and 4 gets active on the whole areaof the disk 1, and thus the superiority of my vacuum propeller plane, as to utilizing the obtained, difference of pressure, is fully explained. Instead of straight back sides 7 and 8, the back side of the air-rarefying planes can be shaped according to the riphery of the disk, and the cross-section o the air-rarefying lanes can decrease in the direction of the ra ius of the disk 1, in order to make the formation of the current-line as eas as possible.
Having thus described my invention, I claim:
- 5 1. In vacuum pro eller planes the combination, with a circu ar disk, of a number of current-line shaped air-rarefying -planes mounted on one side of the said disk, and means for rotating the said disk in order to obtain a lower pressure all over its area on that side, on which the air-rarefying planes are mounted.
2. In vacuum propeller planes the combination, with a disk, of air-rarefying planes mutually connected by the said disk and having their back sides shaped according to the periphery of the disk, on one side of which they are mounted.
3. In "acuum propeller planes the combination, with a (118k, of air-rarefying planes mounted on one side of the disk, and the cross section of which decreases outward in radiate direction, correslponding to the speed.
4. In vacuum propel 'er planes the combination of at least one disk on one side of which air-rarefying planes are mounted, a number ofgroups of such planes, and a common shaft.
In witness whereof I have hereunto set 9 my hand.
OTTO CHRISTENSEN KROGH.
US547360A 1929-07-29 1931-06-27 Vacuum propeller plane Expired - Lifetime US1896089A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DK1896089X 1929-07-29

Publications (1)

Publication Number Publication Date
US1896089A true US1896089A (en) 1933-02-07

Family

ID=8158215

Family Applications (1)

Application Number Title Priority Date Filing Date
US547360A Expired - Lifetime US1896089A (en) 1929-07-29 1931-06-27 Vacuum propeller plane

Country Status (1)

Country Link
US (1) US1896089A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5490763A (en) * 1994-09-15 1996-02-13 Abrams; Andrew L. Pump for shear sensitive fluids

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5490763A (en) * 1994-09-15 1996-02-13 Abrams; Andrew L. Pump for shear sensitive fluids

Similar Documents

Publication Publication Date Title
US3123321A (en) Aircraft channel wing propeller combination
US1896089A (en) Vacuum propeller plane
US1875276A (en) Airckaft of the heavier than air type
USRE18122E (en) Arrangement por exchanging energy between a current and a body therein
US2230398A (en) Aeroturbine propeller
US3101917A (en) Ducted rotor with pressure balancing and lift augmenting means
US1824195A (en) Helicopter
US1986151A (en) Fan
US2918978A (en) Variable contour propeller blades
US3288396A (en) Aircraft having disc-shaped rotating wings
US3603700A (en) Rotating circular wing
US2918128A (en) Propeller
US2397189A (en) Airplane
US1786017A (en) Helicopter
US1876682A (en) Aircraft
US2103242A (en) Aircraft propeller
US1012308A (en) Screw-propeller.
US1365314A (en) Variable-pitch propeller
US1907394A (en) Aeroplane
US1971820A (en) Helicopter airscrew
US2030622A (en) Propeller, fan, and exhauster
US1401537A (en) Aircraft-propeller
US1923325A (en) Airplane propeller
US1927753A (en) Aeroplane
US1397400A (en) burrill