US1423113A - Screw propeller and the like - Google Patents
Screw propeller and the like Download PDFInfo
- Publication number
- US1423113A US1423113A US530952A US53095222A US1423113A US 1423113 A US1423113 A US 1423113A US 530952 A US530952 A US 530952A US 53095222 A US53095222 A US 53095222A US 1423113 A US1423113 A US 1423113A
- Authority
- US
- United States
- Prior art keywords
- central part
- blades
- angle
- camber
- chord
- 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
- 230000007423 decrease Effects 0.000 description 5
- 230000007246 mechanism Effects 0.000 description 3
- 239000012530 fluid Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
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
- B64C11/16—Blades
Definitions
- This invention relates to screw propellers
- FIGS. 1 and 2 are views in elevation and plan of one form theinvention may assume.
- I Figs. 3 and'd are similar views oil. another term, and
- Figs. 5, 6, 7, 8 and 9 are views in transverse section on line a, a; 4, 4L; b, F); 5, 5; and c, 0; in Figs. 2 and 4.
- the blades of the improved propeller each consist of three essential parts, a main or central part 1 which is of quadrangular shape in plan and two end parts 2 and which in plan are so cut away from their points of junction on the lines 4, 1- and 5 respectively with the main or central part 1 that the leading edges 6 and 7 oi the parts 2 and 3 are swept back until they meet the trailing edges 8 and 9 of said parts which are continuations of the trailing edge 10 of the main or central part 1.
- the shape of the main or central part 1 in cross section is such that its chord gradu ally increases from its inner side i. e. from the point a to its outer side i. e. to the point 5, and both its camber and its angle of incidence to the helical plane decrease from its Specification of Letters Patent. fgtentgd J l 13 1922 Application filed January 21, 1922.
- Serial No. 530,952 I inner to its outer side, that is from the point 4 to the point 5.
- the cross section of the inner end part 2 is such that its chord, camber and angle of incidence to the helical plane are all gradually increased from its tip 11 to its junction 1 with the main or central part 1 where said. chord, camber and angle of incidence coincide with those of said main or centralpart at that point.
- the cross section of the outer end part 3 is such that itschord, camber and, angle of incidence to the heli cal plane are all gradually reduced from its junction 5 with the main or central part 1- wheresaid chord, .amber and angle of in cidence coincide with those of said main or central part at that point-'to its tip 12, as is clearly shown in. Figs. 5 to 9 in which the lines at represent the helical plane.
- the blades may either be mounted on the shaft 13 of the propeller by means of radi-o ally arranged L-shaped arms 14lcarried by a central boss 15 as shown in Figs. 1 and 2, or said blades may be mounted by their inner ends on projections 16 carried by or. formed in one with the central boss 15 adapted to be mounted on the shaft 13 as shown in Figs. 3 and t said projections being of stream-line form and their points of junction with the blades being such as will not cause any disturbance of the positive pressure along the leading edge of the blades.
- a blade for screw propellers, windmills, and like fluid operating or operated'mechanisms comprising a central part and two end parts, the shape in plan of the central part being quadrangular'and its shape in cross section being such that its chord gradually increases from; its inner side and its camber and angle of incidence relative to the helical plane decreases towards its outer side; and the shape of each of the end parts in plan being'such that it is cut away from its point of junction with the.
- each of said end parts in cross section being such that its chord, camber and angle of incidence to the helical plane are gradually reduced from their points of junc tion with the central part to their tips.
- Ablade for screw propellers and the quadrangular shape in plan and has such a shape in cross section that its chord increases gradually from the part intended to be nearest to the centre about which the blades rotate and both the camber of its rear surface and its angle of incidence relative to the helical plane decreases from said aforesaid part; and two end parts, each of which is cut away in plan from its point of junction with the central part so that its leading edge is swept back until it meets its trailing edge which is a continuation of the trailing edge of the central part, being so shaped in cross section that its chord, the camber of its rear surface and its angle oli incidence relative to the helical plane are gradually reduced from their points of juuction with the central part to their tips.
- a screw propeller or the like comprising a boss, radially arranged arms on said boss, and blades carried by said arms each of said blades comprising a central part which is 0t quadrangular shape in plan and has such a shape in cross section that its chord gradually increases from that part nearest to the boss, and both the camber of its rear surface and its angle of incidence relative to the helical plane decreases from that part nearest to the boss, and two end parts each of which is cut away in plan from its point of junction with the central part so that its leading edge is swept back until it meets its trailing edge which is a continuation of the trailing edge of the central part, the shape of each of said end parts in cross section being such that its chord the camber of its rear surface and its angle of incidence relative to the helical plane are gradually reduced from their points of junction with the central part to their tips.
- a screw propeller or the like comprising a plu 'ality of blades each of which includes a central part of quadrangular shape in plan and of such a shape in cross section that its chord gradually increases and both the camber of its rear surface and its angle of incidence relative to the helical plane decreases towards the outer end of the blade and two end parts each of which is cut away in plan from its point of junction with the central part so that its leading edge is swept back until it meets its trailing edge which is a continuation of the trailing edge of the central part, the shape of each of said parts in cross section being such that its chord, the camber of its rear surface and its angle of incidence relative to the helical plane are gradually reduced from their points of junction with the central part to their tips; a boss for carrying said blades; and connecting pieces between said blades and said boss which have a streamline form and are so shaped at their points of junction with the blades that they will not cause any disturbance of positive pressure along the leading edges of the blades.
Description
A. A. HOLLE.
SCREW PROPELLER AND THE LIKE.
APPLICATION HLED JAN.21, 1-922.
EAQSA 13L Patented July 18,1922.
3 SHEETS-SHEET I- A.'A. HOLLE. SCREW PROPELLER AND TfiE LIKE.
APPLICATION FILED JAN-21. 1922.
Patented-July 18, 1922 3 SHEETS-SHEET 2.
A. A. HOLLE.
SCREW PROPELLER AND THE LIKE.
APPLICATION FILED 11mm, 1922.
1,423, 1 1'3, Patented July 18, 1922 3 SHEETS-SHEET 3.
man 70,?
QiFt'illE.
PATENT ALEXANDER ALBERT HOLLE, 0F HYDE PARK, LONDON, ENGLAND. i
SCREW PROTELLER AND THE LIKE.
insane.
This invention relates to screw propellers,
water mills. windmills and like mechanism which operates either by d rect pressure om or is operated by the pressure out, the Hand in relation to which it rotates, and it consists of an improved form of blade which has for its object to obtain increased thrust and increased etliciency and to render the use of such mechanism of relatively small diam eter economically possible.
li ith these and other objects in view the invention comprises the various novel features ottconstruction, combination and arrangement of parts hereinafter fully described and specified in the claims hereto appended.
In the accompanying drawings in which like parts are denoted by. similar characters of reterence:
1 and 2 are views in elevation and plan of one form theinvention may assume. I Figs. 3 and'd are similar views oil. another term, and
Figs. 5, 6, 7, 8 and 9 are views in transverse section on line a, a; 4, 4L; b, F); 5, 5; and c, 0; in Figs. 2 and 4.
The blades of the improved propeller each consist of three essential parts, a main or central part 1 which is of quadrangular shape in plan and two end parts 2 and which in plan are so cut away from their points of junction on the lines 4, 1- and 5 respectively with the main or central part 1 that the leading edges 6 and 7 oi the parts 2 and 3 are swept back until they meet the trailing edges 8 and 9 of said parts which are continuations of the trailing edge 10 of the main or central part 1.
The shape of the main or central part 1 in cross section is such that its chord gradu ally increases from its inner side i. e. from the point a to its outer side i. e. to the point 5, and both its camber and its angle of incidence to the helical plane decrease from its Specification of Letters Patent. fgtentgd J l 13 1922 Application filed January 21, 1922.
Serial No. 530,952 I inner to its outer side, that is from the point 4 to the point 5.
The cross section of the inner end part 2 is such that its chord, camber and angle of incidence to the helical plane are all gradually increased from its tip 11 to its junction 1 with the main or central part 1 where said. chord, camber and angle of incidence coincide with those of said main or centralpart at that point. The cross section of the outer end part 3 is such that itschord, camber and, angle of incidence to the heli cal plane are all gradually reduced from its junction 5 with the main or central part 1- wheresaid chord, .amber and angle of in cidence coincide with those of said main or central part at that point-'to its tip 12, as is clearly shown in. Figs. 5 to 9 in which the lines at represent the helical plane.
The blades may either be mounted on the shaft 13 of the propeller by means of radi-o ally arranged L-shaped arms 14lcarried by a central boss 15 as shown in Figs. 1 and 2, or said blades may be mounted by their inner ends on projections 16 carried by or. formed in one with the central boss 15 adapted to be mounted on the shaft 13 as shown in Figs. 3 and t said projections being of stream-line form and their points of junction with the blades being such as will not cause any disturbance of the positive pressure along the leading edge of the blades.
lVhat I claim is 1. A blade for screw propellers, windmills, and like fluid operating or operated'mechanisms comprising a central part and two end parts, the shape in plan of the central part being quadrangular'and its shape in cross section being such that its chord gradually increases from; its inner side and its camber and angle of incidence relative to the helical plane decreases towards its outer side; and the shape of each of the end parts in plan being'such that it is cut away from its point of junction with the. central part so as to bring its leading edge back until it meets its trailing edge which is a continuation of the trailing edge of the central part, and the shape of each of said end parts in cross section being such that its chord, camber and angle of incidence to the helical plane are gradually reduced from their points of junc tion with the central part to their tips.=
2. Ablade for screw: propellers and the quadrangular shape in plan and has such a shape in cross section that its chord increases gradually from the part intended to be nearest to the centre about which the blades rotate and both the camber of its rear surface and its angle of incidence relative to the helical plane decreases from said aforesaid part; and two end parts, each of which is cut away in plan from its point of junction with the central part so that its leading edge is swept back until it meets its trailing edge which is a continuation of the trailing edge of the central part, being so shaped in cross section that its chord, the camber of its rear surface and its angle oli incidence relative to the helical plane are gradually reduced from their points of juuction with the central part to their tips.
3. A screw propeller or the like comprising a boss, radially arranged arms on said boss, and blades carried by said arms each of said blades comprising a central part which is 0t quadrangular shape in plan and has such a shape in cross section that its chord gradually increases from that part nearest to the boss, and both the camber of its rear surface and its angle of incidence relative to the helical plane decreases from that part nearest to the boss, and two end parts each of which is cut away in plan from its point of junction with the central part so that its leading edge is swept back until it meets its trailing edge which is a continuation of the trailing edge of the central part, the shape of each of said end parts in cross section being such that its chord the camber of its rear surface and its angle of incidence relative to the helical plane are gradually reduced from their points of junction with the central part to their tips.
4. A screw propeller or the like comprising a plu 'ality of blades each of which includes a central part of quadrangular shape in plan and of such a shape in cross section that its chord gradually increases and both the camber of its rear surface and its angle of incidence relative to the helical plane decreases towards the outer end of the blade and two end parts each of which is cut away in plan from its point of junction with the central part so that its leading edge is swept back until it meets its trailing edge which is a continuation of the trailing edge of the central part, the shape of each of said parts in cross section being such that its chord, the camber of its rear surface and its angle of incidence relative to the helical plane are gradually reduced from their points of junction with the central part to their tips; a boss for carrying said blades; and connecting pieces between said blades and said boss which have a streamline form and are so shaped at their points of junction with the blades that they will not cause any disturbance of positive pressure along the leading edges of the blades.
ALEXANDER ALBERT HOLLE.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US530952A US1423113A (en) | 1922-01-21 | 1922-01-21 | Screw propeller and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US530952A US1423113A (en) | 1922-01-21 | 1922-01-21 | Screw propeller and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
US1423113A true US1423113A (en) | 1922-07-18 |
Family
ID=24115655
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US530952A Expired - Lifetime US1423113A (en) | 1922-01-21 | 1922-01-21 | Screw propeller and the like |
Country Status (1)
Country | Link |
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US (1) | US1423113A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422388A (en) * | 1943-04-05 | 1947-06-17 | Arthur W Billings | Airplane propeller |
-
1922
- 1922-01-21 US US530952A patent/US1423113A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422388A (en) * | 1943-04-05 | 1947-06-17 | Arthur W Billings | Airplane propeller |
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