US1927247A - Method of making propeller blades - Google Patents
Method of making propeller blades Download PDFInfo
- Publication number
- US1927247A US1927247A US454137A US45413730A US1927247A US 1927247 A US1927247 A US 1927247A US 454137 A US454137 A US 454137A US 45413730 A US45413730 A US 45413730A US 1927247 A US1927247 A US 1927247A
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- blank
- pressure
- pressing
- tube
- dies
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- Expired - Lifetime
Links
- 238000004519 manufacturing process Methods 0.000 title description 2
- 238000003825 pressing Methods 0.000 description 25
- 238000000034 method Methods 0.000 description 21
- 239000002184 metal Substances 0.000 description 13
- 230000006835 compression Effects 0.000 description 8
- 238000007906 compression Methods 0.000 description 8
- 208000020401 Depressive disease Diseases 0.000 description 7
- 239000012530 fluid Substances 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 7
- 238000007493 shaping process Methods 0.000 description 7
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 7
- 238000007723 die pressing method Methods 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000001816 cooling Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 208000018999 crinkle Diseases 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 235000019628 coolness Nutrition 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/78—Making other particular articles propeller blades; turbine blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49332—Propeller making
- Y10T29/49334—Utilizing hollow tube blank
Definitions
- This invention relates to a method of working metal tubes and to apparatus used to carry out this method, and has particular reference to certain steps in the manufacture of airplane propeller blades out of preheated tubes during which the tube is subjected to internal and external pressure.
- One object of this invention is to provide, in a general pressing operation in which a tubular body is being changed in cross-section, suitable internal bracing, yielding and pressing means to cooperate with the external pressing means.
- Another object is to provide such an internal bracing means and pressure forming means that will be applicable to the interior of a heated tube.
- Another object is to provide a means for maintaining the interior of a heated tubular body under suitable pressure while simultaneously modifying the cross sectional shape thereof by external pressure, the means for providing such internal pressure being such as to result in a minimum amount of cooling effect on the body.
- Another object is to provide compressed fluid supply means that will not allow any substantial expansion (and resultant cooling) of the fluid in entering the interior of the tube being processed.
- Another object is to provide internal pressure means cooperating with the external pressure means during the pressing operation and then, after the external pressing has been completed, greatly increasing the internal pressure to insure exact conformance of the tubular body with the shape desired'in the. final product.
- Another object is to provide suitable apparatus for carrying out such methods.
- I avoid this diificulty by providing internal as well as external pressing means, by maintaining the tube hot during the process, by using a compressed internal pressing fluid that is given very little chance to expand and cool thereby, and by using a relatively small internal pressure during the closing of the dies and -a. relatively great pressure after they are closed.
- a tubular unit for purposes of illustration a blank 6 for an airplane propeller, is shown as having a co-extensive internal cavity 7 and at its lower end is provided with an outstanding radial flange 8.
- a .conducting pipe 9 is connected in communication with the interior of the blank 6 by means of a flange 11 on the conducting pipe.
- the lower annular surface of the outstanding radial flangeB on the blank 6 and the flange 11 on the conducting pipe are drawn into contacting relation by means of nuts 12 and bolts 13 and a ring flange 14 received over the blank 6.
- These surfaces may be provided with any suit-. able means such as gasket packing or by a ground fit between the respective surfaces thereof, to prevent any substantial loss of fluid therebetween during the forming process.
- the communicating pipe 9 extends to a selective supply valve 10 and is thereby selectively connected to an airline 15, or to a high pressure air compressor generally designated as 16, to permit the interior of the blank to be selectively filled with low or high pressure air. It may be noted that in Fig. 1 the compressor assembly 16 is shown on a considerably more reduced scale than the other portion of the figure.
- the air line 15 may be the usual type of shop air line used in most foundries and other shops and contains air which may be under a pressure of 100 lbs. per square inch and having the usual supply means therefor, although it will be understood that pressures between 50 lbs. per square inch and 500 lbs. per square inch may be practical for this operation depending upon circumstances.
- the air compressor 16 preferably consists of a compression tank 1'7 in which a compressible fluid such as air 18 is compressed by its displacement by an uncompressible fluid such as water 19.
- a compressible fluid such as air 18
- an uncompressible fluid such as water 19.
- the hydraulic pump 32 may be any usual type of positive acting pump and is shown in this embodiment-for the purpose of illustration as a usual type of gear pump driven by an electric motor by means of pulleys 34 and 3t; and belt 37, and obtaining its supply of water by means of a water supply pipe 38 running to a convenient source of water 39.
- any transverse section thereof is preferably in exact conformance to the perimeter of the depressions 33 and &6 as measured in a plane corresponding with' such transverse section.
- the circumference of each increment of length of the tube is equal to the perimeter of the corresponding increment of length of the finished article and the metal of the tube, while bent to a new and different shape, is not elongated'or compressed in any part of its internal structure during the process. Because of this the material of the tube or blank is not subjected to such stresses as would tend to rupture or weaken it or cause it to fold up or crinkle during the forming operation.
- the operation is as follows:
- the relief valve 2 is set to yield at a suitable predetermined prom which may be, for example 3,000 pounds to the squarednch, although the pressures may range from 1,000 to mono lbs. per square inch depend- 'rl s p dis heated in a 1:
- the tube until it reaches a suitable predetermined heat, which may be between 2282 degrees Fahrenheit and 1652 degrees Fahrenheit for soft steel, or between 1922 degrees Fahrenheit and 1292 degrees Fahrenheit for steel with a carbon content of .85 per cent or greater carbon percentage.
- a suitable predetermined heat which may be between 2282 degrees Fahrenheit and 1652 degrees Fahrenheit for soft steel, or between 1922 degrees Fahrenheit and 1292 degrees Fahrenheit for steel with a carbon content of .85 per cent or greater carbon percentage.
- the tube When the tube reaches the predetermined heat it is withdrawn from the furnace and placed between the. dies.
- the conducting pipe .9 is then rigidly and detachably secured thereby by means of the described attaching means 11, 12 and 13 or any other suitable attaching means.
- the valve 10 is then turned to admit air from the shop air line 15 to the conducting pipe 9.
- the communicating pipe 9 preferably has an internal passage 10 comparable in diameter with the interior 7 of the tubular blank 6 and the pipe 15 of the shop air line, the compressed air in passing into it from the shop air supply (not shown) does not materially expand, but is compressed all along the line, avoiding the cool ing sheet that would be caused by expansion through a restricted orifice.
- the dies 41 and 42 are now brought together on the blank 6 and as they come together they press the blank between them and the internal pressure of the air tends to prevent collapsing of the blank beyond that defined by the. die depressions and prevents any tendency of the tube to crinkle or buckle. 1
- valve 10 As soon as the die halves are brought together the valve 10 is turned so that it is in the position shown in Fig. l, which allows the passage of air from the compression chamber 18 into the con- I ducting pipe 9.
- the motor 33 is started which causes the pump 32 to force water from ⁇ the supply 38 into the 11-5 compression chamber 1'? wherein it compresses the air until the relief valve 21 opens at the set pressure which may be 3000 lbs. per square inch.
- the air within the tank 17, may be brought to a suitable pressure before the tan valve 10 is turned to connect the blank with the tank 17, in which case this pressure is immediately applied to the interior of the blank when the valve 10 is turned as above described.
- the communicating pipe 9 has an internal passage 10 comparable in diameter with the interior '1 of the tubular blank d-and the pipe 20 leading to the compression chamber, the compressed air 18 in passing into it from the compression chamber 17 does not materially expand, but instead is compressed all along the line avoiding the cooling eifect that would be caused by the expansion of air through a restricted orifice into the hollow interior of the tubular blank.
- the same method may be used throughout, utilizing the same apparatus and the same tubular blank, but omitting the heating of the tubular blank, as under certain favorable circumstances the preheating of the blank is unnecessary.
- the method of bringing said blank to the desired cross-sectional shape comprising placing said blank between a pair of dies having matching depressions of the desired size, shape and contour, subjecting said blank to an internal expanding pressure of from 50 to 500 lbs. per square inch while bringing said dies together, and then increasing said pressure to from 1,000 to 10,000 lbs. per square inch while the dies are fully closed.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
Description
Sept. 119 1933a J. soumss 1,927,247
METHOD MAKING PROPELLER BLADES Filed m 20, 1930 &
INVENIOR J5 Jyazres.
@hzl HM ATTORNEKS,
Patented Sept. 19-, 1933 UNITED STATES ENT OFFICE 11 ('ilaims.
This invention relates to a method of working metal tubes and to apparatus used to carry out this method, and has particular reference to certain steps in the manufacture of airplane propeller blades out of preheated tubes during which the tube is subjected to internal and external pressure.
One object of this invention is to provide, in a general pressing operation in which a tubular body is being changed in cross-section, suitable internal bracing, yielding and pressing means to cooperate with the external pressing means.
Another object is to provide such an internal bracing means and pressure forming means that will be applicable to the interior of a heated tube.
Another object is to provide a means for maintaining the interior of a heated tubular body under suitable pressure while simultaneously modifying the cross sectional shape thereof by external pressure, the means for providing such internal pressure being such as to result in a minimum amount of cooling effect on the body.
Another object is to provide compressed fluid supply means that will not allow any substantial expansion (and resultant cooling) of the fluid in entering the interior of the tube being processed.
, Another object is to provide internal pressure means cooperating with the external pressure means during the pressing operation and then, after the external pressing has been completed, greatly increasing the internal pressure to insure exact conformance of the tubular body with the shape desired'in the. final product.
Another object is to provide suitable apparatus for carrying out such methods.
Numerous other objects and features of novelty will be apparent in the accompanying specifica-- reference numerals apply to like parts throughout the figures of the-drawing.
, relation of the parts after the forming dies have been brought together.
The method described in this appllcationior patent is particularly useful in working or forming propeller blades of elongated tubular seamless steel closed tubes or blanks, but the method is equally applicable for use in connection with the forming of any type of hollow body wherein the cross-sectional shape of the hollow body is to be changed by compressing the article between forming dies.-
In the process of forming objects from tubular blanks or tubes by pressure, considerable difficulty has been experienced where the change involved in the cross-sectional proportions of the article during the forming operation is relatively great.
The tendency to buckle, crack, or crinkle increases directly as the relative change in proportion increases, and previous efforts have failed where this change has been relatively great.
I avoid this diificulty by providing internal as well as external pressing means, by maintaining the tube hot during the process, by using a compressed internal pressing fluid that is given very little chance to expand and cool thereby, and by using a relatively small internal pressure during the closing of the dies and -a. relatively great pressure after they are closed.
In Fig. 1 such a tubular unit, for purposes of illustration a blank 6 for an airplane propeller, is shown as having a co-extensive internal cavity 7 and at its lower end is provided with an outstanding radial flange 8. A .conducting pipe 9 is connected in communication with the interior of the blank 6 by means of a flange 11 on the conducting pipe. The lower annular surface of the outstanding radial flangeB on the blank 6 and the flange 11 on the conducting pipe are drawn into contacting relation by means of nuts 12 and bolts 13 and a ring flange 14 received over the blank 6.
These surfaces may be provided with any suit-. able means such as gasket packing or by a ground fit between the respective surfaces thereof, to prevent any substantial loss of fluid therebetween during the forming process.
The communicating pipe 9 extends to a selective supply valve 10 and is thereby selectively connected to an airline 15, or to a high pressure air compressor generally designated as 16, to permit the interior of the blank to be selectively filled with low or high pressure air. It may be noted that in Fig. 1 the compressor assembly 16 is shown on a considerably more reduced scale than the other portion of the figure.
The air line 15 may be the usual type of shop air line used in most foundries and other shops and contains air which may be under a pressure of 100 lbs. per square inch and having the usual supply means therefor, although it will be understood that pressures between 50 lbs. per square inch and 500 lbs. per square inch may be practical for this operation depending upon circumstances.
The air compressor 16 preferably consists of a compression tank 1'7 in which a compressible fluid such as air 18 is compressed by its displacement by an uncompressible fluid such as water 19. I prefer to provide a relief valve for the tank 17 and consequently I rigidly secure to a portion of the upper wall of compression tank a relief valve casing 21 enclosing a valve-forming ball 24 constantly urged towards closed position by the spring portion of the compression chamber and is fedthereto by a conducting pipe 31 from a hydraulic pump 32 actuated by an electric motor 33, or other suitable source of power. The hydraulic pump 32 may be any usual type of positive acting pump and is shown in this embodiment-for the purpose of illustration as a usual type of gear pump driven by an electric motor by means of pulleys 34 and 3t; and belt 37, and obtaining its supply of water by means of a water supply pipe 38 running to a convenient source of water 39. Q
In Figs. 2 and 3 the forming dies 41 and 42,
\ between which the blank is adapted to be received and be modified incross-sectional shape thereby, are provided with flat surfaces 43 for limiting their travel and with forming surfaces or depressions 44 and 46 which give to the article being formed in the dies the desired cross-sectional and other configuration. These dies may be operated by a hydraulic press, the hydraulic cylinder of which may be actuated by water pressure from the pump 32. v I
The circumference of the tube or blank 6, at
any transverse section thereof, is preferably in exact conformance to the perimeter of the depressions 33 and &6 as measured in a plane corresponding with' such transverse section. I Because of this the circumference of each increment of length of the tube is equal to the perimeter of the corresponding increment of length of the finished article and the metal of the tube, while bent to a new and different shape, is not elongated'or compressed in any part of its internal structure during the process. Because of this the material of the tube or blank is not subjected to such stresses as would tend to rupture or weaken it or cause it to fold up or crinkle during the forming operation. a
The operation is as follows: The relief valve 2 is set to yield at a suitable predetermined prom which may be, for example 3,000 pounds to the squarednch, although the pressures may range from 1,000 to mono lbs. per square inch depend- 'rl s p dis heated in a 1:
The tube until it reaches a suitable predetermined heat, which may be between 2282 degrees Fahrenheit and 1652 degrees Fahrenheit for soft steel, or between 1922 degrees Fahrenheit and 1292 degrees Fahrenheit for steel with a carbon content of .85 per cent or greater carbon percentage.
When the tube reaches the predetermined heat it is withdrawn from the furnace and placed between the. dies. The conducting pipe .9 is then rigidly and detachably secured thereby by means of the described attaching means 11, 12 and 13 or any other suitable attaching means. The valve 10 is then turned to admit air from the shop air line 15 to the conducting pipe 9.
Because the communicating pipe 9 preferably has an internal passage 10 comparable in diameter with the interior 7 of the tubular blank 6 and the pipe 15 of the shop air line, the compressed air in passing into it from the shop air supply (not shown) does not materially expand, but is compressed all along the line, avoiding the cool ing sheet that would be caused by expansion through a restricted orifice.
The dies 41 and 42 are now brought together on the blank 6 and as they come together they press the blank between them and the internal pressure of the air tends to prevent collapsing of the blank beyond that defined by the. die depressions and prevents any tendency of the tube to crinkle or buckle. 1
As soon as the die halves are brought together the valve 10 is turned so that it is in the position shown in Fig. l, which allows the passage of air from the compression chamber 18 into the con- I ducting pipe 9.
At this point there may or may not be any water in the compression tank 17. If not, then as soon as the valve 10 connects it to the blank 6 the motor 33 is started which causes the pump 32 to force water from} the supply 38 into the 11-5 compression chamber 1'? wherein it compresses the air until the relief valve 21 opens at the set pressure which may be 3000 lbs. per square inch.
On the other hand, the air within the tank 17, may be brought to a suitable pressure before the tan valve 10 is turned to connect the blank with the tank 17, in which case this pressure is immediately applied to the interior of the blank when the valve 10 is turned as above described.
Because the communicating pipe 9 has an internal passage 10 comparable in diameter with the interior '1 of the tubular blank d-and the pipe 20 leading to the compression chamber, the compressed air 18 in passing into it from the compression chamber 17 does not materially expand, but instead is compressed all along the line avoiding the cooling eifect that would be caused by the expansion of air through a restricted orifice into the hollow interior of the tubular blank.
Inasmuch as air has a very low specific heat, and inasmuch as its temperature is not materially lowered by expansion in being introduced into ids . the blank, the reduction of the temperature of the blank due to the introduction of the air into it is substantially negligible, and this feature is of prime importance.- 7
The great pressure of this air "on the interior of the blank forces the heated metal thereof evenly and firmly outwardly against the surfaces of the depressions 44 and t6 and causes the tube to take the exact internal shape of the depres sions, straightening out any crumpled parts there by, and setting the crystalline structure of themetal of the tube so that it will thereafter exactly it pressed form. ltmay' be leit under this pressure until below the critical temperature (1652 Fahrenheit for soft steel and 1292 Fahrenheit for .85 carbon steel) corresponding to the material, after which the air pressure may be relieved, the die halves separated, and the blank removed from the dies and disconnected from the pipe 9.
Under certain conditions the same method may be used throughout, utilizing the same apparatus and the same tubular blank, but omitting the heating of the tubular blank, as under certain favorable circumstances the preheating of the blank is unnecessary.
The advantages of this method are too numerous to properly enumerate; by means of this hot, dry elastic gas in the interior of the blank furnishing forming pressure during the operation greater changes in cross-section may be accomplished than would be normally possible, and by use of the final high pressure exact conformance of the finished blade to the desired shape and contour is assured.
While I have shown in the drawing a. particular illustrative form of my apparatus various modifications may be made in the same and in the various features of construction without materially changing the invention therein, and formal changes may be made in the specific embodiment of the invention described without departing from the spirit or substance of the broad invention, the scope of which is commensurate with the appended claims.
I claim:
- 1. In the formation of a propeller blade from a tubular metallic blank by modifying the crosssectional shape thereof between a pair of dies, the successive steps of subjecting said blank to a material internal expansive pressure during closing of the dies and a materially greater internal expansive pressure thereafter while maintaining said dies in fully closed positions.
2. In the formation of a propeller blade from a hollow metallic blank, the method of bringing said blank to the desired cross-sectional shape comprising placing said blank between a pair of dies having matching depressions of the desired size, shape and contour, subjecting said blank to an internal expanding pressure of from 50 to 500 lbs. per square inch while bringing said dies together, and then increasing said pressure to from 1,000 to 10,000 lbs. per square inch while the dies are fully closed.
3. The method of forming a hollow metal propeller blade from a tubular blank, comprising heating said blank, placing said blank in heated condition between a pair 01' dies having match-v ing depressions therein of the desired shape and size, bringing said dies together while maintaining the interior of said tube under internal pressure to resist inward collapsing of the walls there-' of and then subjecting the interior of said blank while said dies are retained in fully closed positions to an increased internal pressure suflicient to work the crystalline structure of the metal of said blank.
4. The method of shaping a metal tube which consists in die pressing it, externally, and expansively pressing it internally gently during the die pressing by the admission of gas under moderate pressure, and then firmly expansively pressing it internally by the admission of gas under a greater pressure while braced against undesirable expansion by said die.
5. The method of shaping a metal tube which consists in die pressing it externally, expansively pressing it internally gently during the die pressing, and then firmly expansively pressing it internally while maintained between said dies in fully 'closed condition.
6. The method of shaping a metal tube which consists in heating the tube, die pressing it externally, and expansively pressing it internally expansively pressing it internally while the dies are held together in fully closed relation.
8. The method of shaping a metal tube which consists in heating the tube, pressing it internally and externally simultaneously into final shape, and then bracing it in final shape externally and internally expansively pressing it with force materially greater than that employed in, the first internal pressing operation.
9. The method of shaping a metal tube which consists in heating the tube, pressing it internally and externally simultaneously into final shape, and then bracing it in final shape externally and pressing it internally with a materially increased expansive pressure that would rupture it if not so externally braced.
10. The method of shaping a metal tube which consists in heating the tube to above its critical temperature, pressing it internally and externally simultaneously into final shape, said internal pressing being accomplished by a fluid under pressure, and then bracing it in final shape externally and internally expansively pressing it with a force relatively greater than that employed in the first mentioned internal pressing operation, until it is below its critical temperature. I
11. The method of shaping a metal tube which consists in heating the tube to a temperature above the critical point of the metal, pressing it internally and externally simultaneously into final shape, and then bracing it in final shape extemelly and internally expansively pressing it with a force materially greater than that employed in the first mentioned internal pressing operation.
JOHN SQUIRES.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US454137A US1927247A (en) | 1930-05-20 | 1930-05-20 | Method of making propeller blades |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US454137A US1927247A (en) | 1930-05-20 | 1930-05-20 | Method of making propeller blades |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1927247A true US1927247A (en) | 1933-09-19 |
Family
ID=23803456
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US454137A Expired - Lifetime US1927247A (en) | 1930-05-20 | 1930-05-20 | Method of making propeller blades |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1927247A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2440127A (en) * | 1944-07-31 | 1948-04-20 | Curtiss Wright Corp | Art of producing propeller blades |
| US2577336A (en) * | 1943-04-23 | 1951-12-04 | United Aircraft Corp | Method of making propeller blades |
| US2652121A (en) * | 1950-06-06 | 1953-09-15 | United Aircraft Corp | Hollow propeller blade with bulbed core |
| US2849788A (en) * | 1952-08-02 | 1958-09-02 | A V Roe Canada Ltd | Method and apparatus for making hollow blades |
| US2927953A (en) * | 1957-01-28 | 1960-03-08 | Itt | Electrical lead conductor |
| US2944327A (en) * | 1956-10-17 | 1960-07-12 | Curtiss Wright Corp | Method of making hollow blades for turbine engines |
| US3008223A (en) * | 1955-09-29 | 1961-11-14 | Curtiss Wright Corp | Methods of manufacture of compressor blades |
-
1930
- 1930-05-20 US US454137A patent/US1927247A/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2577336A (en) * | 1943-04-23 | 1951-12-04 | United Aircraft Corp | Method of making propeller blades |
| US2440127A (en) * | 1944-07-31 | 1948-04-20 | Curtiss Wright Corp | Art of producing propeller blades |
| US2652121A (en) * | 1950-06-06 | 1953-09-15 | United Aircraft Corp | Hollow propeller blade with bulbed core |
| US2849788A (en) * | 1952-08-02 | 1958-09-02 | A V Roe Canada Ltd | Method and apparatus for making hollow blades |
| US3008223A (en) * | 1955-09-29 | 1961-11-14 | Curtiss Wright Corp | Methods of manufacture of compressor blades |
| US2944327A (en) * | 1956-10-17 | 1960-07-12 | Curtiss Wright Corp | Method of making hollow blades for turbine engines |
| US2927953A (en) * | 1957-01-28 | 1960-03-08 | Itt | Electrical lead conductor |
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