GB578994A - - Google Patents
Info
- Publication number
- GB578994A GB578994A GB578994DA GB578994A GB 578994 A GB578994 A GB 578994A GB 578994D A GB578994D A GB 578994DA GB 578994 A GB578994 A GB 578994A
- Authority
- GB
- United Kingdom
- Prior art keywords
- abutment
- frame
- jaws
- section
- datum line
- 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.)
- Active
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B5/00—Measuring arrangements characterised by the use of mechanical techniques
- G01B5/20—Measuring arrangements characterised by the use of mechanical techniques for measuring contours or curvatures
- G01B5/205—Measuring arrangements characterised by the use of mechanical techniques for measuring contours or curvatures of turbine blades or propellers
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- A Measuring Device Byusing Mechanical Method (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB578994T |
Publications (1)
Publication Number | Publication Date |
---|---|
GB578994A true GB578994A (enrdf_load_stackoverflow) |
Family
ID=10480316
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB578994D Active GB578994A (enrdf_load_stackoverflow) |
Country Status (2)
Country | Link |
---|---|
US (1) | US2402567A (enrdf_load_stackoverflow) |
GB (1) | GB578994A (enrdf_load_stackoverflow) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5625958A (en) * | 1995-09-06 | 1997-05-06 | United Technologies Corporation | Method and a gauge for measuring the service life remaining in a blade |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2737722A (en) * | 1956-03-13 | Propeller blade angle measuring device | ||
US2749623A (en) * | 1956-06-12 | La barre | ||
US2523226A (en) * | 1950-09-19 | Gauge for airfoils | ||
US2461143A (en) * | 1946-05-15 | 1949-02-08 | Western Electric Co | Gauging apparatus for checking the relative alignment of reference planes of spaced articles |
US2638680A (en) * | 1947-05-07 | 1953-05-19 | Baker Mfg Co | Averaging protractor for matching aircraft propeller blades |
US2636280A (en) * | 1947-12-02 | 1953-04-28 | Vasili S Drake | Propeller template |
FR3018910B1 (fr) * | 2014-03-19 | 2018-04-13 | Safran Aircraft Engines | Outil de controle d'une dimension d'une aube d'un disque aubage monobloc pour turbomachine d'aeronef |
-
0
- GB GB578994D patent/GB578994A/en active Active
- US US2402567D patent/US2402567A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5625958A (en) * | 1995-09-06 | 1997-05-06 | United Technologies Corporation | Method and a gauge for measuring the service life remaining in a blade |
Also Published As
Publication number | Publication date |
---|---|
US2402567A (en) | 1946-06-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB578994A (enrdf_load_stackoverflow) | ||
CN106741228A (zh) | 一种高升阻比可变尾翼的赛车空气动力学套件 | |
CN108583847B (zh) | 一种适用于长航时无人机的低雷诺数高功率因子翼型 | |
CN113092000B (zh) | 一种带外置电桥修正的片式铰链力矩天平的校准方法 | |
CN103482054A (zh) | 一种匹配全翼太阳能无人机的低雷诺数翼型 | |
CN213981061U (zh) | 一种风电机组叶片校零装置 | |
CN212501113U (zh) | 一种螺旋桨桨距角调节装置 | |
Goodson et al. | Wind-tunnel investigation at high subsonic speeds of the stability characteristics of a complete model having sweptback-, M-, W-, and cranked-wing plan forms and several horizontal-tail locations | |
Flechner | Experimental results of winglets on first, second, and third generation jet transports | |
FR3130319B1 (fr) | Turbomachine non carénée comprenant des aubes de stator présentant des cordes différentes | |
CN216801581U (zh) | 一种多夹具等距调节机构 | |
CN213933423U (zh) | 螺旋桨桨叶弯曲试验工装 | |
CN114180074B (zh) | 冲压翼伞主参数安装角调校方法 | |
CN219054119U (zh) | 一种车桥定位加工装置 | |
CN222269098U (zh) | 基于梯式电缆线桥架的焊接工作台结构 | |
CN220054146U (zh) | 一种直升机操纵拉杆修理与多参数调整控制台 | |
CN212145516U (zh) | 一种高效气动夹具 | |
Wilson Jr et al. | Aerodynamic Characteristics at High and Low Subsonic Mach Numbers of Four NACA 6-series Airfoil Sections at Angles of Attack from-2 to 31 Degrees | |
CN112324626A (zh) | 一种风电机组叶片校零装置 | |
Naeseth | Low-speed Longitudinal Aerodynamic Characteristics of a 45 Degree Sweptback Wing with Double Slotted Flaps | |
Weick | Full Scale Wind Tunnel Tests on Several Metal Propellers Having Different Blade Forms | |
Lockwood | Aerodynamic and lateral-control characteristics of a 1/28-scale model of the Bell X-1 airplane wing-fuselage combination: transonic-bump method | |
Hammond | Lateral-control investigation of flap-type controls on a wing with upswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: transonic-bump method | |
Lindsey | AIRFOIL SECTION CHARACTERISTICS AT TRANSONIC SPEEDS | |
Fuller et al. | Effects of thickness on supersonic performance of a wing-body configuration employing a warped highly swept arrow wing |